Airbus S.A.S.

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        Patent 706
        Trademark 217
Jurisdiction
        United States 685
        World 144
        Europe 73
        Canada 21
Owner / Subsidiary
[Owner] Airbus S.A.S. 923
Airbus Operations S.A.S. 199
Airbus Operations GmbH 95
Airbus Operations S.L. 22
Airbus Operations Limited 19
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Date
New (last 4 weeks) 4
2026 January (MTD) 2
2025 December 2
2025 November 12
2025 October 13
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IPC Class
G08G 5/00 - Traffic control systems for aircraft 38
B64D 45/00 - Aircraft indicators or protectors not otherwise provided for 37
B64D 11/00 - Passenger or crew accommodationFlight-deck installations not otherwise provided for 30
B64D 27/24 - Aircraft characterised by the type or position of power plants using steam or spring force 23
B64D 37/30 - Fuel systems for specific fuels 21
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NICE Class
12 - Land, air and water vehicles; parts of land vehicles 172
42 - Scientific, technological and industrial services, research and design 122
09 - Scientific and electric apparatus and instruments 98
37 - Construction and mining; installation and repair services 93
28 - Games; toys; sports equipment 77
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Status
Pending 207
Registered / In Force 716
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1.

Method, Computer Program, Computer-Readable Data Carrier And Computing Device For Deterministic Execution Of An Instruction Set As Well As Apparatus Comprising Same

      
Application Number 19249250
Status Pending
Filing Date 2025-06-25
First Publication Date 2026-01-01
Owner Airbus S.A.S. (France)
Inventor Uhrig, Sascha

Abstract

A method for deterministic execution of an instruction set (I) containing instructions (M) to be carried out by a processing unit of the computing device includes the steps of executing a predefined number of pre-branch instructions (A) up to a conditional branch (C) of the instruction set (I) containing at least one branch condition determining a subsequent instruction which is to be executed after the conditional branch (C); predicting at least one of the pre-branch instructions (A) and/or a target instruction (T) to be executed as the subsequent instruction if the at least one condition is met; and inserting the at least one predicted pre-branch instruction (A) and/or the target instruction (T) into the instruction set (I) after the conditional branch (C). A computer program, computer-readable data-carrier, computing device, and apparatus, such as a vehicle, in particular an aircraft may be configured to perform the method.

IPC Classes  ?

  • G06F 9/38 - Concurrent instruction execution, e.g. pipeline or look ahead
  • G06F 9/30 - Arrangements for executing machine instructions, e.g. instruction decode

2.

FILLING LEVEL MONITORING DEVICE FOR MONITORING THE FILLING LEVEL OF A FLUID CONTAINER, HYDROGEN TANK, AND AIRCRAFT COMPRISING SUCH HYDROGEN TANK

      
Application Number 19252036
Status Pending
Filing Date 2025-06-27
First Publication Date 2026-01-01
Owner
  • Airbus Operations GmbH (Germany)
  • Airbus (S.A.S.) (France)
Inventor
  • Schramm, Gerrit
  • Geisler, Helge
  • Meyerhoff, Thomas
  • Zoghaib, Lionel

Abstract

A filling level monitoring device includes an exciting element, first and second sensors, a signal source, and a processor. The exciting element can be mounted to the fluid container. The first and second sensors can be mounted to the fluid container at opposite sides. The signal source is connected to the exciting element and can generate an input signal including frequency components. The first and second sensors are each connected to the processor to sense vibrations within the fluid container and to generate and send corresponding vibration signals to the processor. The processor can determine a horizontal vibration mode from the vibration signals of the first and second sensors and the input signal, to determine a modal frequency of the determined horizontal vibration mode, and to determine a current filling level of the fluid container based on the modal frequency of the determined horizontal vibration mode.

IPC Classes  ?

  • F17C 13/02 - Special adaptations of indicating, measuring, or monitoring equipment
  • G01F 23/2965 - Measuring attenuation of transmitted waves
  • G01F 23/80 - Arrangements for signal processing

3.

FIRE ALERT SIGNAL MANAGEMENT METHOD AND FIRE ALERT SIGNAL DETECTION AND MANAGEMENT SYSTEM ENABLING IMPLEMENTATION OF SAID METHOD

      
Application Number 19227660
Status Pending
Filing Date 2025-06-04
First Publication Date 2025-12-11
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Clavel, Thierry
  • Cote, Stéphane
  • Pugliese, Stéphane
  • Gris, Christine
  • Abbas, Stephane
  • Hermeline, Agnès

Abstract

A method of managing fire alert signals coming from at least one fire detector configured to generate at least one fire alert signal if overheating is detected, a fault signal being generated if the fire detector is malfunctioning. The management method includes a step of determining a transitory time between the end of the fire alert signal and the start of the fault signal, and a step of emitting an alert signal if the transitory time is less than or equal to an alert threshold time. This solution enables reliable determination if the end of the fire alert signal is the result of extinction of the fire or malfunctioning of the fire detector. A system for executing the method is also provided.

IPC Classes  ?

  • G08B 29/04 - Monitoring of the detection circuits
  • G08B 7/06 - Signalling systems according to more than one of groups Personal calling systems according to more than one of groups using electric transmission

4.

ACOUSTIC ATTENUATION PANEL COMPRISING AT LEAST ONE C-SHAPED REINFORCEMENT HELD BY AT LEAST ONE EXPANDABLE CORE AND METHOD FOR MANUFACTURING SUCH A PANEL

      
Application Number 19231682
Status Pending
Filing Date 2025-06-09
First Publication Date 2025-12-11
Owner Airbus SAS (France)
Inventor
  • Ravise, Florian
  • Metayer, Arnaud
  • Dousset, Julien
  • Couvet, Marc
  • Menay, Hassan

Abstract

An acoustic attenuation panel with at least one acoustically resistive layer, at least one reflective layer, at least one cellular structure and at least one C-shaped reinforcement which are interposed between the acoustically resistive and reflective layers, and at least one expandable core, positioned between the first and second wings of the C-shaped reinforcement, which increases in volume during a polymerization cycle. Also a method for manufacturing such a panel.

IPC Classes  ?

  • G10K 11/168 - Plural layers of different materials, e.g. sandwiches
  • B29D 24/00 - Producing articles with hollow walls
  • B32B 3/08 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
  • B32B 3/12 - Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shapeLayered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. apertured or formed of separate pieces of material characterised by a layer of regularly-arranged cells whether integral or formed individually or by conjunction of separate strips, e.g. honeycomb structure

5.

DETECTION MODULE, DETECTION DEVICE, DETECTION SYSTEM, AND DETECTION METHOD

      
Application Number 19205617
Status Pending
Filing Date 2025-05-12
First Publication Date 2025-11-27
Owner AIRBUS (S.A.S.) (France)
Inventor Huang, Jinming

Abstract

Disclosed are a detection module, a detection device, a detection system, and a detection method. The detection module includes a scanning unit configured to perform 3D scanning on a detected surface and having a laser projecting device including a laser source and at least two MEMS micro scanning mirrors configured to reflect laser emitted by the laser source onto the detected surface, and a laser receiving device configured to receive the reflected laser from the detected surface to obtain at least two laser images of the detected surface; a RGB image sensor configured to capture a RGB image of the detected surface; and a processor connected to the scanning unit and the RGB image sensor, and configured to stitch the at least two laser images, and detect a defect of the detected surface based on the stitched laser image and the RGB image.

IPC Classes  ?

  • G01N 21/88 - Investigating the presence of flaws, defects or contamination
  • H04N 23/10 - Cameras or camera modules comprising electronic image sensorsControl thereof for generating image signals from different wavelengths
  • H04N 23/56 - Cameras or camera modules comprising electronic image sensorsControl thereof provided with illuminating means
  • H04N 23/667 - Camera operation mode switching, e.g. between still and video, sport and normal or high and low resolution modes

6.

ACOUSTIC ABSORPTION STRUCTURE COMPRISING AT LEAST ONE PARTITION SYSTEM POSITIONED IN AT LEAST ONE CELL TO FORM TWO TYPES OF RESONATORS, METHOD OF MANUFACTURING SUCH A STRUCTURE

      
Application Number 19213307
Status Pending
Filing Date 2025-05-20
First Publication Date 2025-11-27
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Albet, Gregory
  • Le Clainche, Stéphane
  • Przybyla, Benoit
  • Teigne, Manuel

Abstract

An acoustic absorption structure including a cellular structure that includes at least one cell delimited by at least one wall and at least one partition system. The system includes at least one subsystem positioned in the cell and adapted to divide it into at least two cavities and at least one tongue connected to the subsystem and having a hook shape straddling one of the first and second edges of the wall. The tongue facilitates installing and retaining each partition system in the cell.

IPC Classes  ?

  • B64C 1/40 - Sound or heat insulation
  • B64F 5/10 - Manufacturing or assembling aircraft, e.g. jigs therefor

7.

FIBER COMPOSITE MATERIAL, A METHOD OF MANUFACTURING A COMPOSITE STRUCTURE AND COMPOSITE STRUCTURE

      
Application Number 19199619
Status Pending
Filing Date 2025-05-06
First Publication Date 2025-11-20
Owner Airbus (S.A.S.) (France)
Inventor
  • Bautz, Brian
  • Beier, Uwe
  • Hübner, Fabian
  • Meer, Thomas

Abstract

A fiber composite material containing at least one layer of reinforcing fibers embedded in a polymer matrix, with the polymer matrix being formed by a curable resin and including at least one first region having a first curing property of the resin and at least one second region having a second curing property of the resin, wherein the at least one first curing property is different from the at least one second curing property, a method of manufacturing a composite structure, and a composite structure manufactured in the method.

IPC Classes  ?

  • B29C 70/54 - Component parts, details or accessoriesAuxiliary operations
  • B29K 307/04 - Carbon
  • B29L 31/00 - Other particular articles
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials

8.

AUTOMATIC AIRCRAFT TAXI SYSTEMS AND METHODS

      
Application Number 19211889
Status Pending
Filing Date 2025-05-19
First Publication Date 2025-11-20
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Laurens, Pascal
  • Bizet, Pierre
  • Perrin, Fabien
  • Rigaud, Jonathan
  • Servoles, Sebastien
  • Lacouture, Guillaume

Abstract

An automated taxi system for an aircraft includes a mapping module configured to generate a collaborative map that identifies traffic within the airport environment, a path trajectory module configured to receive digital taxi clearance from an Air Traffic Control (ATC) identifying a destination within the airport environment, such as a designated take-off runway, and to generate a taxi path trajectory to the destination, a guidance module configured to compute guidance instructions based on the taxi path trajectory, and an aircraft protection module configured to identify obstacles or incursion risks on the collaborative map in the taxi path trajectory and to modify the guidance instructions to avoid the obstacles or incursion risks.

IPC Classes  ?

  • G08G 5/51 - Navigation or guidance aids for control when on the ground, e.g. taxiing or rolling
  • B64F 1/18 - Visual or acoustic landing aids

9.

AIRBUS ATLANTIC CADREAN

      
Application Number 1887160
Status Registered
Filing Date 2025-05-14
Registration Date 2025-05-14
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 37 - Construction and mining; installation and repair services
  • 39 - Transport, packaging, storage and travel services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Apparatus for locomotion by air, water and rail; aeronautical apparatus, machines and devices; airplanes; structural accessories, parts and components for airplanes; structural accessories, parts and components for aircraft; Unmanned aerial vehicles [UAV]; structural accessories, parts and components for unmanned aerial vehicles; drones; structural accessories, parts and components for drones. Repair, maintenance and overhaul in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; dismantling in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; repair, maintenance and overhaul of machines in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; dismantling machines in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; installation services for machines, in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; providing information in relation to repair, maintenance and overhaul in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; technical support and technical assistance in the field of aviation, namely concerning the repair, maintenance, overhaul, servicing, reconditioning of airplanes, aircrafts, unmanned aerial vehicles and drones. Air transport; warehousing and storage of parts, components, accessories and connectors for airplanes, aircrafts, unmanned aerial vehicles and drones; freighting; airplane rental; aircraft rental; rental of unmanned aerial vehicles; rental of drones; rental of aircraft and aerial vehicles; transport by airplane, aircraft, unmanned aerial vehicle and drone. Scientific services, research services and technological services in relation to the following fields: aviation; industrial analysis in relation to the following fields: aviation; design and development services in relation to the following fields: aviation; conducting technical project studies, in relation to the following fields: aviation; technological advice in relation to the following fields: aviation; industrial design, in relation to the following fields: aviation; interior furnishing design services in the field of aviation; interior design, in the following fields: aviation; graphic design, in the following fields: aviation; certification and re-certification with respect to industry standards and aircraft quality; technical flight testing; providing scientific, technical and technological support center services, in relation to the following fields: aviation; testing services for airplanes, aircrafts, unmanned aerial vehicles and drones, in particular safety testing; technical support in the field of avionics for airplanes, aircrafts, unmanned aerial vehicles and drones; engineering solutions for the modification of airplanes, aircrafts, unmanned aerial vehicles and drones.

10.

MULTIFUNCTIONAL VITRIMER COMPOSITES

      
Application Number 19210081
Status Pending
Filing Date 2025-05-16
First Publication Date 2025-11-20
Owner Airbus (S.A.S.) (France)
Inventor
  • Beier, Uwe
  • Metzner, Christian
  • Zimmermann, Kristian
  • Hübner, Fabian
  • Kempf, Manuel
  • Gallardo, Santiago Aranda
  • Meer, Thomas

Abstract

A semi-finished product including at least one vitrimer, a method of joining using the semi-finished product with a sub-component, a component produced by the method, and a method of debonding such component.

IPC Classes  ?

  • B32B 38/10 - Removing layers, or parts of layers, mechanically or chemically
  • B32B 27/08 - Layered products essentially comprising synthetic resin as the main or only constituent of a layer next to another layer of a specific substance of synthetic resin of a different kind
  • B32B 27/38 - Layered products essentially comprising synthetic resin comprising epoxy resins
  • B32B 43/00 - Operations specially adapted for layered products and not otherwise provided for, e.g. repairingApparatus therefor

11.

SYSTEMS AND METHOD FOR PROVIDING A COLLABORATIVE MAP FOR AN AIRCRAFT

      
Application Number 19211824
Status Pending
Filing Date 2025-05-19
First Publication Date 2025-11-20
Owner Airbus (S.A.S.) (France)
Inventor
  • Bizet, Pierre
  • Rigaud, Jonathan
  • Servoles, Sebastien
  • Luce-Vayrac, Pierre
  • Lagarrigue, Alain
  • Gianni, Frederick

Abstract

A communication system is disclosed herein and includes aircraft equipment and on-ground equipment and uses a collaborative map, which has a graphic user interface that includes digital layers that each display a different interface view, and a digital assistant to optimize missions of the aircraft on ground and in flight. A first instance of the collaborative map and a first instance of the digital assistant are onboard the aircraft for one or more pilots to view and interact with. At least one second instance of the collaborative map and a second instance of the digital assistant are on-ground for one or more operators to view and interact with. Communications are managed to ensure synchronization of the instances of the collaborative map and the instances of the digital assistant.

IPC Classes  ?

  • G08G 5/23 - Details of user output interfaces, e.g. information presented
  • G08G 5/21 - Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
  • G08G 5/265 - Transmission of traffic-related information between aircraft and ground stations for managing air traffic control [ATC] clearance
  • G08G 5/34 - Flight plan management for flight plan modification
  • G08G 5/51 - Navigation or guidance aids for control when on the ground, e.g. taxiing or rolling
  • G08G 5/59 - Navigation or guidance aids in accordance with predefined flight zones, e.g. to avoid prohibited zones
  • G08G 5/76 - Arrangements for monitoring traffic-related situations or conditions for monitoring atmospheric conditions

12.

HUMAN-MACHINE INTERFACE FOR ANTI-INCURSION SYSTEMS AND METHODS

      
Application Number 19211860
Status Pending
Filing Date 2025-05-19
First Publication Date 2025-11-20
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Mazoin, Benjamin
  • Fersing, Laura
  • Bizet, Pierre
  • Rigaud, Jonathan

Abstract

Systems and methods for managing an anti-incursion function of an aircraft taxiing within an airport environment can be implemented by a monitoring equipment embedded in the aircraft. A human-machine interface of the monitoring equipment can be configured to display a guidance tile that presents context-dependent information as the aircraft taxies within the airport environment. In this way, the pilot of the aircraft can be first warned to ensure that the incursion-risk area (such as a runway) is cleared before operating the aircraft to enter into the incursion-risk area, and if the pilot fails to timely make steps to confirm clearance of the incursion-risk area, then the monitoring equipment can trigger automatic braking so as to stop the aircraft, thus preventing the aircraft from unsafely entering the incursion-risk area.

IPC Classes  ?

  • G08G 5/80 - Anti-collision systems
  • G08G 5/21 - Arrangements for acquiring, generating, sharing or displaying traffic information located onboard the aircraft
  • G08G 5/23 - Details of user output interfaces, e.g. information presented
  • G08G 5/265 - Transmission of traffic-related information between aircraft and ground stations for managing air traffic control [ATC] clearance
  • G08G 5/51 - Navigation or guidance aids for control when on the ground, e.g. taxiing or rolling

13.

SYSTEMS AND METHODS FOR SMART TRAJECTORY PROTECTION

      
Application Number 19211920
Status Pending
Filing Date 2025-05-19
First Publication Date 2025-11-20
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Laurens, Pascal
  • Bizet, Pierre
  • Rigaud, Jonathan
  • Servoles, Sebastien
  • Faure, Louise
  • Nicolas, Dorothee
  • Brunot, Mathieu

Abstract

An automated aircraft taxi system for an aircraft taxiing within an airport environment implements a collision-avoidance function. The collision-avoidance function triggers revision of guidance instructions and or alerts the pilots of the aircraft when a predicted trajectory of moving objects intersects a taxi path trajectory of the aircraft. The collision-avoidance function disregards an identified object that is moving on a taxiway in the airport environment when a predicted trajectory of the identified object does not intersect the taxi path trajectory of the aircraft according to the location of the identified object and the layout of taxiways on the airport map.

IPC Classes  ?

  • G08G 5/51 - Navigation or guidance aids for control when on the ground, e.g. taxiing or rolling
  • B64F 1/18 - Visual or acoustic landing aids
  • G08G 5/72 - Arrangements for monitoring traffic-related situations or conditions for monitoring traffic

14.

AIRBUS UPNEXT FLIGHTMIND

      
Application Number 019277275
Status Pending
Filing Date 2025-11-17
Owner Airbus S.A.S. (France)
NICE Classes  ? 42 - Scientific, technological and industrial services, research and design

Goods & Services

Scientific and industrial research; Technological research; Industrial analysis and research; Scientific and technological services and research and design relating thereto; Engineering services; Engineering research; Engineering design and consultancy; Estimations in the field of technology provided by engineers; Architectural design; Conducting industrial tests, Conducting industrial experiments; Virtual testing of new product designs using computer simulations; Technological project studies; Technological analysis services; Design and development services in the field of aviation; Design of prototypes; Design of vehicles; Design of computer-simulated models; Design and development of navigation systems; Testing, analysis and monitoring of navigation signals; Technological research, Relating to target recognition.

15.

CIRCUIT BREAKER WITH A PASSIVE CLAMPING CIRCUIT INCLUDING CAPACITORS, OPERATION METHOD, DC NETWORK AND AIRCRAFT

      
Application Number 19195962
Status Pending
Filing Date 2025-05-01
First Publication Date 2025-11-06
Owner Airbus SAS (France)
Inventor
  • Kapaun, Florian
  • Steiner, Gerhard
  • Witti, Michael

Abstract

A circuit breaker having a main switching unit configured to be switched off in the event of a fault, and a passive clamping circuit for absorbing energy and protecting against overvoltage wherein the clamping circuit is connected in parallel to the main switching unit. The clamping circuit includes a plurality of passive transient suppression components and delaying components arranged and configured to shift the action of the passive transient compression components so that the passive transient suppression components respond sequentially rather than simultaneously.

IPC Classes  ?

  • H02H 3/20 - Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition, with or without subsequent reconnection responsive to excess voltage
  • B64D 47/00 - Equipment not otherwise provided for
  • H02H 9/00 - Emergency protective circuit arrangements for limiting excess current or voltage without disconnection

16.

AIRBUS UPNEXT SPARKHAVEN

      
Application Number 019271321
Status Pending
Filing Date 2025-11-05
Owner Airbus S.A.S. (France)
NICE Classes  ? 42 - Scientific, technological and industrial services, research and design

Goods & Services

Scientific and industrial research; Technological research; Aeronautical research; Scientific and technological services and research and design relating thereto; testing and research services in the field of electricity; Research in the field of extra high voltage technology; Electrical safety research; Engineering services; Engineering research; Engineering design and consultancy; Conducting industrial tests, Conducting industrial experiments; Testing services, in the field of aviation; Testing services in the field of electricity; scientific feasibility studies; Technical feasibility studies; Industrial analysis and research, in the field of aviation; Development of energy and power management systems; Technological project studies; Technological analysis services; Design and development services; Design of prototypes; Design of vehicles.

17.

HIGH-PRESSURE HYDROGEN DISTRIBUTION SYSTEM FOR AN AIRCRAFT WITH A TANK STORING SUPERCRITICAL HYDROGEN

      
Application Number 19175777
Status Pending
Filing Date 2025-04-10
First Publication Date 2025-10-30
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Raveneau, Guillaume
  • Landolt, Jonathan

Abstract

A system for supplying hydrogen to hydrogen consumer on an aircraft with a tank storing supercritical hydrogen. Energy is added to the tank to ensure tank pressure maintains supercritical. The system includes a supply pipe fluidly connected between the tank and the hydrogen consumer; a primary heat exchanger arranged on the supply pipe and configured to heat the hydrogen flowing in the supply pipe from the tank to the hydrogen consumer; and a tank heater arranged in the tank and configured to heat the hydrogen in the tank.

IPC Classes  ?

  • F17C 7/00 - Methods or apparatus for discharging liquefied, solidified, or compressed gases from pressure vessels, not covered by another subclass
  • B64D 37/02 - Tanks
  • B64D 37/30 - Fuel systems for specific fuels

18.

FRICTION STIR WELDING METHOD AND DEVICE, AS WELL AS WORKPIECE COMPRISING A BUTT WELD SEAM

      
Application Number 19259880
Status Pending
Filing Date 2025-07-03
First Publication Date 2025-10-30
Owner
  • Airbus Operations GmbH (Germany)
  • AIRBUS (S.A.S) (France)
Inventor
  • Linde, Peter
  • Lenczowski, Blanka

Abstract

A welding device (70) includes a probe assembly (90) including at least a first and second probe device (100a, 100b). A first and second part (31a, 31b) to be joined along the weld line (40) are provided, wherein the parts are each formed as a laminate (1; 1′) including at least a first layer (2a, 2b) formed with a first material and a second layer (5a, 5b) formed with a second material. The first and second materials have different material properties. The method friction stir welds of the parts using the welding device, wherein simultaneously the first probe device acts on the first layers and the second probe device acts on the second layers.

IPC Classes  ?

  • B23K 20/12 - Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating the heat being generated by frictionFriction welding
  • B23K 11/00 - Resistance weldingSevering by resistance heating
  • B23K 101/00 - Articles made by soldering, welding or cutting

19.

SYSTEM AND METHOD FOR MANAGING AN ENERGY SOURCE IN A HYBRID ELECTRIC PROPULSION ARCHITECTURE

      
Application Number 19192594
Status Pending
Filing Date 2025-04-29
First Publication Date 2025-10-30
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Kornstaedt, Lars
  • Kahalerras, Mohamed Khaled
  • Antonio, Gilian
  • Drissi El Bouzaidi, Israe
  • Perrotte, Lancelot
  • Basset, Olivier

Abstract

An aircraft with an energy management system for an electrical energy source in a hybrid electric propulsion architecture with at least one heat engine, an avionics system and components conveying parameters of the aircraft. An energy management module stores functions available for a given mission of the aircraft that are likely to be used by the engine and allowing assistance from the source, as well as the necessary associated charge required for the execution thereof. A controller is provided for authorizing their execution and ensuring the execution of the safety functions, the controller being linked to the components, to the electrical energy source and to an engine activation module in order to send it the authorized functions according to the control that has been completed.

IPC Classes  ?

  • B64D 31/18 - Power plant control systemsArrangement of power plant control systems in aircraft for electric power plants for hybrid-electric power plants
  • B64D 27/33 - Hybrid electric aircraft

20.

METHOD AND SYSTEM FOR PROVIDING COOLING TO THE HOLD OF AN AIRCRAFT

      
Application Number 19194295
Status Pending
Filing Date 2025-04-30
First Publication Date 2025-10-30
Owner
  • Airbus Operations GmbH (Germany)
  • Airbus (S.A.S.) (France)
Inventor
  • Langediers, Jürgen
  • Hadamek, Rainer
  • Thomas, Jan
  • Klockgether, Jörg

Abstract

A method for providing cooling to cargo in the hold of an aircraft includes providing a temperature-reactive cargo item in the hold of an aircraft, providing an alert condition associated with the temperature-reactive cargo item corresponding to a need to cool the temperature-reactive cargo item in the aircraft hold, identifying via a sensor arrangement the alert condition within the aircraft hold, and cooling the aircraft hold after identification of the alert condition.

IPC Classes  ?

  • B64D 13/06 - Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
  • A62C 3/06 - Fire prevention, containment or extinguishing specially adapted for particular objects or places of highly inflammable material, e.g. light metals, petroleum products
  • A62C 3/08 - Fire prevention, containment or extinguishing specially adapted for particular objects or places in vehicles, e.g. in road vehicles in aircraft
  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for

21.

TAPE STRUCTURE FOR USE IN AN AUTOMATED FIBER PLACEMENT (AFP) METHOD, AUTOMATED FIBER PLACEMENT DEVICE AND AUTOMATED FIBER PLACEMENT (AFP) METHOD

      
Application Number 19176574
Status Pending
Filing Date 2025-04-11
First Publication Date 2025-10-23
Owner
  • Airbus Operations GmbH (Germany)
  • Airbus (S.A.S.) (France)
Inventor
  • Wolf, Johannes
  • Kolbe, Andreas
  • Hübner, Fabian
  • Beier, Uwe

Abstract

A tape structure for use in automated fiber placement method to manufacture a composite structure includes a first layer and a second layer connected to the first layer with the first layer being configured as a support layer and the second layer being configured as a pre-impregnated layer, wherein the first layer is removable from the second layer during or after placement of the second layer on the composite structure to be manufactured, an automated fiber placement device an automated fiber placement method and a composite structure manufactured in the method.

IPC Classes  ?

  • B29C 70/38 - Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
  • B29K 105/08 - Condition, form or state of moulded material containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
  • B29K 307/04 - Carbon
  • B29L 31/00 - Other particular articles

22.

COMPUTER-IMPLEMENTED METHOD FOR NETWORK-ASSISTED DATA TRANSPORT

      
Application Number 19098361
Status Pending
Filing Date 2025-04-02
First Publication Date 2025-10-16
Owner Airbus SAS (France)
Inventor Milheiro Mendes, Paulo Jorge

Abstract

A computer-implemented method for transporting data between an end-user device and a server device for providing a network service via a time-varying network, the time-varying network including a plurality of nodes that are interconnected intermittently in time. Also, a network arrangement, a gateway device, a computer program, and a computer-readable data carrier for carrying out the method.

IPC Classes  ?

23.

DISTRIBUTED COOPERATIVE CACHE MANAGEMENT IN INFORMATION CENTRIC NETWORKS

      
Application Number 19098379
Status Pending
Filing Date 2025-04-02
First Publication Date 2025-10-16
Owner Airbus SAS (France)
Inventor Milheiro Mendes, Paulo Jorge

Abstract

A computer-implemented method for transmitting data in an information-centric network, the information-centric network being connectable to a plurality of server devices for providing network service data, respectively, the information-centric network being configured for receiving a request for network service data from a client device, wherein the information-centric network includes a plurality of interconnected nodes including, respectively, a cache for caching network service data, each of the nodes being configured for routing any request to another of the nodes along a corresponding routing path from the client device to the corresponding server device, the corresponding routing path having one or more nodes successively visitable by the request via one hop.

IPC Classes  ?

  • H04L 45/122 - Shortest path evaluation by minimising distances, e.g. by selecting a route with minimum of number of hops
  • H04L 45/74 - Address processing for routing

24.

CRITICAL FLYTECH

      
Application Number 019259081
Status Pending
Filing Date 2025-10-10
Owner Airbus S.A.S. (France)
NICE Classes  ? 42 - Scientific, technological and industrial services, research and design

Goods & Services

Engineering services; Technological research; Scientific technological services, in relation to software; Research and consultancy relating to computer software; industrial analisys; industry research; Industrial design; Development (design) of software, Installation of computer software, Maintenance of computer software, Updating of computer software and Rental of computer software; Computer specification design; Integration of computer software; Providing temporary use of on-line non-downloadable software development tools; Development of computer platforms; Software as a service [SaaS]; Platform as a service [PaaS]; Data security services; AI as a Service (AIaaS); Platforms for artificial intelligence being software as a service [SaaS]; Testing, authentication and quality control; Product certification services.

25.

AIRBUS UPNEXT VOLTIFY

      
Application Number 019259327
Status Pending
Filing Date 2025-10-10
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electrical and electronic apparatus and instruments for air vehicles, namely Electrical and electronic components for aircraft; Electrical and electronic security apparatus and instruments for aircraft; Electrical and electronic communications apparatus and instruments for aircraft; Electrical and electronic apparatus and instruments for monitoring aircraft; Navigation apparatus and instruments, For use with the following goods: Air vehicles; Measuring apparatus and instruments, For use with the following goods: Air vehicles; Apparatus and instruments for use in the control and surveillance of aerial vehicles; Flight simulators; Computer hardware and computer peripheral devices for providing of training and games; computer software for use in the field of aviation; Design, development, control, navigation, maintenance software In the field of aircraft; Teaching apparatus and instruments; Flight simulation software; Training software; Software programs for video games; Game software. Vehicles; apparatus for transport and locomotion by land, air, water and rail; Air vehicles; Aircraft; Pilotless aircraft; Space vehicles; Helicopters; Drones; Parts, components and elements of aircraft. Engineering services; Engineering research; Engineering design and consultancy; Testing services, in the field of aviation; Conducting industrial tests, Conducting industrial experiments; Scientific research, Industrial research, in the field of aviation; scientific feasibility studies; Technical feasibility studies; Technological research, in the field of aviation; Aeronautical research; industrial analisys, Industrial research, in the field of aviation; testing and research services in the field of electricity; Design and development services in the field of aviation; Design of prototypes; Design of vehicles.

26.

MONITORING A COOLANT FLOW OF A POWER ELECTRONIC SEMICONDUCTOR DEVICE

      
Application Number 19171696
Status Pending
Filing Date 2025-04-07
First Publication Date 2025-10-09
Owner Airbus (S.A.S.) (France)
Inventor
  • Steiner, Gerhard
  • Kapaun, Florian

Abstract

A method for monitoring a cooling system for power electronics, especially on aircraft. For improving monitoring of a cooling system of a power electronic semiconductor device, wherein the cooling system can generate a coolant flow along a coolant flow path over at least one semiconductor power module of the power electronic semiconductor device, the method includes providing several temperature sensors arranged along the coolant flow path, measuring temperatures at different locations of the coolant flow path by the temperature sensors, comparing an actual temperature difference between the temperatures measured with an expected temperature difference calculated on basis of losses of the at least one semiconductor power module and on basis of nominal coolant flow conditions, and determining the status of the coolant flow on basis of the comparison.

IPC Classes  ?

  • G01M 99/00 - Subject matter not provided for in other groups of this subclass
  • G01K 3/14 - Thermometers giving results other than momentary value of temperature giving differences of valuesThermometers giving results other than momentary value of temperature giving differentiated values in respect of space
  • H01L 23/34 - Arrangements for cooling, heating, ventilating or temperature compensation

27.

AIRBUS FLY INK

      
Application Number 019256806
Status Pending
Filing Date 2025-10-06
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 02 - Paints, varnishes, lacquers
  • 37 - Construction and mining; installation and repair services
  • 40 - Treatment of materials; recycling, air and water treatment,

Goods & Services

Paints; Varnishes; Lacquers; Primers; Coatings; paints for vehicles; Dyes, colorants, pigments and inks; Printing ink; Printing pigments; Printing ink lacquers; Anti-corrosive coatings [paints]; Preparations for undercoating the exposed surfaces of motor vehicles; Preparations for the treatment of metal surfaces to resist tarnishing; Preparations for use as waterproofing coatings on the surfaces of structures [paints]; Protective coatings in the form of sprays for use on metals [paints]. Painting; Decorative painting services; Painting of aircraft; painting of vehicles; Spray painting; Consultancy relating to vehicle painting; Cleaning by means of sanding (Services for -); Buffing and polishing; Repair, maintenance, servicing, disassembly, refurbishment, cleaning and coating of vehicles and parts therefor; Vehicle undercoating services; Inspection of aircraft and parts thereof prior to maintenance and repair; Repair and finishing of air vehicle bodies for others. Inkjet printing services; Printing; Digital printing; Digital printing services; Direct printing on mould.

28.

TRAINING MACHINE LEARNING MODEL WITH PERIPHERAL IGNORE MASK

      
Application Number 19091357
Status Pending
Filing Date 2025-03-26
First Publication Date 2025-10-02
Owner Airbus (S.A.S.) (France)
Inventor Chandrashekar, Puneeth Bilagunda

Abstract

A method of training a machine learning model to identify image features including providing training image data including pixels, assigning a groundtruth annotation to each pixel relating to a respective pixel and each groundtruth annotation indicating whether or not that the pixel corresponds with an image feature, providing an ignore mask including a set of ignore flags relating to a respective pixel and each ignore flag providing an indication that the pixel should be ignored, for each pixel, receiving a prediction value from the machine learning model indicating a probability of the pixel corresponding with an image feature, for each pixel which has no ignore flag, determining a loss value based on the prediction value and groundtruth annotation for that pixel, and training the machine learning model based on the loss value, and for each pixel having an ignore flag, ignoring the prediction value for that pixel.

IPC Classes  ?

29.

COOLING OF GAS FLOWING OVER AIRCRAFT STRUCTURE

      
Application Number 19046235
Status Pending
Filing Date 2025-02-05
First Publication Date 2025-10-02
Owner AIRBUS (S.A.S.) (France)
Inventor
  • Joy, Joewin
  • Patil, Jitendra
  • Hebbar, Nihal

Abstract

An aircraft structure configured to be exposed to an ambient airflow which flows over the structure in an airflow direction. The aircraft structure includes: a first exhaust vent configured to exhaust a first stream of gas into the ambient airflow; and a second exhaust vent configured to exhaust a second stream of gas into the ambient airflow. The first exhaust vent is positioned downstream of the second exhaust vent in the airflow direction, the first exhaust vent is positioned in line with the second exhaust vent relative to the airflow direction, and the first exhaust vent has a larger area than the second exhaust vent.

IPC Classes  ?

  • B64D 15/04 - Hot gas application
  • B64D 29/00 - Power-plant nacelles, fairings or cowlings
  • B64D 33/04 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
  • F02C 7/141 - Cooling of plants of fluids in the plant of working fluid

30.

METHOD FOR COMPUTING AT LEAST ONE OUTPUT VALUE FOR A NUMBER OF INPUT VALUES BY A COMPUTING DEVICE, AS WELL AS CORRESPONDING COMPUTING DEVICE, COMPUTER PROGRAM, COMPUTER-READABLE DATA CARRIER, AND APPARATUS

      
Application Number 19070135
Status Pending
Filing Date 2025-03-04
First Publication Date 2025-09-18
Owner Airbus SAS (France)
Inventor Schertler, Klaus

Abstract

A method for computing an output value from a number of input values, a computer program, apparatus, and a vehicle, an aircraft. The method includes an input number representing a vector size of an input vector containing the input values; defining a projection number of projections as a multiple of the input number based on a multiplying number; precomputing a transformed projection tensor as a transformation of a projection tensor having a projection size of the input number multiplied by the multiplying number and containing weight values in the frequency domain; obtaining a transformed embedded input tensor by computing a transformed input vector as a transformation of the input vector into the frequency domain; embedding the transformed input vector into the transformed embedded input vector; and using the transformed projection tensor and the transformed embedded input vector for computing the output value.

IPC Classes  ?

31.

METHOD FOR OBTAINING A CASCADE OF VANES OF AN AIRCRAFT THRUST REVERSAL DEVICE FROM TUBULAR PREFORMS, CASCADE OF VANES OBTAINED USING THIS METHOD

      
Application Number 19078970
Status Pending
Filing Date 2025-03-13
First Publication Date 2025-09-18
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Chancerelle, Emeric
  • Destombes, Gautier
  • Cazalis, Julie
  • Bonnet, Sébastien

Abstract

A method for obtaining a cascade of vanes of an aircraft thrust reversal device by: manufacturing tubular preforms each having transverse and longitudinal facets that form a single piece, delimit a cell of the cascade of vanes and constitute at least one layer of the vanes, and longitudinal walls of the cascade of vanes situated around the cell; assembling the tubular preforms by connecting the transverse facets of the two tubular preforms so as to form a common vane, and/or the longitudinal facets of two tubular preforms so as to form a segment of a common longitudinal wall. Also a cascade of vanes obtained using such a method.

IPC Classes  ?

  • B29D 99/00 - Subject matter not provided for in other groups of this subclass
  • F02K 1/62 - Reversing jet main flow by blocking the rearward discharge by means of flaps

32.

AIRBUS MINDSHARE

      
Application Number 019245633
Status Pending
Filing Date 2025-09-12
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Computer software for use in real-time collaborative engagement by a group of vehicles across multiple domains and environments, especially air, land, sea, space and submarine; Computer software for single vehicle autonomy and real-time collaborative engagement with other vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed or uncrewed aircraft; Computer software for enabling communication and data exchange among vehicles, especially crewed or uncrewed aircraft; Computer software for enabling communication and data exchange among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially crewed and uncrewed aircraft; Computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Computer software for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft. Providing online non-downloadable computer software for use in real-time collaborative engagement by a group of vehicles across multiple domains and environments especially air, land, sea, space and submarine; Software as a service (SaaS) featuring software for enabling communication and data exchange among diverse vehicles for collaborative purposes; Providing computer software for use in facilitating single vehicle autonomy and real-time collaboration and information sharing among vehicles; Updating and maintenance of computer software for use in real-time collaborative engagement by a group of vehicles across multiple domains and environments, especially air, land, sea, space and submarine; Updating and maintenance of computer software for single vehicle autonomy and real-time collaborative engagement with other vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed or uncrewed aircraft; Updating and maintenance of computer software for enabling communication and data exchange among vehicles, especially crewed or uncrewed aircraft; Updating and maintenance of computer software for enabling communication and data exchange among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Updating and maintenance of computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially crewed and uncrewed aircraft; Updating and maintenance of computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Updating and maintenance of computer software for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for use in real-time collaborative engagement by a group of vehicles across multiple domains and environments, especially air, land, sea, space and submarine; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for single vehicle autonomy and real-time collaborative engagement with other vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed or uncrewed aircraft; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for enabling communication and data exchange among vehicles, especially crewed or uncrewed aircraft; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for enabling communication and data exchange among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially crewed and uncrewed aircraft; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Technical support services, namely, providing troubleshooting in the nature of diagnosing problems with computer software for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Licensing of computer software for use in real-time collaborative engagement by a group of vehicles across multiple domains and environments, especially air, land, sea, space and submarine; Licensing of computer software for single vehicle autonomy and real-time collaborative engagement with other vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed or uncrewed aircraft; Licensing of computer software for enabling communication and data exchange among vehicles, especially crewed or uncrewed aircraft; Licensing of computer software for enabling communication and data exchange among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Licensing of computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially crewed and uncrewed aircraft; Licensing of computer software for use in facilitating real-time collaboration and information sharing among vehicles, especially for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft; Licensing of computer software for planning, enhancement and execution of missions for vehicles, especially crewed and uncrewed aircraft.

33.

ENCODING METHOD AND DECODING METHOD FOR A MULTIPLE LINK COMMUNICATION NETWORK AND ASSOCIATED DEVICES

      
Application Number 19041107
Status Pending
Filing Date 2025-01-30
First Publication Date 2025-09-04
Owner Airbus (S.A.S.) (France)
Inventor Klügel, Markus

Abstract

A computer-implemented encoding method for encoding an input data stream for transmission from a transmitter coding point using a plurality of data links to improve communication networks. After segmenting the input data stream into data symbols, a link set of transmission data links is randomly selected from all data links. The data symbols are encoded by network coding. The encoded data symbol is packetized into a data packet together with decoding information and the randomly selected data links. The data packets are sent each along one randomly selected data link.

IPC Classes  ?

  • H04L 1/1812 - Hybrid protocolsHybrid automatic repeat request [HARQ]
  • H04W 76/15 - Setup of multiple wireless link connections

34.

WIRELESS NETWORK INFRASTRUCTURE, AIRCRAFT AND METHOD FOR WIRELESS COMMUNICATION ONBOARD AN AIRCRAFT

      
Application Number 19065435
Status Pending
Filing Date 2025-02-27
First Publication Date 2025-09-04
Owner
  • Airbus Operations GmbH (Germany)
  • Airbus S.A.S. (France)
Inventor
  • Mueller, Jan
  • Meyerhoff, Thomas
  • Krueger, Leo
  • Yin, Chunjiang
  • Schwark, Uwe

Abstract

A wireless network infrastructure for an aircraft includes a first communication unit to receive and transmit data signals from and to a control system in a secured domain of the aircraft, the first communication unit configured as a first network node of a wireless communication network, second communication units of corresponding aircraft devices in an unsecured domain of the aircraft and configured as second network nodes of the wireless communication network. The aircraft devices are operable by control signals sent from the control system to the aircraft devices and transmit control signals to the control system over the wireless communication network, each aircraft device having a communication unit further comprising additional control dissimilar from the control signals sent over the wireless communication network for operating the aircraft device independently. Also provided are an aircraft including the wireless network infrastructure and a method for wireless communication onboard an aircraft.

IPC Classes  ?

35.

RING-SHAPED SOLID OXIDE FUEL CELL ASSEMBLY FOR AN AIRCRAFT ENGINE

      
Application Number 19062396
Status Pending
Filing Date 2025-02-25
First Publication Date 2025-08-28
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Ahilan, Vignesh
  • Kierbel, Daniel
  • Roux, Paul-Emile

Abstract

A ring-shaped solid oxide fuel cell assembly, for an aircraft engine, with a ring-shaped inner manifold, a ring-shaped outer manifold arranged coaxially around the inner manifold, wherein one of the manifolds comprises a hydrogen inlet and the other comprise a hydrogen outlet, a plurality of tubular solid oxide fuel cells arranged radially between the manifolds, wherein each fuel cell comprises an anode formed as an inner tube, an inner end fluidly connected to the inner manifold and an outer end fluidly connected to the outer manifold, a cathode formed as an outer porous tube around the anode, and, between, the anode and the cathode, an electrolyte. For each fuel cell, an inner electrical contact electrically connects at the inner end of that fuel cell to the anode or the cathode, and an outer electrical contact electrically connects at the outer end to the other.

IPC Classes  ?

  • H01M 8/243 - Grouping of unit cells of tubular or cylindrical configuration
  • H01M 8/00 - Fuel cellsManufacture thereof
  • H01M 8/12 - Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte
  • H01M 8/1246 - Fuel cells with solid electrolytes operating at high temperature, e.g. with stabilised ZrO2 electrolyte characterised by the process of manufacturing or by the material of the electrolyte the electrolyte consisting of oxides
  • H01M 8/2485 - Arrangements for sealing external manifoldsArrangements for mounting external manifolds around a stack

36.

METHOD, CONTROL UNIT AND COMMUNICATION SYSTEM FOR PROVIDING A DATA CONNECTION, AND VEHICLE COMPRISING SAME

      
Application Number 19048313
Status Pending
Filing Date 2025-02-07
First Publication Date 2025-08-14
Owner Airbus SAS (France)
Inventor
  • Schupke, Dominic
  • Baltaci, Aygün

Abstract

A method, a control unit, a communication system, and a vehicle for providing a data connection between a sender on an aircraft, and at least one receiver, via terrestrial transceiving module of the aircraft primarily configured to communicate with a terrestrial station and/or via non-terrestrial transceiving module of the aircraft primarily configured to communicate with at least one a non-terrestrial station, the method comprising monitoring a connection parameter of the data connection and/or an orientation parameter of the aircraft with respect to the at least one terrestrial station and/or to the at least one non-terrestrial station; comparing the connection parameter to a connection threshold value and/or the orientation parameter to an orientation threshold value. The data connection provided depends on when the comparison indicates regular conditions and when the comparison indicates irregular conditions.

IPC Classes  ?

  • G08G 5/27 - Arrangements for acquiring, generating, sharing or displaying traffic information for managing network coverage, e.g. ensuring transmission connections for UAVs
  • H04B 7/185 - Space-based or airborne stations
  • H04B 17/309 - Measuring or estimating channel quality parameters

37.

OPTICAL DETECTOR AND METHOD FOR QUANTUM COMMUNICATION

      
Application Number 19050591
Status Pending
Filing Date 2025-02-11
First Publication Date 2025-08-14
Owner Airbus SAS (France)
Inventor
  • Comin, Alberto
  • Tepper, Jan

Abstract

An optical detector for quantum communication, comprising an optical setup configured to separate a single-photon signal beam encoded by a plurality of photon states into a plurality of separated single-photon beams having mutually different photon states, and a camera comprising a plurality of detection elements arranged as a two-dimensional array forming a detection area. Each detection element is configured to resolve a single photon incident on the detection element and provide a corresponding electric signal. The camera is arranged such that the separated beams are incident on mutually different designated areas of the detection area. Each designated area comprises a plurality of detection elements. Also a method for quantum communication.

IPC Classes  ?

  • H04B 10/70 - Photonic quantum communication
  • G02B 27/28 - Optical systems or apparatus not provided for by any of the groups , for polarising
  • H04B 10/60 - Receivers

38.

STORAGE TANK FOR LIQUIFIED GAS, AIRCRAFT OR SPACECRAFT COMPRISING SUCH A STORAGE TANK, AND FIBER METAL LAMINATES

      
Application Number 18615336
Status Pending
Filing Date 2024-03-25
First Publication Date 2025-08-07
Owner
  • Airbus Operations GmbH (Germany)
  • Airbus S.A.S. (France)
Inventor
  • Linde, Peter
  • Lenczowski, Blanka

Abstract

A storage tank for liquified gas, in particular for liquid hydrogen, including a vessel having a vessel wall formed from a fiber metal laminate including metal layers formed with an aluminum alloy and one or more synthetic layers with reinforcing fibers embedded in a thermoplastic matrix. Further, an aircraft or spacecraft including such a storage tank as well as a hydrogen-based propulsion system configured to be supplied with hydrogen at least from the storage tank is disclosed. Further, fiber metal laminates are disclosed.

IPC Classes  ?

  • F17C 1/14 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of aluminiumPressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of non-magnetic steel
  • B64D 37/02 - Tanks
  • B64G 1/40 - Arrangements or adaptations of propulsion systems
  • F17C 1/16 - Pressure vessels, e.g. gas cylinder, gas tank, replaceable cartridge constructed of plastics materials

39.

METHOD FOR DETERMINING AT LEAST ONE POSITION OF A MOBILE STRUCTURE OF AN AIRCRAFT FROM ITS SPEED AND AIRCRAFT COMPRISING A DEVICE FOR EXECUTING IT

      
Application Number 19037862
Status Pending
Filing Date 2025-01-27
First Publication Date 2025-07-31
Owner Airbus SAS (France)
Inventor Cooke, Cameron

Abstract

A method of determining at a given time at least one position of a mobile structure by determining at least one speed of the mobile structure at the given time, comparing the speed determined with listed speeds each associated with a listed position, and determining the position of the mobile structure at the given time that corresponds to the listed position associated with the listed speed equal to or closest to the speed determined at the given time. Also, a device for executing the method and an aircraft including at least one such device.

IPC Classes  ?

  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for
  • G01S 13/58 - Velocity or trajectory determination systemsSense-of-movement determination systems
  • G06V 10/52 - Scale-space analysis, e.g. wavelet analysis
  • G06V 20/56 - Context or environment of the image exterior to a vehicle by using sensors mounted on the vehicle

40.

METHOD FOR DETERMINING AT LEAST ONE CHARACTERISTIC OF A MOVEMENT OF A MOBILE STRUCTURE OF AN AIRCRAFT AND AIRCRAFT COMPRISING A DEVICE FOR ITS IMPLEMENTATION

      
Application Number 19037887
Status Pending
Filing Date 2025-01-27
First Publication Date 2025-07-31
Owner
  • Airbus SAS (France)
  • Airbus Operations Limited (United Kingdom)
Inventor
  • Cooke, Cameron
  • Nwaefulu, Chioma

Abstract

A method for determining, at a given moment in time, at least one characteristic of a movement of a mobile structure of an aircraft. The method includes determining a pair of coordinates in a reference plane corresponding to a projection of a reference feature forming part of the mobile structure in the reference plane, determining the characteristic of the movement of the mobile structure by comparing the pair of coordinates previously determined with reference coordinate pairs, at least one characteristic of the movement of the mobile structure being associated with each pair of reference coordinates. Also an aircraft having a device for implementing the method.

IPC Classes  ?

  • B64D 45/00 - Aircraft indicators or protectors not otherwise provided for
  • B64C 25/10 - Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
  • G06T 7/00 - Image analysis
  • G06T 7/246 - Analysis of motion using feature-based methods, e.g. the tracking of corners or segments
  • G06T 7/73 - Determining position or orientation of objects or cameras using feature-based methods

41.

SEMANTIC ROUTING FOR TIME VARYING NETWORKS

      
Application Number 19028664
Status Pending
Filing Date 2025-01-17
First Publication Date 2025-07-24
Owner Airbus SAS (France)
Inventor Milheiro Mendes, Paulo-Jorge

Abstract

A semantic routing method for time varying networks, wherein the method is configured to provide a congestion-aware source-based routing for satellites, preferably LEO constellations, with a distributed name resolution system, comprising a multitude of routers, a multitude of border routers, and a service provider. Wherein the method comprises an announcement phase and a forwarding phase executed in a proactive mode or a reactive mode.

IPC Classes  ?

42.

TRANSPORT OF PASSENGERS WITH REDUCED MOBILITY

      
Application Number 19021670
Status Pending
Filing Date 2025-01-15
First Publication Date 2025-07-17
Owner
  • Airbus Operations GmbH (Germany)
  • Airbus SAS (France)
Inventor
  • Giesa, Hans-Gerhard
  • Meiranke, Dirk
  • Payk, Jakob
  • Martinez, Paul

Abstract

A restraining device for restraining a wheelchair in a cabin area on board of an aircraft. The device comprises a beam-like base structure being elongate in a beam extension direction, at least two floor connectors attached to the base structure and at least one restraining connector attached to the base structure. The floor connectors are spaced apart from each other in the beam extension direction. The floor connectors are configured to temporarily mount the base structure to a seat rail floor support in an aircraft cabin. The restraining connectors are configured to be temporarily connected to a structural part of the wheelchair to hold the wheelchair in place with a passenger seated therein.

IPC Classes  ?

  • A61G 3/08 - Accommodating or securing wheelchairs
  • B64D 11/06 - Arrangements or adaptations of seats

43.

AIR/PARTICLE SEPARATION DEVICE COMPRISING A ROTARY FILTER MADE OF CELLULAR MATERIAL

      
Application Number 19009300
Status Pending
Filing Date 2025-01-03
First Publication Date 2025-07-10
Owner Airbus SAS (France)
Inventor Bauer, Fabian

Abstract

An air/particle separation device which comprises a container and a rotary filter positioned in the container, between a laden-air inlet and a treated-air outlet, the container is configured to channel air laden with particles through the rotary filter, the rotary filter comprises at least one block of cellular material configured to be passed through by the laden air and to promote the separation of the particles from the laden air and the ejection of the particles from the rotary filter which migrate, by virtue of the centrifugal effect, toward the periphery of the rotary filter.

IPC Classes  ?

  • B01D 46/00 - Filters or filtering processes specially modified for separating dispersed particles from gases or vapours

44.

ASSESSMENT METHOD, PROGRAMM, COMPUTER-READABLE DATA-CARRIER, COMPUTING DEVICE, AND ARRANGEMENT FOR A COMPUTER ASSISTED SUBSTANCE ASSESSMENT

      
Application Number 18987520
Status Pending
Filing Date 2024-12-19
First Publication Date 2025-07-03
Owner Airbus SAS (France)
Inventor
  • Carré, Camille
  • Tandon, Akshat

Abstract

An assessment method, a corresponding assessment program, a computer-readable data-carrier having stored thereon the assessment program, a computing device configured to carry out the assessment program and/or comprising the computer-readable data-carrier, and an assessment arrangement for a computer assisted assessment of at least one property parameter. Generally, the method includes obtaining a molecular structure of the chemical substance; obtaining at least one reference structure of at least one reference substance having at least one reference parameter, comparing the molecular structure to the at least one reference structure; and deriving the at least one property parameter from the comparison based on the at least one reference parameter.

IPC Classes  ?

  • G16C 20/30 - Prediction of properties of chemical compounds, compositions or mixtures
  • G16C 20/70 - Machine learning, data mining or chemometrics

45.

SUPERCONDUCTING ELECTRICAL SUPPLY LINE, METHOD FOR CONTROLLING A SUPERCONDUCTING ELECTRICAL SUPPLY LINE AND AIRCRAFT COMPRISING SUCH A LINE

      
Application Number 18985158
Status Pending
Filing Date 2024-12-18
First Publication Date 2025-06-26
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Ybanez, Ludovic
  • Colle, Alexandre
  • Rouquette, Jean-François
  • Surapaneni, Ravi Kiran
  • Galla, Gowtham

Abstract

A method for controlling a superconducting electrical supply line that is carried out in a control circuit obtains a piece of information representative of a first electric current in the superconducting electrical supply line, then, when the piece of information representative of a first electric current is greater than or equal to a first predetermined threshold value, generates a current, referred to as the second current, in a superconducting coil arranged in the vicinity of the supply line, the value of the second current being determined on the basis of the piece of information representative of the first current. A control circuit is configured to implement the method. Current limiter functions are reversibly performed by initiating a quench phenomenon in the superconducting electrical supply line.

IPC Classes  ?

  • H02H 7/00 - Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions

46.

AIRBUS UNIVERSE

      
Application Number 019205845
Status Registered
Filing Date 2025-06-20
Registration Date 2025-11-14
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 38 - Telecommunications services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Communications apparatus and instruments For use with the following goods: Air vehicles; Electric and electronic regulating apparatus and instruments For use with the following goods: Air vehicles; Navigation apparatus and instruments For use with the following goods: Air vehicles; Measuring apparatus and instruments For use with the following goods: Air vehicles; Apparatus and instruments for use in the control and surveillance of aerial vehicles; Data communications apparatus and instruments; Software; Application software; Flight simulators; Computer software platforms, recorded or downloadable; data storage, management and processing software; data processing equipment and systems; Databases; Computer programs for accessing, browsing and searching online databases; Computer software for database management In the field of aircraft; Interactive computer software for computers and mobile devices providing navigational and travel information For use with the following goods: Air vehicles. Air vehicles; Aircraft; Aeroplanes; Parts, components and fittings for aerial vehicles. Telecommunication services; Data transmission; Providing access to databases; Computer communications and Internet access; Communication services by satellite; Communications via a global computer network or the internet; Provision of internet access services. Development (design) of software, Installation of computer software, Maintenance of computer software, Updating of computer software and Rental of computer software; Software as a service [SaaS]; Development of computer platforms; Platform as a service [PaaS]; Technical data analysis services; Data security services.

47.

AIRSPACE BY AIRBUS

      
Serial Number 99219027
Status Pending
Filing Date 2025-06-05
Owner AIRBUS S.A.S. (France)
NICE Classes  ?
  • 11 - Environmental control apparatus
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 20 - Furniture and decorative products

Goods & Services

Lighting installations; electric lighting fixtures; electric lighting apparatus for vehicles Aircraft; vehicle seats; headrests for vehicle seats; fitted seat covers for vehicles; overhead cargo storage bins especially adapted to fit in aircraft Furniture for aircraft; furniture being seats and couches and holders in the nature of seats and couches sold with cup holders therefor; furniture being seats and couches containing audio and video apparatus; beds; bedding except linen, namely, pillows; convertible seats, namely, furniture that converts to a bed; non-metallic trays, namely, corrugated plastic trays being commercial packaging materials, computer keyboard trays, rigid plastic trays being packaging materials, plastic trays for use when manually counting pills, and tool and tool accessory trays not made of metal sold empty and parts and fittings therefor; cabinets; footrests

48.

METHOD OF TRAINING MACHINE-LEARNING MODEL

      
Application Number 18963305
Status Pending
Filing Date 2024-11-27
First Publication Date 2025-06-05
Owner AIRBUS (S.A.S.) (France)
Inventor Chandrashekar, Puneeth Bilagunda

Abstract

A method of training a machine-learning model to identify image features is disclosed including: a. receiving a set of predicted feature regions from the machine-learning model, each predicted feature region comprising a prediction of a feature in training image data; b. generating a set of similarity coefficients, each similarity coefficient indicative of a similarity between a predicted feature region and a corresponding groundtruth region which overlaps with the predicted feature region; c. determining a loss value based on the similarity coefficients and a threshold; and d. training the machine-learning model on a basis of the loss value, wherein a.-d. are repeated, each repeat comprising a respective training epoch; in one or more of the training epochs, the set of similarity coefficients comprises one or more similarity coefficients less than the threshold, and the loss value is based on a difference between the threshold and each similarity coefficient less than the threshold.

IPC Classes  ?

  • G06V 10/82 - Arrangements for image or video recognition or understanding using pattern recognition or machine learning using neural networks
  • G06V 10/74 - Image or video pattern matchingProximity measures in feature spaces

49.

LASER SHOCK PEENING APPARATUS

      
Application Number 19052468
Status Pending
Filing Date 2025-02-13
First Publication Date 2025-06-05
Owner Airbus SAS (France)
Inventor
  • Berger, Tyler T.
  • Hilty, Devin R.
  • Bloomberg, Mark D.
  • Grossenbacher, Gary
  • Dulaney, Jeff L.

Abstract

A system for performing a laser peening application on a workpiece. A purge system is included with the system to provide a compartment housing combustion sources with compressed air so that the compartment has an increased air pressure. Also, a method of operating the system in which power is provided to the system, but only the purge system operates initially. Only after the purge system has bene operating, are the other subsystems and components of the systems, like the laser, provided with operational power.

IPC Classes  ?

  • C21D 10/00 - Modifying the physical properties by methods other than heat treatment or deformation
  • B23K 26/12 - Working by laser beam, e.g. welding, cutting or boring in a special environment or atmosphere, e.g. in an enclosure
  • B23K 26/14 - Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beamNozzles therefor
  • B23K 26/356 - Working by laser beam, e.g. welding, cutting or boring for surface treatment by shock processing

50.

MANAGING MICROBIAL CONTAMINATION OF FUEL TANK

      
Application Number 18844169
Status Pending
Filing Date 2023-03-07
First Publication Date 2025-06-05
Owner
  • Airbus Operations Limited (United Kingdom)
  • Airbus SAS (France)
Inventor
  • Fallon, Adam
  • Lee, Martin
  • Dautelle, Jean-Marie
  • Brousse, Pierre-Henri

Abstract

A computer-implemented method of determining a maintenance schedule or maintenance plan for a fuel tank of an aircraft. In a training phase, a predictive model is trained with training data. The training data is associated with fuel tanks of plural aircraft. The training data comprises environmental data indicative of an environmental parameter at locations of the plural aircraft, and test data which is indicative of a level of microbial contamination of fuel in fuel tanks of the plural aircraft. In a prediction phase, input data is received and the predictive model is operated, along with an optimisation algorithm, to determine a maintenance schedule or maintenance plan. One or more microbial contamination maintenance tasks are performed on the fuel tank based on the maintenance schedule or maintenance plan.

IPC Classes  ?

  • B64F 5/40 - Maintaining or repairing aircraft
  • B64F 5/60 - Testing or inspecting aircraft components or systems
  • G06Q 10/20 - Administration of product repair or maintenance

51.

METHOD OF TRAINING MACHINE LEARNING MODEL

      
Application Number 18963110
Status Pending
Filing Date 2024-11-27
First Publication Date 2025-06-05
Owner Airbus (S.A.S.) (France)
Inventor Chandrashekar, Puneeth Bilagunda

Abstract

A method of training a machine learning model to identify image features is disclosed including: a. providing training image data, the training image data comprising a plurality of pixels; b. assigning a groundtruth annotation to each pixel, each groundtruth annotation relates to a respective one of the pixels and each groundtruth annotation indicates whether or not that the pixel corresponds with an image feature; c. providing an ignore mask comprising a set of ignore flags; each ignore flag relates to a respective one of the pixels and each ignore flag provides an indication that the pixel should be ignored; d. receiving a prediction value from the machine learning model, each prediction value provides an indication of a probability of the pixel corresponding with an image feature; e. for each pixel which has no ignore flag, determining a loss value based on the prediction value and groundtruth annotation for that pixel.

IPC Classes  ?

  • G06V 20/70 - Labelling scene content, e.g. deriving syntactic or semantic representations
  • G06V 10/98 - Detection or correction of errors, e.g. by rescanning the pattern or by human interventionEvaluation of the quality of the acquired patterns

52.

METHOD OF TRAINING MACHINE-LEARNING MODEL

      
Application Number 18963252
Status Pending
Filing Date 2024-11-27
First Publication Date 2025-06-05
Owner AIRBUS (S.A.S.) (France)
Inventor Chandrashekar, Puneeth Bilagunda

Abstract

A method of training a machine-learning model to identify image features is disclosed including: a. providing a set of groundtruth regions, each groundtruth region comprising an annotation of a feature in training image data; b. providing a set of ignore regions; c. receiving a set of predicted feature regions from the machine-learning model, each predicted feature region comprising a prediction of a feature in the training image data; d. for each predicted feature region which overlaps with a corresponding groundtruth region, generating a similarity coefficient indicative of a similarity between the predicted feature region and the corresponding groundtruth region; e. determining a loss value based on the similarity coefficients; f. training the machine-learning model on a basis of the loss value; g. for each predicted feature region which does not overlap with any of the ignore regions and does not overlap with any of the groundtruth regions.

IPC Classes  ?

  • G06V 20/70 - Labelling scene content, e.g. deriving syntactic or semantic representations
  • G06V 10/74 - Image or video pattern matchingProximity measures in feature spaces
  • G06V 10/82 - Arrangements for image or video recognition or understanding using pattern recognition or machine learning using neural networks
  • G06V 10/98 - Detection or correction of errors, e.g. by rescanning the pattern or by human interventionEvaluation of the quality of the acquired patterns

53.

OPTICAL TERMINAL AND METHOD FOR QUANTUM COMMUNICATION

      
Application Number 18940394
Status Pending
Filing Date 2024-11-07
First Publication Date 2025-05-29
Owner Airbus SAS (France)
Inventor Comin, Alberto

Abstract

An optical terminal for quantum communication, comprising a first terminal unit configured to receive and/or transmit a first signal beam from or to a first target terminal and having a first optical axis, a second terminal unit configured to receive and/or transmit a second signal beam from and/or to a second target terminal and having a second optical axis, and a connecting part to communicate with the terminal units, wherein each terminal units comprises: a telescope provided on an optical axis to collimate the respective signal beams, a beam corrector placed on the respective optical axis and configured to correct the respective optical signals beam over a predetermined field of view of the telescope, a steering system to adjust a propagation direction of the signal beams to the respective optical axis, and a coupling portion coupling the respective signal beams to the connecting part. Also a method for quantum communication.

IPC Classes  ?

  • H04B 10/70 - Photonic quantum communication
  • G02B 26/08 - Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
  • H04B 10/50 - Transmitters

54.

MEASURES ALLOWING ACCELERATION IN THE EXECUTION OF CRYPTOGRAPHIC ALGORITHMS THAT HAVE A PRIORI INDETERMINABLE PROCESSING TIME AND APPLICATIONS THEREOF

      
Application Number 18958607
Status Pending
Filing Date 2024-11-25
First Publication Date 2025-05-29
Owner Airbus (S.A.S.) (France)
Inventor Klügel, Markus

Abstract

A method for pipelining data processing includes a data processing step taking an a priori indeterminable amount of processing time. The method involves generating a unique ID and associating it with the input data, feeding the input data and UID to a pipeline module including a data processing module and processing delay module, delaying outputting the UID by the processing delay module for a delay time corresponding to processing time required by the data processing module for a single iteration, wherein, in response to the branching part determining the condition is met or not met, the pipeline module re-inputs the UID into the processing delay module. In response to the branching part determining that the condition is another of met or not met, the processing delay module outputs the UID unblocking transmission of further input data to the processing module, and the processing module outputs processed data as output data.

IPC Classes  ?

  • H04L 9/32 - Arrangements for secret or secure communicationsNetwork security protocols including means for verifying the identity or authority of a user of the system

55.

AIRCRAFT TURNAROUND MONITORING SYSTEM

      
Application Number 18962148
Status Pending
Filing Date 2024-11-27
First Publication Date 2025-05-29
Owner
  • Airbus SAS (France)
  • Airbus Singapore Private Limited (Singapore)
Inventor
  • Shin, Yenny
  • Tan, Da Jun
  • Larasati, Larasati
  • Le Donge, Romain
  • Yon, Germain

Abstract

A monitoring system comprising multiple portable camera units may be formed by aircraft safety cones each housing a video camera for locally viewing under-wing turnaround activities of an aircraft at the stand. Each portable camera unit has a processor for relaying or processing data, images and the like captured by the unit. Data is sent wirelessly to a separate computer/or to other systems or personnel at the airport, or both.

IPC Classes  ?

  • G08G 5/06 - Traffic control systems for aircraft for control when on the ground
  • G06V 20/58 - Recognition of moving objects or obstacles, e.g. vehicles or pedestriansRecognition of traffic objects, e.g. traffic signs, traffic lights or roads

56.

A320

      
Application Number 1855108
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 14 - Precious metals and their alloys; jewelry; time-keeping instruments
  • 18 - Leather and imitations of leather
  • 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electric and electronic apparatus and instruments for air vehicles; navigation apparatus and instruments for air vehicles; measuring apparatus and instruments for air vehicles; apparatus and instruments used for control and monitoring of air vehicles; flight simulators; computer hardware and peripherals for computers for training and games; software in the field of aviation; software for design, development, control, navigation, maintenance in the field of aviation; teaching apparatus and instruments; flight simulation software; training software; software for video games; computer game software. Aircraft; parts, structural components and component parts for aircraft; airplanes; parts, structural components and component parts for airplanes. Key rings; lanyards for keys; pins (jewelry); watches. Luggage; carrier bags; umbrellas; vanity cases, not fitted; address tags for luggage. Cups; mugs; bottles. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game consoles; model vehicles (toys); educational games; electronic games. Repair, installation, maintenance and overhaul in the field of aviation; technical assistance and technical advice (repair, installation, maintenance and overhaul) in the field of aviation; advisory and information services with respect to repair, installation, maintenance and overhaul in the field of aviation. Entertainment services in the field of aviation; organization of aerial demonstrations for information and for entertainment; educational and instructional services in the field of aviation; pilot and cabin crew training; training of engineers, mechanics and technicians. Scientific, research and technological services in the field of aviation; industrial analysis in the field of aviation; testing services in the field of aviation; technological advice in the field of aerospace; engineering design in the field of aviation; software development (design), installation, maintenance, updating and rental service in the field of aviation.

57.

A321

      
Application Number 1855109
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 14 - Precious metals and their alloys; jewelry; time-keeping instruments
  • 18 - Leather and imitations of leather
  • 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electric and electronic apparatus and instruments for air vehicles; navigation apparatus and instruments for air vehicles; measuring apparatus and instruments for air vehicles; apparatus and instruments used for control and monitoring of air vehicles; flight simulators; computer hardware and peripherals for computers for training and games; software in the field of aviation; software for design, development, control, navigation, maintenance in the field of aviation; teaching apparatus and instruments; flight simulation software; training software; software for video games; computer game software. Aircraft; parts, structural components and component parts for aircraft; airplanes; parts, structural components and component parts for airplanes. Key rings; lanyards for keys; pins (jewelry); watches. Luggage; carrier bags; umbrellas; vanity cases, not fitted; address tags for luggage. Cups; mugs; bottles. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game consoles; model vehicles (toys); educational games; electronic games. Repair, installation, maintenance and overhaul in the field of aviation; technical assistance and technical advice (repair, installation, maintenance and overhaul) in the field of aviation; advisory and information services with respect to repair, installation, maintenance and overhaul in the field of aviation. Entertainment services in the field of aviation; organization of aerial demonstrations for information and for entertainment; educational and instructional services in the field of aviation; pilot and cabin crew training; training of engineers, mechanics and technicians. Scientific, research and technological services in the field of aviation; industrial analysis in the field of aviation; testing services in the field of aviation; technological advice in the field of aerospace; engineering design in the field of aviation; software development (design), installation, maintenance, updating and rental service in the field of aviation.

58.

A330

      
Application Number 1855110
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 14 - Precious metals and their alloys; jewelry; time-keeping instruments
  • 18 - Leather and imitations of leather
  • 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electric and electronic apparatus and instruments for air vehicles; navigation apparatus and instruments for air vehicles; measuring apparatus and instruments for air vehicles; apparatus and instruments used for control and monitoring of air vehicles; flight simulators; computer hardware and peripherals for computers for training and games; software in the field of aviation; software for design, development, control, navigation, maintenance in the field of aviation; teaching apparatus and instruments; flight simulation software; training software; software for video games; computer game software. Aircraft; parts, structural components and component parts for aircraft; airplanes; parts, structural components and component parts for airplanes. Key rings; lanyards for keys; pins (jewelry); watches. Luggage; carrier bags; umbrellas; vanity cases, not fitted; address tags for luggage. Cups; mugs; bottles. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game consoles; model vehicles (toys); educational games; electronic games. Repair, installation, maintenance and overhaul in the field of aviation; technical assistance and technical advice (repair, installation, maintenance and overhaul) in the field of aviation; advisory and information services with respect to repair, installation, maintenance and overhaul in the field of aviation. Entertainment services in the field of aviation; organization of aerial demonstrations for information and for entertainment; educational and instructional services in the field of aviation; pilot and cabin crew training; training of engineers, mechanics and technicians. Scientific, research and technological services in the field of aviation; industrial analysis in the field of aviation; testing services in the field of aviation; technological advice in the field of aerospace; engineering design in the field of aviation; software development (design), installation, maintenance, updating and rental service in the field of aviation.

59.

A350

      
Application Number 1855197
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 14 - Precious metals and their alloys; jewelry; time-keeping instruments
  • 18 - Leather and imitations of leather
  • 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electric and electronic apparatus and instruments for air vehicles; navigation apparatus and instruments for air vehicles; measuring apparatus and instruments for air vehicles; apparatus and instruments used for control and monitoring of air vehicles; flight simulators; computer hardware and peripherals for computers for training and games; software in the field of aviation; software for design, development, control, navigation, maintenance in the field of aviation; teaching apparatus and instruments; flight simulation software; training software; software for video games; computer game software. Aircraft; parts, structural components and component parts for aircraft; airplanes; parts, structural components and component parts for airplanes. Key rings; lanyards for keys; pins (jewelry); watches. Luggage; carrier bags; umbrellas; vanity cases, not fitted; address tags for luggage. Cups; mugs; bottles. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game consoles; model vehicles (toys); educational games; electronic games. Repair, installation, maintenance and overhaul in the field of aviation; technical assistance and technical advice (repair, installation, maintenance and overhaul) in the field of aviation; advisory and information services with respect to repair, installation, maintenance and overhaul in the field of aviation. Entertainment services in the field of aviation; organization of aerial demonstrations for information and for entertainment; educational and instructional services in the field of aviation; pilot and cabin crew training; training of engineers, mechanics and technicians. Scientific, research and technological services in the field of aviation; industrial analysis in the field of aviation; testing services in the field of aviation; technological advice in the field of aerospace; engineering design in the field of aviation; software development (design), installation, maintenance, updating and rental service in the field of aviation.

60.

A400M

      
Application Number 1855111
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 14 - Precious metals and their alloys; jewelry; time-keeping instruments
  • 18 - Leather and imitations of leather
  • 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electric and electronic apparatus and instruments for air vehicles; navigation apparatus and instruments for air vehicles; measuring apparatus and instruments for air vehicles; apparatus and instruments used for control and monitoring of air vehicles; flight simulators; computer hardware and peripherals for computers for training and games; software in the field of aviation; software for design, development, control, navigation, maintenance in the field of aviation; teaching apparatus and instruments; flight simulation software; training software; software for video games; computer game software. Aircraft; parts, structural components and component parts for aircraft; airplanes; parts, structural components and component parts for airplanes. Key rings; lanyards for keys; pins (jewelry); watches. Luggage; carrier bags; umbrellas; vanity cases, not fitted; address tags for luggage. Cups; mugs; bottles. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game consoles; model vehicles (toys); educational games; electronic games. Repair, installation, maintenance and overhaul in the field of aviation; technical assistance and technical advice (repair, installation, maintenance and overhaul) in the field of aviation; advisory and information services with respect to repair, installation, maintenance and overhaul in the field of aviation. Entertainment services in the field of aviation; organization of aerial demonstrations for information and for entertainment; educational and instructional services in the field of aviation; pilot and cabin crew training; training of engineers, mechanics and technicians. Scientific, research and technological services in the field of aviation; industrial analysis in the field of aviation; testing services in the field of aviation; technological advice in the field of aerospace; engineering design in the field of aviation; software development (design), installation, maintenance, updating and rental service in the field of aviation.

61.

STATOR SYSTEM FOR AN AXIAL FLUX MACHINE FOR AN AIRCRAFT, AS WELL AS DRIVE TRAIN AND AIRCRAFT EQUIPPED THEREWITH

      
Application Number 18940367
Status Pending
Filing Date 2024-11-07
First Publication Date 2025-05-15
Owner Airbus SAS (France)
Inventor
  • Kapaun, Florian
  • Galek, Marek

Abstract

A stator system for an axial flux machine for an aircraft, the stator system comprising a plurality of inverters and a stator including a plurality of disks wherein each disk comprises at least one dielectric substrate and at least a one conductive trace included in at least one conductive layer defined by the dielectric substrate, the at least one conductive trace forming at least a part of a winding of a at least one phase of the stator, wherein each disk is associated and connected to its own inverter.

IPC Classes  ?

  • H02K 1/18 - Means for mounting or fastening magnetic stationary parts on to, or to, the stator structures
  • H02K 1/2798 - Rotors axially facing stators the rotor consisting of two or more circumferentially positioned magnets where both axial sides of the stator face a rotor
  • H02K 11/33 - Drive circuits, e.g. power electronics
  • H02K 16/02 - Machines with one stator and two rotors

62.

AIRBUS ATLANTIC CADREAN

      
Serial Number 79437291
Status Pending
Filing Date 2025-05-14
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 37 - Construction and mining; installation and repair services
  • 39 - Transport, packaging, storage and travel services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Apparatus for locomotion by air, water and rail; aeronautical apparatus, machines and devices; airplanes; structural accessories, parts and components for airplanes; structural accessories, parts and components for aircraft; Unmanned aerial vehicles [UAV]; structural accessories, parts and components for unmanned aerial vehicles; drones; structural accessories, parts and components for drones. Repair, maintenance and overhaul in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; dismantling in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; repair, maintenance and overhaul of machines in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; dismantling machines in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; installation services for machines, in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; providing information in relation to repair, maintenance and overhaul in the field of aviation, in particular for airplanes, aircrafts, unmanned aerial vehicles and drones; technical support and technical assistance in the field of aviation, namely concerning the repair, maintenance, overhaul, servicing, reconditioning of airplanes, aircrafts, unmanned aerial vehicles and drones. Air transport; warehousing and storage of parts, components, accessories and connectors for airplanes, aircrafts, unmanned aerial vehicles and drones; freighting; airplane rental; aircraft rental; rental of unmanned aerial vehicles; rental of drones; rental of aircraft and aerial vehicles; transport by airplane, aircraft, unmanned aerial vehicle and drone. Scientific services, research services and technological services in relation to the following fields: aviation; industrial analysis in relation to the following fields: aviation; design and development services in relation to the following fields: aviation; conducting technical project studies, in relation to the following fields: aviation; technological advice in relation to the following fields: aviation; industrial design, in relation to the following fields: aviation; interior furnishing design services in the field of aviation; interior design, in the following fields: aviation; graphic design, in the following fields: aviation; certification and re-certification with respect to industry standards and aircraft quality; technical flight testing; providing scientific, technical and technological support center services, in relation to the following fields: aviation; testing services for airplanes, aircrafts, unmanned aerial vehicles and drones, in particular safety testing; technical support in the field of avionics for airplanes, aircrafts, unmanned aerial vehicles and drones; engineering solutions for the modification of airplanes, aircrafts, unmanned aerial vehicles and drones.

63.

AIRBUS ATLANTIC CADREAN

      
Application Number 243822500
Status Pending
Filing Date 2025-05-14
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 37 - Construction and mining; installation and repair services
  • 39 - Transport, packaging, storage and travel services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

(1) Appareils de locomotion par air, par eau et par rail; appareils, machines et dispositifs pour l'aéronautique; avions; accessoires, pièces et composants structurels pour avions; accessoires, pièces et composants structurels pour aéronefs; véhicules aériens sans pilote [UAV]; accessoires, pièces et composants structurels pour véhicules aériens sans pilote; drones; accessoires, pièces et composants structurels pour drones. (1) Réparation, maintenance et révision dans le domaine de l'aviation, en particulier pour avions, aéronefs, véhicules aériens sans pilote et drones; démontage dans le domaine de l'aviation, en particulier pour avions, aéronefs, véhicules aériens sans pilote et drones; réparation, maintenance et révision de machines dans le domaine de l'aviation, en particulier pour avions, aéronefs, véhicules aériens sans pilote et drones; démontage de machines dans le domaine de l'aviation, en particulier pour avions, aéronefs, véhicules aériens sans pilote et drones; services d'installation pour machines, dans le domaine de l'aviation, en particulier pour avions, aéronefs, véhicules aériens sans pilote et drones; fourniture d'informations en rapport avec la réparation, la maintenance et la révision dans le domaine de l'aviation, en particulier pour avions, aéronefs, véhicules aériens sans pilote et drones; support technique et assistance technique dans le domaine de l'aviation, à savoir concernant la réparation, la maintenance, la révision, l'entretien, le reconditionnement d'avions, aéronefs, véhicules aériens sans pilote et drones. (2) Transports aériens; entreposage et stockage de pièces, composants, accessoires et connecteurs pour avions, aéronefs, véhicules aériens sans pilote et drones; affrètement; location d'avions; location d'aéronefs; location de véhicules aériens sans pilote; location de drones; location d'aéronefs et véhicules aériens; transport en avion, aéronef, véhicule aérien sans pilote et drone. (3) Services scientifiques, services de recherche et services technologiques en rapport avec les domaines suivants: aviation; analyse industrielle en rapport avec les domaines suivants: aviation; services de conception et de développement en rapport avec les domaines suivants: aviation; conduite d'études de projets techniques, en rapport avec les domaines suivants: aviation; conseils technologiques en rapport avec les domaines suivants: aviation; dessin industriel, en rapport avec les domaines suivants: aviation; services de conception d'ameublement intérieur dans le domaine de l'aviation; décoration intérieure, dans les domaines suivants: aviation; conception graphique, dans les domaines suivants: aviation; certification et re-certification en matière de normes industrielles et de qualité des aéronefs; tests techniques de vol; fourniture de services de centres d'assistance scientifique, technique et technologique, en rapport avec les domaines suivants: aviation; services de test pour avions, aéronefs, véhicules aériens sans pilote et drones, en particulier tests de sécurité; assistance technique dans le domaine de l'avionique pour avions, aéronefs, véhicules aériens sans pilote et drones; solutions d'ingénierie pour la modification d'avions, aéronefs, véhicules aériens sans pilote et drone.

64.

A319

      
Application Number 1852853
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 09 - Scientific and electric apparatus and instruments
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services
  • 42 - Scientific, technological and industrial services, research and design

Goods & Services

Electric and electronic apparatus and instruments for air vehicles; navigation apparatus and instruments for air vehicles; measuring apparatus and instruments for air vehicles; apparatus and instruments used for control and monitoring of air vehicles; flight simulators; computer hardware and peripherals for computers for training and games; software in the field of aviation; software for design, development, control, navigation, maintenance in the field of aviation; teaching apparatus and instruments; flight simulation software; training software; software for video games; computer game software. Aircraft; parts, components, connectors and component parts for aircraft; airplanes; parts, components, connectors and component parts for airplanes. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games. Repair, installation, maintenance and overhaul in the field of aviation; technical assistance and technical advice in the field of aviation; advisory and information services with respect to repair, installation, maintenance and overhaul in the field of aviation. Entertainment services in the field of aviation; organization of aerial demonstrations for information and for entertainment; educational and instructional services in the field of aviation; pilot and cabin crew training; training of engineers, mechanics and technicians. Scientific, research and technological services in the field of aviation; industrial analysis in the field of aviation; testing services in the field of aviation; technical advice in the field of aerospace; engineering design in the field of aviation; development (design), installation, maintenance, updating and rental of software in the field of aviation.

65.

PRINTING METHOD FOR PRODUCING A PAINTED SUPPORT

      
Application Number 18926457
Status Pending
Filing Date 2024-10-25
First Publication Date 2025-05-08
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
  • Airbus Operations GmbH (Germany)
Inventor
  • Moriniere, Boris
  • Bürgy, Olivier
  • Leleu, Samuel
  • Mahler, Fabian

Abstract

A printing method comprising application of an ink on a support, pinning of the ink under UV radiation, capture of an image of the decoration and analysis of the image. In the absence of defects, the method continues with deposition of a varnish and solidification under UV radiation. In the event of a defect, the method includes erasure of the ink in a removal zone surrounding the defect, capture of a second image of the removal zone, analysis of the second image so as to determine the part of the decoration to be redone, the repair of the ink by deposition on the support so as to form the part of the decoration to be redone, and looping back to the analysis step.

IPC Classes  ?

  • B41J 29/26 - Devices, non-fluid media or methods for cancelling, correcting errors, underscoring or ruling
  • B41J 3/407 - Typewriters or selective printing or marking mechanisms characterised by the purpose for which they are constructed for marking on special material
  • B41M 7/00 - After-treatment of printed works, e.g. heating, irradiating
  • G06T 7/00 - Image analysis

66.

A310

      
Application Number 1852021
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment

Goods & Services

Aircraft; parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games.

67.

CARAVELLE

      
Application Number 1852022
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment

Goods & Services

Aircraft; parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes. Clothing; headwear; shoes; none of the aforesaid goods for or relating to maternity, postpartum or breastfeeding. Scale model vehicles and parts thereof; toys; games; the aforesaid goods excluding motor vehicles; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games.

68.

Miscellaneous Design

      
Application Number 1852023
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment

Goods & Services

Aircraft; parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games.

69.

METHOD FOR MANUFACTURING A STIFFENED PANEL MADE OF COMPOSITE MATERIAL COMPRISING A STEP OF LAYING A SKIN THEN A STEP OF LAYING PROFILES, AND TOOL FOR IMPLEMENTING SAID METHOD

      
Application Number 18911357
Status Pending
Filing Date 2024-10-10
First Publication Date 2025-05-01
Owner Airbus SAS (France)
Inventor
  • Pridie, Jago
  • Percevault, Maxime

Abstract

A method for manufacturing a stiffened panel, obtained from profiles and a skin, comprising a step of obtaining the profiles and of positioning each of the profiles on a mandrel, a step of laying the skin on a laying surface of a mold and then a step of laying the mandrels on the skin, the bases of the profiles being positioned against the skin, as well as a step of polymerizing or consolidating the profiles and the skin to obtain a stiffened panel. Also a tool for implementing such a method.

IPC Classes  ?

  • B29C 51/12 - Shaping by thermoforming, e.g. shaping sheets in matched moulds or by deep-drawingApparatus therefor of articles having inserts or reinforcements
  • B29C 51/18 - Thermoforming apparatus
  • B29C 51/30 - Moulds
  • B29C 51/42 - Heating or cooling
  • B29C 51/46 - Measuring, controlling or regulating
  • B29L 7/00 - Flat articles, e.g. films or sheets
  • B29L 31/30 - Vehicles, e.g. ships or aircraft, or body parts thereof
  • E04C 2/38 - Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure with attached ribs, flanges, or the like, e.g. framed panels

70.

AIRCRAFT CARGO DOOR ACTUATION SYSTEM

      
Application Number 18926829
Status Pending
Filing Date 2024-10-25
First Publication Date 2025-05-01
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations GmbH (Germany)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • K V, Mayur
  • Ramaraja, Nishith
  • Bentivoglio, Marc Antonio
  • Brito Maur, Cristobal Federico
  • Thomas, Benoît
  • Grisel, Dominique
  • Jagadeesan, Jayaparthan
  • Lutz, Marco

Abstract

A method of opening a cargo door of an aircraft, the aircraft including a body with an opening into a cargo bay, and a cargo door which covers the opening when it is in a closed position. A cargo door is outwardly rotated with a first actuator from the closed position to a first open position. Then an actuator rod is installed by coupling a first end of an actuator rod to the body and coupling a second end of the actuator rod to the cargo door in the first open position. Then the cargo door is outwardly rotated with the actuator rod from the first open position to a second open position by increasing a distance between the first and second ends of the actuator rod.

IPC Classes  ?

  • B64C 1/14 - WindowsDoorsHatch covers or access panelsSurrounding frame structuresCanopiesWindscreens
  • E05F 15/60 - Power-operated mechanisms for wings using electrical actuators

71.

A300

      
Application Number 1852020
Status Registered
Filing Date 2024-12-13
Registration Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment

Goods & Services

Aircraft, parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes. Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games.

72.

AIRCRAFT CARGO DOOR ACTUATION SYSTEM

      
Application Number 18926793
Status Pending
Filing Date 2024-10-25
First Publication Date 2025-05-01
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations GmbH (Germany)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • K V, Mayur
  • Ramaraja, Nishith
  • Bentivoglio, Marc Antonio
  • Brito Maur, Cristobal Federico
  • Thomas, Benoît
  • Grisel, Dominique
  • Jagadeesan, Jayaparthan
  • Lutz, Marco

Abstract

An actuation system for a cargo door of an aircraft. The cargo door covers an opening into a cargo bay when it is in a closed position. The actuation system includes a first actuator configured to outwardly rotate the cargo door from the closed position to a first open position, and a second actuator configured to outwardly rotate the cargo door from the first open position to a second open position.

IPC Classes  ?

  • B64C 1/14 - WindowsDoorsHatch covers or access panelsSurrounding frame structuresCanopiesWindscreens

73.

COMPONENT AND METHOD FOR MANUFACTURING SUCH A COMPONENT

      
Application Number 18820391
Status Pending
Filing Date 2024-08-30
First Publication Date 2025-04-24
Owner Airbus (S.A.S.) (France)
Inventor
  • Beier, Uwe
  • Friedberger, Alois

Abstract

A component includes at least a first sub-component and a second sub-component each fully or partially including metal or metal alloy material or having an at least partially metallized surface or surface region, the first sub-component and the second sub-component providing a pair of connection interfaces configured to establish a permanent connection of the first sub-component and the second sub-component, wherein at least one of the pair of connection interfaces comprises nanowires. The disclosure further provides a method for manufacturing such a component.

IPC Classes  ?

  • B29C 70/86 - Incorporating in coherent impregnated reinforcing layers
  • B29C 70/38 - Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
  • B29C 70/88 - Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
  • B29L 31/30 - Vehicles, e.g. ships or aircraft, or body parts thereof

74.

METHOD AND SYSTEM USING A NEURAL NETWORK TO PREDICT A TIME OF OCCUPANCY OF A RUNWAY BY AN AIRCRAFT

      
Application Number 18906473
Status Pending
Filing Date 2024-10-04
First Publication Date 2025-04-24
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Lavielle-Barret, Isabelle
  • Chauvet, Olivier
  • Quentin, Alexandre
  • Mabille, Romain

Abstract

A prediction system with a unit for generating a current value of a parameter relating to the movement of an aircraft, a selection unit for a crew member of the aircraft to select an exit of the runway used for landing, an avionics computer for computing a value of the time of occupancy of the runway and a unit for transmitting this value to a user system. The avionics computer using an initial ground speed and an exit type and an exit distance of the exit selected, and computes the value of the time of occupancy of the runway, with the data and by using a prediction model comprising a neural network trained on the basis of landing data originating from previous landings.

IPC Classes  ?

  • G08G 5/06 - Traffic control systems for aircraft for control when on the ground
  • G06N 3/08 - Learning methods
  • G08G 5/00 - Traffic control systems for aircraft

75.

ENERGY SENDING METHOD, SENDING DEVICE AND AIRCRAFT, AS WELL AS ENERGY RECEIVING METHOD, RECEIVING DEVICE AND AIR VEHICLE COMPRISING SAME

      
Application Number 18906417
Status Pending
Filing Date 2024-10-04
First Publication Date 2025-04-17
Owner Airbus SAS (France)
Inventor Multerer, Thomas

Abstract

An energy sending method for sending an energy beam generated by a sender to an airborne receiver, by targeting an energy receiving element of the receiver; and sending the energy beam to the energy receiving element. Also a device for sending an energy beam to the airborne receiver, an aircraft comprising an energy sending device. Also, a method for receiving with an airborne receiver an energy beam generated by a sender, by receiving the energy beam with an energy receiving element of the receiver; and converting the energy beam for powering at least one energy sink of the receiver. Also, a device for receiving energy and powering an airborne receiver with an energy beam, and an air vehicle having the energy receiving device.

IPC Classes  ?

  • H02J 50/30 - Circuit arrangements or systems for wireless supply or distribution of electric power using light, e.g. lasers
  • H02J 50/80 - Circuit arrangements or systems for wireless supply or distribution of electric power involving the exchange of data, concerning supply or distribution of electric power, between transmitting devices and receiving devices
  • H02J 50/90 - Circuit arrangements or systems for wireless supply or distribution of electric power involving detection or optimisation of position, e.g. alignment

76.

PROPULSION ASSEMBLY FOR AN AIRCRAFT

      
Application Number 18908982
Status Pending
Filing Date 2024-10-08
First Publication Date 2025-04-17
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Devasigamani, Nandakumar
  • Czapla, Lionel
  • Carretero Benignos, Jorge A.

Abstract

A propulsion assembly having a propulsion system comprising a fairing, a rotary assembly having a combustion chamber and housed in the fairing, an exhaust nozzle positioned downstream of the combustion chamber and delimited by a nozzle wall, and ensuring the discharge of the combustion gases originating from the combustion of the dihydrogen in the combustion chamber, a dihydrogen tank, a supply duct which connects the tank and the combustion chamber, and at least one vane positioned inside the exhaust nozzle, wherein the supply duct has a duct portion arranged in the vane.

IPC Classes  ?

  • B64C 7/00 - Structures or fairings not otherwise provided for
  • B64D 33/04 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
  • B64D 37/30 - Fuel systems for specific fuels

77.

PROPULSION ASSEMBLY FOR AN AIRCRAFT

      
Application Number 18909029
Status Pending
Filing Date 2024-10-08
First Publication Date 2025-04-17
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Devasigamani, Nandakumar
  • Czapla, Lionel
  • Carretero Benignos, Jorge A.

Abstract

A propulsion assembly having a fairing, a combustion chamber housed in the fairing, an exhaust nozzle delimited by a nozzle wall, a dihydrogen tank, a double-walled supply duct between the tank and the combustion chamber that has an inner wall delimiting an inner volume for the circulation of the dihydrogen and, around it, an outer wall delimiting an outer volume, and a bypass chamber, which is positioned around the nozzle wall and in which is made an upstream orifice for the introduction of the combustion gases and a downstream orifice for the discharge of the combustion gases, and wherein the supply duct has a portion arranged in the bypass chamber.

IPC Classes  ?

  • B64C 7/02 - Nacelles
  • B64D 33/04 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
  • B64D 37/30 - Fuel systems for specific fuels

78.

METHOD AND NETWORKING NODE FOR INFORMATION CENTRIC DATA NETWORKING, FORWARDING DECISION PROGRAM, DATA CARRIER, AND VEHICLE COMPRISING A NETWORKING NODE

      
Application Number 18826751
Status Pending
Filing Date 2024-09-06
First Publication Date 2025-04-03
Owner Airbus SAS (France)
Inventor Milheiro Mendes, Paulo-Jorge

Abstract

A method for operating a networking node for information centric data networking, comprising queuing a number of request packets and data packets received at the node in a request queue and in a data queue, respectively; outbound request packets and data packets are prioritized over each other by a forward decision module based on a length of the request queue and/or the data queue. Also a forwarding decision program, a networking node, and a vehicle, in particular an aircraft, comprising at least one networking node.

IPC Classes  ?

  • H04L 47/62 - Queue scheduling characterised by scheduling criteria
  • H04L 47/625 - Queue scheduling characterised by scheduling criteria for service slots or service orders

79.

AIRCRAFT CABIN AIR DISTRIBUTION SYSTEM

      
Application Number 18887330
Status Pending
Filing Date 2024-09-17
First Publication Date 2025-03-27
Owner Airbus (S.A.S.) (France)
Inventor Komarla, Sasank

Abstract

An aircraft cabin air distribution system with a fuselage, a cabin in the fuselage, a supply duct, and outlets to feed air into the cabin. The outlets include upper outlets positioned at a higher level than the supply duct, and lower outlets positioned at a lower level than the supply duct. The aircraft cabin air distribution system also includes a branch ducts to feed air from the supply duct to the outlets, wherein each branch duct meets the supply duct at a respective junction. The branch ducts include upper branch ducts which each feed air to one or more of the upper outlets and lower branch ducts which each feed air to one or more of the lower outlets.

IPC Classes  ?

  • B64D 13/06 - Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
  • B64D 13/00 - Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space

80.

AIRPORT INSTALLATION INCLUDING A PLURALITY OF DIHYDROGEN STORAGE TANKS

      
Application Number 18887503
Status Pending
Filing Date 2024-09-17
First Publication Date 2025-03-27
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Dutheil, Jean-Philippe
  • Landolt, Jonathan

Abstract

An airport installation including a plurality of types of aircraft in which each aircraft of one type includes a tank containing dihydrogen at a saturation pressure in a first range different from the other first ranges, for each type of aircraft a storage tank at a saturation pressure in a second range associated with the type of aircraft, and for each storage tank pumps or other devices fill from the storage tank the tank of the aircraft of the type for which the first range corresponds to the storage tank.

IPC Classes  ?

  • F17C 5/00 - Methods or apparatus for filling pressure vessels with liquefied, solidified, or compressed gases
  • B64D 37/16 - Filling systems
  • B64F 1/36 - Other airport installations

81.

TECHNIQUE FOR COMMUNICATION CONNECTION ESTABLISHMENT BY A MOBILE UE USING A PHASED ARRAY ANTENNA

      
Application Number 18890045
Status Pending
Filing Date 2024-09-19
First Publication Date 2025-03-27
Owner
  • Airbus SAS (France)
  • Airbus Operations GmbH (Germany)
Inventor
  • Meyerhoff, Thomas
  • Shah, Aizaz
  • Grünheid, Rainer

Abstract

A method performed by a mobile user equipment, UE, comprising: obtaining measurement information from a mobile phased array antenna, PAA, separate from the UE, the measurement information indicating, for at least one signal received by the PAA from a plurality of base stations, a received power, RP; determining, for the signal, a quality measure based on the RP of the signals; and transmitting, to a network node, a first message indicating the determined quality measure and enabling the network node to select at least one of the plurality of base stations as a target base station for a communication connection with the UE. Also a computer program, a UE, and a system.

IPC Classes  ?

82.

AIRCRAFT COMPRISING A DIHYDROGEN SUPPLY SYSTEM AND A DIHYDROGEN HEAT TREATMENT SYSTEM

      
Application Number 18883043
Status Pending
Filing Date 2024-09-12
First Publication Date 2025-03-20
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Milliere, Jérôme
  • Verseux, Olivier
  • Landolt, Jonathan
  • Paget, Darren

Abstract

An aircraft comprising at least one dihydrogen tank, at least one dihydrogen consumer system, a supply line arranged between a consumer system and a tank, for each consumer system, a loop containing a heat transfer fluid, for each tank and each supply line, a supply heat exchanger which exchanges calories between the heat transfer fluid and the dihydrogen and, for each consumer system, a return heat exchanger which exchanges calories between the heat transfer fluid and the consumer system.

IPC Classes  ?

83.

POWERPLANT FOR AN AIRCRAFT

      
Application Number 18883246
Status Pending
Filing Date 2024-09-12
First Publication Date 2025-03-20
Owner
  • Airbus SAS (France)
  • Airbus Operations SAS (France)
Inventor
  • Czapla, Lionel
  • Pissavin, Alexis

Abstract

A powerplant for an aircraft, comprising a propulsion system with a core enclosed in a casing and having a combustion chamber, a supply pipe conveying dihydrogen to the combustion chamber by passing through the casing in an injection zone, and a closed enclosure, delimited by first and second walls and containing a downstream pipe, a treatment system for treating the dihydrogen, and the injection zone, wherein the first wall is formed by part of the casing.

IPC Classes  ?

84.

AIRCRAFT FUSELAGE

      
Application Number 18819322
Status Pending
Filing Date 2024-08-29
First Publication Date 2025-03-06
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations GmbH (Germany)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Nagara Venkatachala, Adithya
  • Jagadeesan, Jayaparthan
  • Brito Maur, Cristobal Federico
  • Thomas, Benoît

Abstract

An aircraft fuselage includes fore and aft sections, a barrier wall separating the sections and an opening therebetween, a rail attached to the barrier wall, a door moveable across the barrier wall between an open position offset from the opening and a closed position covering the opening, a first roller and a second roller rotatably fixed to the door and moveable on the rail along first and second paths to move the door, the rail including a first ramp engaging the first roller as it moves along the first path and to direct the first roller towards the barrier wall, and a second ramp engaging the second roller as it moves along the second path and to direct the second roller towards the barrier wall, the first roller configured to engage the first ramp as the second roller engages the second ramp to move the door towards the barrier wall.

IPC Classes  ?

  • B64C 1/14 - WindowsDoorsHatch covers or access panelsSurrounding frame structuresCanopiesWindscreens

85.

METHOD FOR MANAGING TAXIING PATHS

      
Application Number 18806150
Status Pending
Filing Date 2024-08-15
First Publication Date 2025-03-06
Owner
  • AIRBUS SAS (France)
  • AIRBUS OPERATIONS SAS (France)
Inventor
  • Mazoin, Benjamin
  • Fersing, Laura

Abstract

A method for managing taxiing paths of an aircraft includes at least one computer system, the method being implemented by the computer system. The method includes the following steps: editing an initial path; displaying a route of the initial path on a screen using a first route symbolism; obtaining a validation of the initial path; displaying a route of the validated initial path on the screen using a second route symbolism; implementing the validated initial path in a taxiing setpoint of the aircraft. The method further includes an editing process and an independent display process.

IPC Classes  ?

  • G08G 5/00 - Traffic control systems for aircraft
  • B64D 43/00 - Arrangements or adaptations of instruments
  • G06F 3/04842 - Selection of displayed objects or displayed text elements

86.

VENT SYSTEM

      
Application Number 18812481
Status Pending
Filing Date 2024-08-22
First Publication Date 2025-02-27
Owner
  • Airbus Operations Limited (United Kingdom)
  • Airbus (S.A.S.) (France)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Mangat, Vikram Singh
  • Greco, Eric
  • Fesselier, Emmanuel
  • Wolf, Pierre
  • Noah, Haziq

Abstract

A vent system includes a vent stack for venting a tank fluid from a fuel tank that is external to the vent stack, during fuelling of the fuel tank. The vent stack includes a conduit including a conduit inlet and a conduit outlet, the conduit outlet opening to atmosphere external to the conduit. The vent stack also includes an opening into the conduit between the conduit inlet and the conduit outlet. The opening is fluidically connected, or connectable, to the fuel tank so the tank fluid from the fuel tank flows through the opening to the conduit outlet, in use. The vent stack also includes a fluid mover operable to cause a mixer fluid receivable in the conduit inlet to flow through the conduit towards the conduit outlet, thereby to mix the mixer fluid with the tank fluid in the conduit, upstream of the conduit outlet.

IPC Classes  ?

  • B64D 37/16 - Filling systems
  • B64D 37/00 - Arrangements in connection with fuel supply for power plant
  • B64D 37/06 - Constructional adaptations thereof

87.

COMPUTING DEVICE, METHODS FOR PROVIDING AND CONFIGURING A COMPUTING DEVICE, AS WELL AS COMPUTER SYSTEM INTEGRATION ARRANGEMENT, PROGRAM AND COMPUTER-READABLE DATA CARRIER

      
Application Number 18800365
Status Pending
Filing Date 2024-08-12
First Publication Date 2025-02-20
Owner Airbus SAS (France)
Inventor
  • Uhrig, Sascha
  • Freitag, Johannes

Abstract

A computing device comprising at least one processing module carrying multiple execution units each with a local memory unit; and a local network of the processing module linking at least some of the execution units to each other by respective communication paths; wherein the execution units are configured to execute a binary code segment at least temporarily stored in their respective associated local memory unit and derived from a computer executable program code application containing application code sections; and wherein at least one of the execution units is designated for executing a binary code segment as an assigned binary code segment based on a pre-determined runtime schedule with fixed time slots during which the execution unit is granted exclusive access to at least one of the communication paths when executing the assigned binary code segment in line with a pre-defined running order of the application code sections.

IPC Classes  ?

  • G06F 9/48 - Program initiatingProgram switching, e.g. by interrupt
  • G06F 9/30 - Arrangements for executing machine instructions, e.g. instruction decode

88.

DATA SENDING METHOD, ENTRY GATEWAY AND COMMUNICATION STATION, AS WELL AS DATA RECEIVING METHOD, EXIT GATEWAY AND VEHICLE COMPRISING SAME

      
Application Number 18800373
Status Pending
Filing Date 2024-08-12
First Publication Date 2025-02-20
Owner Airbus SAS (France)
Inventor Milheiro Mendes, Paulo-Jorge

Abstract

A data sending method for sending an internet data packet from at least one sender via a data entry gateway connected to an ICN infrastructure to at least one receiver, and a data receiving method for receiving with at least one receiver an internet data packet from at least one sender via a data exit gateway connected to an ICN infrastructure, as well as a corresponding data entry gateway, a corresponding data exit gateway, and a communication station, and a vehicle comprising respective gateways.

IPC Classes  ?

  • H04L 67/63 - Routing a service request depending on the request content or context
  • H04L 12/46 - Interconnection of networks
  • H04L 12/66 - Arrangements for connecting between networks having differing types of switching systems, e.g. gateways

89.

DEVICE FOR COOLING AN ELECTRICAL EQUIPMENT ITEM, CORRESPONDING SYSTEM AND AIRCRAFT COMPRISING AT LEAST ONE SUCH SYSTEM

      
Application Number 18794697
Status Pending
Filing Date 2024-08-05
First Publication Date 2025-02-13
Owner Airbus SAS (France)
Inventor Loehrmann, Antoine

Abstract

A device for cooling an electrical equipment item including a circulation channel containing a flow of a diphase coolant; a thermally conductive wall configured to separate the channel and the electrical equipment item, at least one fin disposed within the channel and extending from the wall, each fin being configured to be in a position close to the wall when the temperature of the fin is less than a predetermined temperature, and to be in a distant position when the temperature of the fin is greater than or equal to the predetermined temperature. Such a device makes it possible to effectively cool an electrical equipment item without having to decrease the power thereof in the case of very high thermal losses.

IPC Classes  ?

  • H05K 7/20 - Modifications to facilitate cooling, ventilating, or heating

90.

QUANTUM KEY DISTRIBUTION (QKD) METHOD, QKD END-NODE AND QKD NETWORK

      
Application Number 18772648
Status Pending
Filing Date 2024-07-15
First Publication Date 2025-01-30
Owner Airbus SAS (France)
Inventor Milheiro Mendes, Paulo-Jorge

Abstract

A quantum key distribution, QKD, method, applied to a QKD end-node by locally generating a local key, and dividing the local key into a first local key part and a second local key part, receiving, via a ground-based first path, remote key information including an encrypted remote key generated by a remote, further QKD end-node. In addition, the method includes receiving, via a satellite-based second path, a first remote key part of the remote key and performing decryption on the remote key information using the first remote key part to obtain a second remote key part of the remote key. The method further comprises combining the second remote key part and the second local key part with each other to obtain a secret key. Also an end-node configured to perform such a method and a network with such an end-node.

IPC Classes  ?

91.

METHOD AND SYSTEM FOR AUTOMATICALLY GUIDING AN AIRCRAFT TO A LANDING RUNWAY

      
Application Number 18770043
Status Pending
Filing Date 2024-07-11
First Publication Date 2025-01-23
Owner
  • Airbus (S.A.S.) (France)
  • Airbus Operations (S.A.S.) (France)
Inventor
  • Litvova, Monika
  • Penverne, Emmanuel
  • Bernard, Denys
  • Gine Soca, Albert

Abstract

A method for automatically guiding an aircraft includes receiving an ATIS message and decoding the content of the ATIS message. If the decoded content of the ATIS message includes a parameter relating to an active landing runway, the method includes creating a message requesting confirmation of the decoded content and commanding the sending of the message over a communication frequency with air traffic control, receiving a response from air traffic control and decoding the response to determine whether or not the response is a confirmation of the decoded content of the ATIS message. If the response is a confirmation of the decoded content of the ATIS message, the method includes determining a contingency trajectory of the aircraft at least partially in consideration of the decoded content of the ATIS message. The method also includes automatically guiding the aircraft along the determined contingency trajectory.

IPC Classes  ?

  • G08G 5/02 - Automatic landing aids, i.e. systems in which flight data of incoming planes are processed to provide landing data
  • G08G 5/00 - Traffic control systems for aircraft
  • G10L 15/26 - Speech to text systems

92.

AIRCRAFT GROUND ANTI-COLLISION SYSTEM AND METHOD

      
Application Number 18775593
Status Pending
Filing Date 2024-07-17
First Publication Date 2025-01-23
Owner AIRBUS (S.A.S.) (France)
Inventor Huang, Jinming

Abstract

An aircraft ground anti-collision system and method is disclosed including multiple sensors including an on-board sensor and an off-board sensor, and an obstacle detection processing unit, which is configured to: process data received from the multiple sensors to detect an object around the aircraft and/or a trailer for towing the aircraft, and fuse sensing ranges of the multiple sensors and unify information about the object detected by the multiple sensors in a same coordinate system, to generate a view-angle fused view indicating the detected object. Hence, vision blind areas of a pilot and a ground operator during ground movement of the aircraft can be advantageously eliminated, and the cooperation and scene awareness of the pilot and the ground operator can be improved, thereby reducing the accident rate and improving the safety of the ground movement.

IPC Classes  ?

  • G08G 5/04 - Anti-collision systems
  • G06T 15/10 - Geometric effects
  • G06V 20/58 - Recognition of moving objects or obstacles, e.g. vehicles or pedestriansRecognition of traffic objects, e.g. traffic signs, traffic lights or roads
  • G08G 5/00 - Traffic control systems for aircraft

93.

DETECTION MODULE, DETECTION DEVICE, DIGITAL DETECTION SYSTEM, AND DETECTION METHOD

      
Application Number EP2024067837
Publication Number 2025/016683
Status In Force
Filing Date 2024-06-25
Publication Date 2025-01-23
Owner AIRBUS (S.A.S.) (France)
Inventor Huang, Jinming

Abstract

The present disclosure relates to a detection module, a detection device, a digital detection system, and a detection method. The detection module includes: a scanning unit and a processor. The scanning unit is configured to perform three-dimensional scanning on a detected surface, and includes a laser projecting device and a laser receiving device. The laser projecting device includes a laser source and a MEMS micro scanning mirror. The laser receiving device is configured to receive the laser radiation returning from the detected surface to obtain a laser image of the detected surface. The processor is configured to receive and process the laser image to detect a defect on the detected surface. The scanning unit further includes an RGB image sensor configured to obtain an RGB image of the detected surface. The processor is further configured to obtain the RGB image and detect a defect on the detected surface based on the laser image and the RGB image. The present disclosure can achieve the miniaturization of the detection module and improve the detection accuracy of the detection module.

IPC Classes  ?

  • G01B 11/25 - Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures by projecting a pattern, e.g. moiré fringes, on the object
  • G01N 21/88 - Investigating the presence of flaws, defects or contamination

94.

PAINTING DEVICE HAVING A MOVABLE ROBOTIC ARM CARRYING A TOOL AND A MOVABLE PIECE OF EQUIPMENT CONNECTED BY AN UMBILICAL CONNECTION TO THE TOOL

      
Application Number 18734340
Status Pending
Filing Date 2024-06-05
First Publication Date 2024-12-26
Owner
  • Airbus SAS (France)
  • Airbus Operations S.L. (Spain)
  • Airbus Operations GmbH (Germany)
Inventor
  • Lagutin, Wladislav
  • Garcia Amado, Juan Francisco
  • Moriniere, Boris

Abstract

A painting device including at least one guide system, at least a first movable support configured to move along the guide system, a robotic arm secured to the first movable support, at least a first tool connected to the free end of the robotic arm, and at least a first piece of equipment connected to the first tool by at least one umbilical connection, the first piece of equipment being movable and connected to the first movable support. This configuration makes it possible to reduce the length of the umbilical connection. A painting installation having at least one such painting device is also provided.

IPC Classes  ?

  • B25J 11/00 - Manipulators not otherwise provided for

95.

PAINTING SYSTEM FOR AN AIRCRAFT COMPRISING A PAINT BOOTH OF REDUCED CROSS SECTION

      
Application Number 18751620
Status Pending
Filing Date 2024-06-24
First Publication Date 2024-12-26
Owner
  • Airbus SAS (France)
  • Airbus Operations S.L. (Spain)
  • Airbus Operations GmbH (Germany)
Inventor
  • Lagutin, Wladislav
  • Garcia Amado, Juan Francisco
  • Moriniere, Boris

Abstract

A painting system suitable for painting a fuselage of an aircraft, including a paint booth which is positioned on a platform. This paint booth includes at least first and second lateral openings which are configured to permit the wings of the aircraft to pass through the paint booth, in addition to at least two elements, at least one thereof being mobile between an adjacent position corresponding to a closed state of the paint booth in which the two elements are joined together, in addition to a spaced-apart position corresponding to an open state of the paint booth in which the fuselage can be positioned between the two elements.

IPC Classes  ?

  • B05B 16/80 - Movable spray booths
  • B05B 16/40 - Construction elements specially adapted therefor, e.g. floors, walls or ceilings

96.

A330

      
Application Number 240012700
Status Pending
Filing Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 21 - HouseHold or kitchen utensils, containers and materials; glassware; porcelain; earthenware
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services

Goods & Services

(1) Aéronefs; pièces, composants structurels et parties constitutives pour aéronefs; avions; pièces, composants structurels et parties constitutives pour avions. (2) Tasses; mugs; bouteilles. (3) Vêtements; chapellerie; chaussures. (4) Modèles réduits de véhicules et leurs pièces; jouets; jeux; appareils de jeux vidéo; consoles de jeux vidéo; maquettes de véhicules (jouets); jeux éducatifs; jeux électroniques. (1) Réparation, installation, entretien et révision dans le domaine de l'aviation; assistance technique et conseils techniques (réparation, installation, entretien et révision) dans le domaine de l'aviation; services de conseils et d'information en matière de réparation, installation, entretien et révision dans le domaine de l'aviation. (2) Services de divertissement dans le domaine de l'aviation; organisation de démonstrations aériennes pour information et pour le divertissement; services d'éducation et d'instruction dans le domaine de l'aviation; formation de pilotes et de personnel de cabine; formation d'ingénieurs, de mécaniciens et de techniciens.

97.

A319

      
Application Number 239720300
Status Pending
Filing Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 12 - Land, air and water vehicles; parts of land vehicles
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 37 - Construction and mining; installation and repair services
  • 41 - Education, entertainment, sporting and cultural services

Goods & Services

(1) Aéronefs; pièces, composants, connecteurs et parties constitutives pour aéronefs; avions; pièces, composants, connecteurs et parties constitutives pour avions. (2) Vêtements; chapellerie; chaussures. (3) Modèles réduits de véhicules et leurs pièces; jouets; jeux; appareils de jeux vidéo; appareils de jeux vidéo; consoles de jeux vidéo; consoles de jeux d'ordinateur; maquettes de véhicules (jouets); jeux éducatifs; jeux électroniques. (1) Réparation, installation, entretien et révision dans le domaine de l'aviation; assistance technique et conseils techniques dans le domaine de l'aviation; services de conseils et d'information en matière de réparation, installation, entretien et révision dans le domaine de l'aviation. (2) Services de divertissement dans le domaine de l'aviation; organisation de démonstrations aériennes pour information et pour le divertissement; services d'éducation et d'instruction dans le domaine de l'aviation; formation de pilotes et de personnel de cabine; formation d'ingénieurs, de mécaniciens et de techniciens.

98.

A300

      
Serial Number 79422651
Status Pending
Filing Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 12 - Land, air and water vehicles; parts of land vehicles

Goods & Services

Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games. Aircraft, parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes.

99.

A310

      
Serial Number 79422652
Status Pending
Filing Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 12 - Land, air and water vehicles; parts of land vehicles

Goods & Services

Clothing; headwear; shoes. Scale model vehicles and parts thereof; toys; games; video game apparatus; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games. Aircraft; parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes.

100.

CARAVELLE

      
Serial Number 79422653
Status Pending
Filing Date 2024-12-13
Owner Airbus S.A.S. (France)
NICE Classes  ?
  • 25 - Clothing; footwear; headgear
  • 28 - Games; toys; sports equipment
  • 12 - Land, air and water vehicles; parts of land vehicles

Goods & Services

Clothing; headwear; shoes; none of the aforesaid goods for or relating to maternity, postpartum or breastfeeding. Scale model vehicles and parts thereof; toys; games; the aforesaid goods excluding motor vehicles; video game apparatus; video game consoles; computer game consoles; model vehicles (toys); educational games; electronic games. Aircraft; parts, components and component parts for aircraft; airplanes; parts, components and component parts for airplanes.
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