In a method for de-icing a component (12) of an aircraft (2) using a reformer (4) for hydrogen (6) for a fuel cell (10), which reformer creates waste heat (8), the waste heat (8) of the reformer (4) is transported by means of a heat channel (14) to the component (12) in order to heat and de-ice the component. In a method for retrofitting an aircraft with a de-icing device with a heat channel leading to the component, the aircraft is equipped with the reformer/the fuel cell, and the heat channel is upgraded to transport at least additionally waste heat of the reformer to the component and the aircraft is upgraded for the execution of the above-described method. A de-icing device (51) for the aircraft (2) is designed to execute the de-icing method. The aircraft (2) contains the de-icing device (51), the reformer (4), the fuel cell (10), and the component (12).
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
comprising at least one LED (18a-f) having an operating parameter (B), with the LED (18a-f) being able to be dimmed based on a change in said operating parameter, wherein each of the LEDs (18a-f) is assigned a minimum value (Ma-f) of the operating parameter (B) from which the LED (18a-f) lights up,
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
comprising at least one LED (18a-f) having an operating parameter (B), with the LED (18a-f) being able to be dimmed based on a change in said operating parameter, wherein each of the LEDs (18a-f) is assigned a minimum value (Ma-f) of the operating parameter (B) from which the LED (18a-f) lights up,
comprising a control input (16) for receiving an as-intended control signal (14) for the luminaire,
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
comprising at least one LED (18a-f) having an operating parameter (B), with the LED (18a-f) being able to be dimmed based on a change in said operating parameter, wherein each of the LEDs (18a-f) is assigned a minimum value (Ma-f) of the operating parameter (B) from which the LED (18a-f) lights up,
comprising a control input (16) for receiving an as-intended control signal (14) for the luminaire,
wherein the control signal (14) has, in addition to a switch-off value (A), at least two different dimming values (D1, 2) as control values(S), which correspond to respective different brightnesses (H1, 2) of the LEDs (18a-f),
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
comprising at least one LED (18a-f) having an operating parameter (B), with the LED (18a-f) being able to be dimmed based on a change in said operating parameter, wherein each of the LEDs (18a-f) is assigned a minimum value (Ma-f) of the operating parameter (B) from which the LED (18a-f) lights up,
comprising a control input (16) for receiving an as-intended control signal (14) for the luminaire,
wherein the control signal (14) has, in addition to a switch-off value (A), at least two different dimming values (D1, 2) as control values(S), which correspond to respective different brightnesses (H1, 2) of the LEDs (18a-f),
comprising a control unit (22) containing an assignment rule (24) for the LEDs (18a-f), wherein each of the control values (S) is assigned a specific value of the operating parameter (B) of each of the LEDs (18a-f) based on the assignment rule (24),
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
comprising at least one LED (18a-f) having an operating parameter (B), with the LED (18a-f) being able to be dimmed based on a change in said operating parameter, wherein each of the LEDs (18a-f) is assigned a minimum value (Ma-f) of the operating parameter (B) from which the LED (18a-f) lights up,
comprising a control input (16) for receiving an as-intended control signal (14) for the luminaire,
wherein the control signal (14) has, in addition to a switch-off value (A), at least two different dimming values (D1, 2) as control values(S), which correspond to respective different brightnesses (H1, 2) of the LEDs (18a-f),
comprising a control unit (22) containing an assignment rule (24) for the LEDs (18a-f), wherein each of the control values (S) is assigned a specific value of the operating parameter (B) of each of the LEDs (18a-f) based on the assignment rule (24),
the assignment rule (24) is calculated such that the minimum value (Ma-f) of the operating parameter (B) for each of the LEDs (18a-f) is at least reached for each of the dimming values (D1, 2).
In a luminaire (10a, b) for a passenger cabin (2) of a passenger aircraft (4),
comprising at least one LED (18a-f) having an operating parameter (B), with the LED (18a-f) being able to be dimmed based on a change in said operating parameter, wherein each of the LEDs (18a-f) is assigned a minimum value (Ma-f) of the operating parameter (B) from which the LED (18a-f) lights up,
comprising a control input (16) for receiving an as-intended control signal (14) for the luminaire,
wherein the control signal (14) has, in addition to a switch-off value (A), at least two different dimming values (D1, 2) as control values(S), which correspond to respective different brightnesses (H1, 2) of the LEDs (18a-f),
comprising a control unit (22) containing an assignment rule (24) for the LEDs (18a-f), wherein each of the control values (S) is assigned a specific value of the operating parameter (B) of each of the LEDs (18a-f) based on the assignment rule (24),
the assignment rule (24) is calculated such that the minimum value (Ma-f) of the operating parameter (B) for each of the LEDs (18a-f) is at least reached for each of the dimming values (D1, 2).
A luminaire arrangement (6) for a passenger cabin (2) of a passenger aircraft (4) comprising at least one luminaire (10a, b) contains a light control system (8) connected to the control input (16) and set up to generate the as-intended control signal (14).
An actuator (12) for a vehicle (2) having at least two redundant similar vehicle electrical systems (4a,b), which are each provided for full electrical working power (Aa,b) and full powerline communication (PLCa,b), contains an electric drive (16) having supply inputs (24a,b) for the working power (Aa,b) and having similar redundant supply units (26a,b), which comprise a supply output (28a,b) for the full working power (Aa,b) and an electrical-system terminal (14a,b) for the electrical systems (4a,b) for receiving the full working power (Aa,b) and for the full powerline communication (PLCa,b) with the electrical system (4a,b). A vehicle (2) having the electrical systems (4a,b) contains the actuator (12), which is redundantly connected to the electrical systems (4a,b) by means of its electrical-system terminals (4a,b) in order to allow redundant supply with full working power (Aa,b) and to allow redundant full powerline communication (PLCa,b).
B64D 1/00 - Largage, éjection ou réception, en cours de vol, d'objets, de liquides ou similaires
H04B 3/54 - Systèmes de transmission par lignes de réseau de distribution d'énergie
H02P 25/00 - Dispositions ou procédés pour la commande de moteurs à courant alternatif caractérisés par le type de moteur ou par des détails de structure
09 - Appareils et instruments scientifiques et électriques
Produits et services
Control systems and control computers for displays; Computers and sensors for controlling and managing aeroplane and supply systems, in particular in the cockpits and cabins of aeroplanes; Displaying apparatus, Cinematographic equipment, Video devices; Displays for aircraft; Control systems and control computers for lighting in aircraft; Control systems and control computers for entertainment electronics in aircraft; Control systems and control computers for seat status monitoring.
5.
CABIN FOR AN AIRCRAFT, HAVING A MONITORING ASSEMBLY, AIRCRAFT HAVING THE CABIN, MONITORING ASSEMBLY AND METHOD FOR MONITORING A CABIN OF AN AIRCRAFT
In order to control a flow of persons and to implement distancing rules in a cabin (1) for an aircraft, a cabin (1) having a first monitored region (11) and a second monitored region (14) is provided. The cabin (1) has a monitoring assembly (10) for monitoring the first monitored region (11) and the second monitored region (14). The monitoring assembly (10) comprises at least one output device (25), which is designed and/or arranged to output an authorization signal (26) and/or a prohibition signal (27) regarding a change in a position and/or presence of at least one person in the first monitored region (11) and/or in the second monitored region (14).
c) which is formed from an electrically controllable colour-changing film (20), wherein at least a part of the colour-changing film (20) forms a visible surface (22) for the intended purpose in the passenger cabin (2).
A component (6) for a passenger cabin (2) of a passenger aircraft (4) contains a base body (8) with a surface (10), and a layer structure (12), which is applied to the surface (10) and contains at least two layers in the form of at least one active layer (14) and an adhesive layer (16) arranged between the active layer (14) and the surface (10), wherein the active layer (14) contains at least one surface section (18a-c) which is formed from an electrically controllable colour-changing film (20), wherein at least a part of the colour- changing film (20) forms a visible surface (22) for the intended purpose in the passenger cabin (2).
In a method for de-icing a component (12) of an aircraft (2) using a reformer (4) for hydrogen (6) for a fuel cell (10), which reformer creates waste heat (8), the waste heat (8) of the reformer (4) is transported by means of a heat channel (14) to the component (12) in order to heat and de-ice the component. In a method for retrofitting an aircraft with a de-icing device with a heat channel leading to the component, the aircraft is equipped with the reformer / the fuel cell, and the heat channel is upgraded to transport at least additionally waste heat of the reformer to the component and the aircraft is upgraded for the execution of the above-described method. A de-icing device (51) for the aircraft (2) is designed to execute the de-icing method. The aircraft (2) contains the de-icing device (51), the reformer (4), the fuel cell (10), and the component (12).
An inspection arrangement (8) for an interior (4) with objects (6) of a passenger vehicle (2) contains an image recording unit (10a-c) for an image (18) of the interior (4) of the vehicle (2) with the object (6), a classification database (20) with classification values (22) for the objects (6) and assignment rules (24) for assigning the classification values (22) to specific image contents (26) depicting the objects (6), an image analysis unit (28) which is connected to the database (20) in order to automatically analyse the image contents (26) and to assign classification values (22) according to the assignment rules (24), and interfaces (30a,b) for the input and/or output of classification values (22) and/or images (18) from and/or to a downstream entity (34).
An inspection arrangement (8) for an interior (4) with objects (6) of a passenger vehicle (2) contains an image recording unit (10a-c) for an image (18) of the interior (4) of the vehicle (2) with the object (6), a classification database (20) with classification values (22) for the objects (6) and assignment rules (24) for assigning the classification values (22) to specific image contents (26) depicting the objects (6), an image analysis unit (28) which is connected to the database (20) in order to automatically analyse the image contents (26) and to assign classification values (22) according to the assignment rules (24), and interfaces (30a,b) for the input and/or output of classification values (22) and/or images (18) from and/or to a downstream entity (34).
In an inspection method with the aid of the inspection arrangement (8), an image (18) is recorded, the image content (26) analysed automatically using the database (20) by the analysis unit (28), and classification values (22) assigned with the aid of the assignment rules (24) to the image content (26), and the classification values (22) assigned to the image (18), and optionally also the image (18), are output via the interfaces (30a,b) to a downstream entity (34) and/or input.
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
G06V 20/59 - Contexte ou environnement de l’image à l’intérieur d’un véhicule, p. ex. concernant l’occupation des sièges, l’état du conducteur ou les conditions de l’éclairage intérieur
An inspection arrangement (8) for an interior (4) with objects (6) of a passenger vehicle (2) contains an image recording unit (10a-c) for an image (18) of the interior (4) of the vehicle (2) with the object (6), a classification database (20) with classification values (22) for the objects (6) and assignment rules (24) for assigning the classification values (22) to specific image contents (26) depicting the objects (6), an image analysis unit (28) which is connected to the database (20) in order to automatically analyse the image contents (26) and to assign classification values (22) according to the assignment rules (24), and interfaces (30a,b) for the input and/or output of classification values (22) and/or images (18) from and/or to a downstream entity (34). In an inspection method with the aid of the inspection arrangement (8), an image (18) is recorded, the image content (26) analysed automatically using the database (20) by the analysis unit (28), and classification values (22) assigned with the aid of the assignment rules (24) to the image content (26), and the classification values (22) assigned to the image (18), and optionally also the image (18), are output via the interfaces (30a,b) to a downstream entity (34) and/or input.
G06V 10/764 - Dispositions pour la reconnaissance ou la compréhension d’images ou de vidéos utilisant la reconnaissance de formes ou l’apprentissage automatique utilisant la classification, p. ex. des objets vidéo
G06V 20/59 - Contexte ou environnement de l’image à l’intérieur d’un véhicule, p. ex. concernant l’occupation des sièges, l’état du conducteur ou les conditions de l’éclairage intérieur
G06Q 10/20 - Administration de la réparation ou de la maintenance des produits
11.
ROOM REGION FOR AN AIRCRAFT, AIRCRAFT HAVING THE ROOM REGION, AND METHOD FOR DISINFECTING A SURFACE OF A ROOM REGION BY MEANS OF A DISINFECTING DEVICE
A room region (1) for an aircraft is provided, which room region comprises a disinfecting device (3) for disinfecting at least one surface (4) of the room region (1), wherein the disinfecting device (3) is designed to disinfect the surface (4) of the room region (1) by means of UVC radiation (5). The disinfecting device (3) comprises a lighting apparatus (6) for generating and emitting the UVC radiation (5). The lighting apparatus (6) is portable, and, in an active state, the lighting apparatus (6) is stationary and arranged.
A61L 2/10 - Procédés ou appareils de désinfection ou de stérilisation de matériaux ou d'objets autres que les denrées alimentaires ou les lentilles de contactAccessoires à cet effet utilisant des phénomènes physiques des radiations des ultraviolets
A pane assembly (2) for a window (8) arranged in the outer wall (4) of an aircraft (6) in a window plane (10) contains a transparent cover pane (12) in a cover plane (14), a switching film (16) in a scattering plane (18), which is switchable between a transparent state (ZT) and a diffuse state (ZD), a luminous film (20) in a light plane (22) having LEDs (24), wherein a spacing (A) between each two LEDs (24) in relation to one another is at least five times their transverse extension (Q), wherein the pane assembly (2) is arranged in front of the window (8) in an installed state (M), so that scattering plane (18), light plane (22), and window plane (10) extend in parallel to one another and the luminous film (20) is arranged between the window (8) and the switching film (16), and window (8), switching film (16), and luminous film (20) are located aligned one behind another on the line of sight (26).
A window assembly (40) contains the window (8) and the pane assembly (2) arranged in front of it in the installed state (M).
A pane assembly (2) for a window (8) arranged in the outer wall (4) of an aircraft (6) in a window plane (10) contains a transparent cover pane (12) in a cover plane (14), a switching film (16) in a scattering plane (18), which is switchable between a transparent state (ZT) and a diffuse state (ZD), a luminous film (20) in a light plane (22) having LEDs (24), wherein a spacing (A) between each two LEDs (24) in relation to one another is at least five times their transverse extension (Q), wherein the pane assembly (2) is arranged in front of the window (8) in an installed state (M), so that scattering plane (18), light plane (22), and window plane (10) extend in parallel to one another and the luminous film (20) is arranged between the window (8) and the switching film (16), and window (8), switching film (16), and luminous film (20) are located aligned one behind another on the line of sight (26). A window assembly (40) contains the window (8) and the pane assembly (2) arranged in front of it in the installed state (M).
The invention relates to a passenger cabin (4) for a passenger aircraft (2), comprising an illumination assembly (6) for the passenger cabin (4), the illumination assembly (6) containing: - a control cable (8); - a data bus (9); - a luminaire assembly (10), which is connected to the data bus (9); - a first decoder (24), which is connected to the control cable (8) and to the data bus (9); - an operating unit (14), which is connected to the control cable (8) and which has two operating elements (16a-d) for selecting, by means of the transmission of first control signals (20) from the operating unit (14) to the first decoder (24) via the control cable (8), predefined light scenarios (18) to be produced by the luminaire assembly (10); wherein: each of the operating elements (16a-d) is assigned its own first control signal (20); the first decoder (24) has a decoding specification (24) having a menu structure, wherein each menu element (28) of the menu structure is selected by means of a specific sequence (50) of successively received first control signals (20); each menu element (28) of the menu structure is assigned exactly one predefined light scenario of the light scenarios (18) which are to be produced by the luminaire assembly (10); each light scenario (18) is assigned a data set, which is stored in the first decoder (24) and has light scene data, from which second control signals (21) to be sent to the luminaire assembly (10) via the data bus (9) can be produced by means of the first decoder (24).
A room region (1) for an aircraft is provided, which room region comprises a disinfecting device (3) for disinfecting at least one surface (4) of the room region (1), wherein the disinfecting device (3) is designed to disinfect the surface (4) of the room region (1) by means of UVC radiation (5). The disinfecting device (3) comprises a lighting apparatus (6) for generating and emitting the UVC radiation (5). The lighting apparatus (6) is portable, and, in an active state, the lighting apparatus (6) is stationary and arranged.
A61L 2/10 - Procédés ou appareils de désinfection ou de stérilisation de matériaux ou d'objets autres que les denrées alimentaires ou les lentilles de contactAccessoires à cet effet utilisant des phénomènes physiques des radiations des ultraviolets
A room region (1) for an aircraft is provided, which room region comprises a disinfecting device (3) for disinfecting at least one surface (4) of the room region (1), wherein the disinfecting device (3) is designed to disinfect the surface (4) of the room region (1) by means of UVC radiation (5). The disinfecting device (3) comprises a lighting apparatus (6) for generating and emitting the UVC radiation (5). The lighting apparatus (6) is portable, and, in an active state, the lighting apparatus (6) is stationary and arranged.
A61L 2/10 - Procédés ou appareils de désinfection ou de stérilisation de matériaux ou d'objets autres que les denrées alimentaires ou les lentilles de contactAccessoires à cet effet utilisant des phénomènes physiques des radiations des ultraviolets
17.
CABIN FOR AN AIRCRAFT, HAVING A MONITORING ASSEMBLY, AIRCRAFT HAVING THE CABIN, MONITORING ASSEMBLY AND METHOD FOR MONITORING A CABIN OF AN AIRCRAFT
In order to control a flow of persons and to implement distancing rules in a cabin (1) for an aircraft, a cabin (1) having a first monitored region (11) and a second monitored region (14) is provided. The cabin (1) has a monitoring assembly (10) for monitoring the first monitored region (11) and the second monitored region (14). The monitoring assembly (10) comprises at least one output device (25), which is designed and/or arranged to output an authorization signal (26) and/or a prohibition signal (27) regarding a change in a position and/or presence of at least one person in the first monitored region (11) and/or in the second monitored region (14).
In order to control a flow of persons and to implement distancing rules in a cabin (1) for an aircraft, a cabin (1) having a first monitored region (11) and a second monitored region (14) is provided. The cabin (1) has a monitoring assembly (10) for monitoring the first monitored region (11) and the second monitored region (14). The monitoring assembly (10) comprises at least one output device (25), which is designed and/or arranged to output an authorization signal (26) and/or a prohibition signal (27) regarding a change in a position and/or presence of at least one person in the first monitored region (11) and/or in the second monitored region (14).
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 47/02 - Aménagements ou adaptations des dispositifs de signalisation ou d'éclairage
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
19.
TOILET ARRANGEMENT FOR AN AIRCRAFT CABIN OF AN AIRCRAFT, AIRCRAFT HAVING THE TOILET ARRANGEMENT, AND METHOD FOR DRYING A STANDING SURFACE IN THE TOILET ARRANGEMENT
A toilet arrangement for an aircraft cabin of an aircraft having a cabin ventilation system for supplying the aircraft cabin with cabin air, includes at least one standing surface for cladding the toilet arrangement. The standing surface is disposed within the toilet arrangement. A ventilator has an entry interface for connection to the cabin ventilation system for transfer of the cabin air. An outlet element is connected to the entry interface for take-over of the cabin air. The ventilator generates a surface-air stream from the cabin air. The surface-air stream flows over the standing surface from the outlet element to dry the standing surface. An aircraft having the toilet arrangement and a method for drying a standing surface of the toilet arrangement are also provided.
INTERIOR SPACE MANAGEMENT SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING SAID INTERIOR SPACE MANAGEMENT SYSTEM, AND METHOD FOR CONTROLLING SAID INTERIOR SPACE MANAGEMENT SYSTEM
GP 665 CA RT/ND/dk ABSTRACT In passenger aeroplanes, baggage compartments for holding passengers' baggage are usually arranged above the rows of seats. It is the object of the invention to propose an interior space management system which is characterized by improved management of the aeroplane interior. For this purpose, an interior space management system (1) for an aircraft (2) is proposed, the aircraft (2) having a stowage compartment arrangement (6), the stowage compartment arrangement (6) having a plurality of stowage compartment sections (7), each for holding one or more baggage items (8), and having a control unit (16), the control unit (16) being designed to control and/or manage a distribution of interior regions of an interior space (3) of the aircraft (2), and the control unit (16) being designed to control and/or manage an occupancy of the stowage compartment sections (7) on the basis of historical data of the aircraft (2) and/or on the basis of baggage data of the baggage items (8). Figure 1 Date Recue/Date Received 2021-01-05
b, wherein the power transmitting device 5 and the power receiving device 6 are embodied as a power transfer arrangement 2 for supplying the power to a mobile terminal 4, wherein the power transmitting device 5 and the power receiving device 6 are designed to transfer power over a distance of several centimetres, wherein the power transmitting device 5 and the power receiving device 6 are deigned to set up a wireless and/or cordless supply connection segment 10 between the power transmitting device 5 and the power receiving device 6. In addition, an aircraft is proposed that comprises the cabin interior arrangement 1 comprising the power transfer arrangement 2 for supplying power to the terminal 4.
B64D 41/00 - Installations génératrices de puissance pour servitudes auxiliaires
B64D 11/06 - Aménagements ou adaptations des sièges
H02J 4/00 - Circuits pour réseaux principaux ou de distribution, la nature alternative ou continue du courant n'étant pas précisée
H02J 50/30 - Circuits ou systèmes pour l'alimentation ou la distribution sans fil d'énergie électrique utilisant de la lumière, p. ex. des lasers
B60Q 3/41 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules spécialement adaptés à des types spécifiques de véhicules pour les véhicules de transport en commun, p. ex. les bus
22.
CABIN INTERIOR ARRANGEMENT COMPRISING A POWER TRANSFER ARRANGEMENT FOR AN AIRCRAFT, AND AIRCRAFT COMPRISING THE CABIN INTERIOR ARRANGEMENT
ABSTRACT A cabin interior arrangement 1 for an aircraft is proposed that comprises a first cabin interior object and a second cabin interior object 3a, b, comprising a power transmitting device 5 for transmitting power from an aircraft electrical system 7, wherein the power transmitting device 5 is arranged on the first cabin interior object 3a, comprising a power receiving device 6 for receiving the power from the power transmitting device 5, wherein the power receiving device 6 is arranged on the second cabin interior object 3b, wherein the power transmitting device 5 and the power receiving device 6 are embodied as a power transfer arrangement 2 for supplying the power to a mobile terminal 4, wherein the power transmitting device 5 and the power receiving device 6 are designed to transfer power over a distance of several centimetres, wherein the power transmitting device 5 and the power receiving device 6 are deigned to set up a wireless and/or cordless supply connection segment 10 between the power transmitting device 5 and the power receiving device 6. In addition, an aircraft is proposed that comprises the cabin interior arrangement 1 comprising the power transfer arrangement 2 for supplying power to the terminal 4. Figure 1 Date Recue/Date Received 2020-12-02
An announcement device or a passenger aircraft contains a memory or announcements with assigned potential flight phases and a control and evaluation unit with inputs for input signals with information relating to flight phases of the passenger aircraft, an output for the announcements, wherein the control and evaluation unit is configured to determine a current flight phase on the basis of the input signals, to check whether an announcement for the current flight phase is present in the memory, and to output this announcement as the current announcement at the output.
A passenger aircraft contains the announcement device.
In a method for outputting an announcement, announcements and input signals are provided, a current flight phase is automatically determined from the said input signals and a possibly present associated current announcement is output.
A cabin management system of a passenger aircraft is used as an announcement device and/or to carry out the method.
An announcement device (4) for a passenger aircraft (2) contains a memory (6) for announcements (A1-3) with assigned potential flight phases (P1-3) and a control and evaluation unit (16) with inputs (8a-c) for input signals (10a-c) with information (12a-c) relating to flight phases (P1-3) of the passenger aircraft (2), an output (14) for the announcements (A1-3), wherein the control and evaluation unit (16) is configured to determine a current flight phase (AP) on the basis of the input signals (10a- c), to check whether an announcement (A-3) for the current flight phase (AP) is present in the memory (6), and to output this announcement (A1-3) as the current announcement (AA) at the output (14). A passenger aircraft (2) contains the announcement device (4). In a method for outputting an announcement (AA), announcements (A1-3) and input signals (10a-c) are provided, a current flight phase (AP) is automatically determined from the said input signals and a possibly present associated current announcement (AA) is output. A cabin management system (22) of a passenger aircraft (2) is used as an announcement device (4) and/or to carry out the method.
A device module for a galley of a passenger aircraft contains electrical consumers with a maximum total electrical power, a power input for an on-board power supply system of the passenger aircraft to feed in electrical input power, an energy storage device for energy from the power input for the consumers, and a control unit to limit the input power to a maximum value less than the maximum power, and to feed a power surplus of the input power to the energy storage device in order to feed additional power for consumers from the energy storage device.
A galley contains the device module.
In a method for operating the device module, the input power is limited to the maximum value, a power surplus is fed to the energy storage device, and additional power is fed to the consumers from the energy storage device.
A device module (6) for a galley (4) of a passenger aircraft (2) contains electrical consumers (8a-h) with a maximum total electrical power (PM), a power input (10) for an on-board power supply system (12) of the passenger aircraft (2) to feed in electrical input power (PE), an energy storage device (14) for energy from the power input (10) for the consumers (8a-h), and a control unit (20) to limit the input power (PE) to a maximum value (WM) less than the maximum power (PM), and to feed a power surplus (34) of the input power (PE) to the energy storage device (14) in order to feed additional power (36) for consumers (8a-h) from the energy storage device (14). A galley (4) contains the device module (6). In a method for operating the device module (6), the input power (PE) is limited to the maximum value (WM), a power surplus (34) is fed to the energy storage device (14), and additional power (36) is fed to the consumers (8a-h) from the energy storage device (14).
In a method for avoiding dazzling of a person (10) by a light source (6) arranged in an interior (20) of a vehicle (22), wherein the light source (6) during operation emits light (24) within a beam cone (26), a camera (4) is arranged in the interior (20) and oriented such that at least one monitoring section (28) of the beam cone (26), in which the person (10) can enter, is located in the field of view (30) of the camera (4), the camera (4) records a camera image (32), using machine person detection, it is ascertained from the camera image (32) whether at least one part of the person (10) is located within the beam cone (26), in this case, at least the region (18) of the beam cone (26) in which the part of the person (10) is located is switched to glare-free.
B60J 3/04 - Équipement anti-éblouissant combiné avec les fenêtres ou pare-brisePare-soleil pour véhicules réglable en transparence
B60Q 3/72 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet pour éviter l’éblouissement du conducteur
F21W 107/30 - Utilisation ou application de dispositifs d’éclairage sur ou dans des types véhicules spécifiques pour les aéronefs
F21W 106/00 - Dispositifs d’éclairage à l’intérieur des véhicules
In a method for avoiding dazzling of a person (10) by a light source (6) arranged in an interior (20) of a vehicle (22), wherein the light source (6) during operation emits light (24) within a beam cone (26), a camera (4) is arranged in the interior (20) and oriented such that at least one monitoring section (28) of the beam cone (26), in which the person (10) can enter, is located in the field of view (30) of the camera (4), the camera (4) records a camera image (32), using machine person detection, it is ascertained from the camera image (32) whether at least one part of the person (10) is located within the beam cone (26), in this case, at least the region (18) of the beam cone (26) in which the part of the person (10) is located is switched to glare-free.
G09G 5/00 - Dispositions ou circuits de commande de l'affichage communs à l'affichage utilisant des tubes à rayons cathodiques et à l'affichage utilisant d'autres moyens de visualisation
H04N 21/80 - Génération ou traitement de contenu ou de données additionnelles par un créateur de contenu, indépendamment du processus de distributionContenu en soi
B60Q 3/41 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules spécialement adaptés à des types spécifiques de véhicules pour les véhicules de transport en commun, p. ex. les bus
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
F21V 9/00 - Éléments modifiant les caractéristiques spectrales, la polarisation ou l’intensité de la lumière émise, p. ex. filtres
G01N 21/84 - Systèmes spécialement adaptés à des applications particulières
29.
Passenger cabin, lighting arrangement and operating method
A lighting arrangement for a passenger cabin of an aircraft is provided. The lighting arraignment has a display surface for displaying image content, at least two luminaires in a lighting environment of the display surface and a control unit. The luminaires radiate light in accordance with at least one lighting parameter. In the control unit, each luminaire is assigned part of the display surface as an evaluation region and a mapping rule. The mapping rule assigns image content of the evaluation region values of the lighting parameters. The control unit, for each of the luminaires, assigns the image content of its evaluation region values of its lighting parameters using the mapping rule and actuates the luminaires with the values with regard to the assigned lighting parameters. A passenger cabin having the lighting arrangement and a method for actuating the luminaires are also provided.
A lighting arrangement (20) for a passenger cabin (2) of an aircraft having a display surface (10) for image content (12) having at least two surface portions (14a- c) for content portions (16a-c) contains at least two luminaires (8) in a lighting environment (18) of the display surface (10) for light (22) in accordance with at least one lighting parameter (24), and a control unit (26) in which each luminaire (8) is assigned part of the display surface (10) as evaluation region (28) and a mapping rule (30), wherein the mapping rule (30) assigns image content (12) of the evaluation region (28) values of the lighting parameters (24), wherein the control unit (26), for each of the luminaires (8), assigns the image content (12) of its evaluation region (28) values of its lighting parameters (24) using the mapping rule (30) and actuates them with the values with regard to the assigned lighting parameters (24). A passenger cabin (2) contains the lighting arrangement (20) and the display surface (10), wherein the luminaires (8) are arranged in the lighting environment (18). In a method for actuating the luminaires (8), the image content (12) is depicted on the display surface (10), each of the luminaires (8) is assigned its evaluation region (28) and its mapping rule (30) and, for each of the luminaires (8), the image content (12) of its evaluation region (28) is assigned values of its lighting parameters (24) using the mapping rule (30), and each of the luminaires (8) is actuated with the values with regard to the assigned lighting parameters (24).
g) is a camera or a capacitive seat occupancy sensor.
A monitoring device (4) for a passenger aircraft (2) contains monitoring modules (6) and a monitoring unit (8), which is configured for at least two of the monitoring modules (6) together.
A passenger aircraft (2) contains a monitoring module (6) and/or a monitoring device (4).
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
H01M 8/0662 - Traitement des réactifs gazeux ou des résidus gazeux, p. ex. nettoyage
B64D 27/24 - Aéronefs caractérisés par le type ou la position des groupes moteurs utilisant la vapeur ou l'énergie de ressorts
B64D 31/00 - Systèmes de commande des groupes moteursAménagement de systèmes de commande des groupes moteurs sur aéronefs
H01M 8/04119 - Dispositions pour la commande des paramètres des réactifs, p. ex. de la pression ou de la concentration des réactifs gazeux avec apport simultané ou évacuation simultanée d’électrolyteHumidification ou déshumidification
34.
Ascertainment of predistortion data for a projection and projector module
In a method for ascertaining predistortion data (2) for a projection from a projector (4) onto a target surface (13) with known geometry data, a camera (10) is placed in a known relative pose (RKP) with respect to the projector and aligned toward the target surface (13), the relative pose of the camera with respect to the target surface (RKZ) is ascertained from a camera image by means of machine vision, and the relative pose (RPZ) of the projector (4) with respect to the target surface (13) is ascertained herefrom and from the relative pose (RKP), and the predistortion data (2) are ascertained on the basis of the geometry data and of the relative pose (RPZ) of the projector (4) with respect to the target surface (13).
A projector module (22) contains a calculation unit (3) for performing the method, and the projector (4) and the camera (10).
The camera (10) of the projector module (22) or in the method is used for optically monitoring the interior (5).
An interior camera is used as the camera (10) of the projector module (22) or in the method.
In a method for ascertaining predistortion data (2) for a projection from a projector (4) onto a target surface (13) with known geometry data, a camera (10) is placed in a known relative pose (RKP) with respect to the projector and aligned toward the target surface (13), the relative pose of the camera with respect to the target surface (RKZ) is ascertained from a camera image by means of machine vision, and the relative pose (RPZ) of the projector (4) with respect to the target surface (13) is ascertained herefrom and from the relative pose (RKP), and the predistortion data (2) are ascertained on the basis of the geometry data and of the relative pose (RPZ) of the projector (4) with respect to the target surface (13). A projector module (22) contains a calculation unit (3) for performing the method, and the projector (4) and the camera (10). The camera (10) of the projector module (22) or in the method is used for optically monitoring the interior (5). An interior camera is used as the camera (10) of the projector module (22) or in the method.
G03B 43/00 - Test du fonctionnement correct d'appareils photographiques ou de leurs pièces
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
G08B 13/196 - Déclenchement influencé par la chaleur, la lumière, ou les radiations de longueur d'onde plus courteDéclenchement par introduction de sources de chaleur, de lumière, ou de radiations de longueur d'onde plus courte utilisant des systèmes détecteurs de radiations passifs utilisant des systèmes de balayage et de comparaison d'image utilisant des caméras de télévision
36.
Reproduction appliance, reproduction structure, operating method and use
Disclosed is a reproduction appliance for a passenger cabin of an aircraft, for reproducing visual contents in the passenger cabin with a lighting device having luminaires, a control unit and a control line, wherein the control unit contains an instruction set of light instructions for actuating the luminaires, contains a memory for the contents to be reproduced, an interface to the control line and a decoder for receiving the light instructions having an association rule for associating control instructions for the reproduction appliance with the light instructions. A reproduction structure for the passenger cabin for reproducing the contents contains the reproduction unit and the lighting device. Also disclosed is a method for operating the reproduction appliance involves the contents being stored in the memory in a storage period and the reproduction appliance being controlled by means of light instructions in an operating period.
B60Q 3/60 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par les aspects optiques
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
H04N 9/31 - Dispositifs de projection pour la présentation d'images en couleurs
B60Q 3/70 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet
37.
REPRODUCTION APPLIANCE, REPRODUCTION STRUCTURE, OPERATING METHOD AND USE
A reproduction appliance (30) for a passenger cabin (4) of an aircraft (2), for reproducing visual contents (l) in the passenger cabin (4) with a lighting device (6) having luminaires (L), a control unit (8) and a control line (10), wherein the control unit (8) contains an instruction set (16) of light instructions (18) for actuating the luminaires (L), contains a memory (32) for the contents (l) to be reproduced, an interface (34) to the control line (10) and a decoder (36) for receiving the light instructions (18) having an association rule (38) for associating control instructions (40) for the reproduction appliance (30) with the light instructions (18). A reproduction structure (60) for the passenger cabin (4) for reproducing the contents (l) contains the reproduction unit (30) and the lighting device (6). A method for operating the reproduction appliance (30) involves the contents (l) being stored in the memory (32) in a storage period (ZS) and the reproduction appliance (30) being controlled by means of light instructions (18) in an operating period (ZB). Use of the lighting device (6) involves the reproduction appliance (30) being connected to the control line (10) and being actuated by the control unit (8) with the light instructions (18) as control instructions (40).
G09G 3/22 - Dispositions ou circuits de commande présentant un intérêt uniquement pour l'affichage utilisant des moyens de visualisation autres que les tubes à rayons cathodiques pour la présentation d'un ensemble de plusieurs caractères, p. ex. d'une page, en composant l'ensemble par combinaison d'éléments individuels disposés en matrice utilisant des sources lumineuses commandées
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
A method for setting up a projector (10) for a passenger cabin (4) of an aeroplane (2), wherein the passenger cabin (4) comprises a projection surface (14) with a known configuration (G) and the projector (10) in the passenger cabin (4) is in a known relative position (RP) with respect to the projection surface (14) in a mounting position (M), geometrical data (16) relating to the configuration (G) and relative position (RP) are received by the projector (10), and predistortion data (22) are determined from the geometrical data (16) according to an imaging rule (18) in order to predistort the images (12) and represent them as rectified images (12″) on the projection surface, and the projector (10) is set up by storing the predistortion data (22) in the projector (10).
A projector (10) contains an imaging rule (18) and an input (20) for geometrical data (16), and is configured to carry out the method according to the invention and, during operation when set up, to predistort images (12) with the aid of the predistortion data (22) and to project them.
A passenger cabin (4) having at least one projector (10) and at least one projection surface (14) has at least one of the projectors (10) according to the invention.
In a method for setting up a projector (10) for a passenger cabin (4) of an aeroplane (2), wherein the passenger cabin (4) comprises a projection surface (14) with a known configuration (G) and the projector (10) in the passenger cabin (4) is in a known relative position (RP) with respect to the projection surface (14) in a mounting position (M), geometrical data (16) relating to the configuration (G) and relative position (RP) are received by the projector (10), and predistortion data (22) are determined from the geometrical data (16) according to an imaging rule (18) in order to predistort the images (12) and represent them as rectified images (12") on the projection surface, and the projector (10) is set up by storing the predistortion data (22) in the projector (10). A projector (10) contains an imaging rule (18) and an input (20) for geometrical data (16), and is configured to carry out the method according to the invention and, during operation when set up, to predistort images (12) with the aid of the predistortion data (22) and to project them. A passenger cabin (4) having at least one projector (10) and at least one projection surface (14) has at least one of the projectors (10) according to the invention.
A method for allocating addresses to passenger service units (PSUs) and a service controller for a passenger cabin of an aircraft are provided. A coding device of the controller defines multiple coding parameters each corresponding to an installation position of a PSU. Each coding parameter defines a coding value. The PSUs are installed at respective installation positions in an installation space. A head unit of the controller communicates with the PSUs. In response to a start command, a respective coding value is determined at a respective installation position of a respective PSU. A respective waiting time is determined from the respective coding value according to a time rule. A response is transmitted to the head unit for each PSU upon expiration of the waiting time from the start command. Upon receiving the response, an address is allocated to a PSU which transmitted the response.
G06F 12/06 - Adressage d'un bloc physique de transfert, p. ex. par adresse de base, adressage de modules, extension de l'espace d'adresse, spécialisation de mémoire
G06F 13/42 - Protocole de transfert pour bus, p. ex. liaisonSynchronisation
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
41.
ADDRESS ALLOCATION TO PSUS, SERVICE ARRANGEMENT AND PASSENGER CABIN
In a method for allocating a respective address (Aa-e) to a plurality of PSUs (20a-e) of a service arrangement (12) for a passenger cabin (4) of an aircraft (2), a start command (40) is transmitted to all PSUs (20a-e), a respective coding value (Pa-e) of a coding parameter (P) is determined at an installation position (22a-e) of the respective PSU (20a-e), a respective waiting time (Wa-e) is determined from the coding value (Pa-e) according to a time rule (42), a response (Ra-e) is transmitted to a head unit (26) on expiry of the respective waiting time (Wa-e) and an address (Aa-e) is allocated to the responding PSU (20a-e) in response to the reception of the response (Ra-e). A service arrangement (12) for a passenger cabin (4) of an aircraft (2), with a coding means (14) extending along an extension line (16) in an installation space (18) for a plurality of PSUs (20a-e) and having different coding values (Pa-e) of a coding parameter (P) at different installation positions (22a-e) for PSUs (20a-e), with the PSUs (20a-e) with a head unit (26) which is connected to the PSUs (20a-e) via a communication channel (28) contains a control unit (29) to carry out the above method. In the case of a passenger cabin (4) of an aircraft (2) with the service arrangement (12), the PSUs (20a-e) are installed on a support structure (25) in the passenger cabin (4).
H04L 67/12 - Protocoles spécialement adaptés aux environnements propriétaires ou de mise en réseau pour un usage spécial, p. ex. les réseaux médicaux, les réseaux de capteurs, les réseaux dans les véhicules ou les réseaux de mesure à distance
H02J 4/00 - Circuits pour réseaux principaux ou de distribution, la nature alternative ou continue du courant n'étant pas précisée
G09G 3/34 - Dispositions ou circuits de commande présentant un intérêt uniquement pour l'affichage utilisant des moyens de visualisation autres que les tubes à rayons cathodiques pour la présentation d'un ensemble de plusieurs caractères, p. ex. d'une page, en composant l'ensemble par combinaison d'éléments individuels disposés en matrice en commandant la lumière provenant d'une source indépendante
B60N 2/02 - Sièges spécialement adaptés aux véhiculesAgencement ou montage des sièges dans les véhicules le siège ou l'une de ses parties étant mobile, p. ex. réglable
B60R 5/00 - Compartiments, à l'intérieur du véhicule, principalement destinés ou suffisamment spacieux pour loger des malles, des valises ou des objets analogues
G09F 9/30 - Dispositifs d'affichage d'information variable, dans lesquels l'information est formée sur un support, par sélection ou combinaison d'éléments individuels dans lesquels le ou les caractères désirés sont formés par une combinaison d'éléments individuels
B60N 2/90 - Détails ou éléments non prévus ailleurs
B64D 11/06 - Aménagements ou adaptations des sièges
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B60R 11/02 - Autres aménagements pour tenir ou monter des objets pour postes radio, de télévision, téléphones, ou objets similairesDisposition de leur commande
B61D 41/00 - Indicateurs de places réservéesÉcriteaux d'avertissement ou signes similairesDispositifs ou aménagements relatifs aux billets, p. ex. porte-ticketsPorte-étiquettes pour marchandises ou articles similaires
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
B63B 29/04 - Mobilier spécialement adapté aux navires
B60R 11/00 - Autres aménagements pour tenir ou monter des objets
An illumination arrangement of a passenger cabin for a passenger aircraft contains a control line with a connected lamp arrangement and operating unit having operating elements for selecting light scenarios of the lamp arrangement by transmitting dedicated control signals of the operating elements from the operating unit to the lamp arrangement via the control line, the lamp arrangement has a first decoder for allocating a sequence of control signals to a prescribed one of the light scenarios, the first decoder has a decoding instruction in a menu structure, the selection of menu elements of the menu structure is effected by the control signals, the illumination arrangement contains an add-on display which is connected to the control line, the add-on display contains a second decoder with the same decoding instruction, according to which a respectively received control signal is assigned a graphic representation of the menu element that is in each case currently selected by the control signals, the graphic representation which is in each case currently recognized is displayed on the add-on display.
In a method for producing a 2D image (18) of a 3D surface (2) on a viewing area (8) of a vision cone (12) which extends from a viewing position (14) to the 3D surface (2), wherein at least one marker location (20a,b) is assigned to the 3D surface (2), assigned to each image location (24) of the viewing area (8) is a depth dimension (T), which is correlated to the respective distance (A) between the viewing area (8) and the 3D surface (2) along a respective straight line (26) from the viewing position (14) through the image location (24) to the 3D surface (2), for at least one of the marker locations (20a,b) located within the vision cone (12), a marker field (28a,b) is produced in the 2D image (18), wherein the marker field (28a,b) in the 2D image (18) is placed as closely as possible to the image location (24a,b) of the marker location (20a,b), with the additional condition that all image locations (24) of the marker field (28a,b) have depth dimensions (T) which are greater than the depth dimension (Ta,b) of the image location (24a,b) of the marker location (20a,b), after placement of the marker fields (28a,b) a projection image (10) of the 3D surface (2) onto the viewing area (8) is placed therebehind in the 2D image (18).
In the case of a luminaire (2) for an interior (4) of a vehicle (6), comprising a main body (8) for securing to the vehicle (6), comprising at least one light source (10) secured to the main body (8), at least one of the light sources (10) is a matrix LED (12), wherein the matrix LED (12) comprises at least two mutually independently drivable LED pixels (14), and the LED pixels (14) are integrated on an LED chip. A matrix LED (12) is used as a light source (10) in a luminaire (2). A luminaire module (46), comprising at least one luminaire (2), wherein at least one of the luminaires (2) is a luminaire (2) according to the invention comprising a control input (44), and comprising a transducer (48) connected to the control input (44), contains a control and evaluation unit (49) for driving at least one of the matrix LEDs (12) via the control input (44) depending on the transducer (48).
F21S 2/00 - Systèmes de dispositifs d'éclairage non prévus dans les groupes principaux ou , p. ex. à construction modulaire
F21K 9/00 - Sources lumineuses utilisant des dispositifs à semi-conducteurs en tant qu’éléments générateurs de lumière, p. ex. utilisant des diodes électroluminescentes [LED] ou des lasers
B60Q 3/41 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules spécialement adaptés à des types spécifiques de véhicules pour les véhicules de transport en commun, p. ex. les bus
B60Q 3/85 - CircuitsAgencements de commande pour la commande manuelle de la lumière, p. ex. de la couleur, de l’orientation ou de l’intensité
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 47/02 - Aménagements ou adaptations des dispositifs de signalisation ou d'éclairage
47.
ASSEMBLY AND METHOD FOR AN AIRPLANE FOR TRANSMITTING AN ANALOG AUDIO SIGNAL
The invention relates to an assembly (2) for an airplane (4), comprising a line (12) and switching elements (14a, b). In order to connect the line (12) to digital transceivers (16a, b) in a first operating state (B1) and to an analog signal source/sink (18a, b) for the audio signal (A) in a second operating state (B2), the line (12) is operated as a digital data bus for data (D) in the first operating state (B1) and as an analog signal line for transmitting an analog audio signal (A) from the signal source (18a) to the signal sink (18b) in the second operating state (B2). In a corresponding method, the line (12) is operated as a digital data bus for transmitting data (D) in a first operating state (B1), the line (12) is switched to the second operating state (B2) in order to transmit the audio signal (A), and the audio signal (A) is transmitted from the signal source (18a) to the signal sink (18b) via the line (12).
The invention relates to an assembly (2) for an airplane (4), comprising a line (12) and switching elements (14a, b). In order to connect the line (12) to digital transceivers (16a, b) in a first operating state (B1) and to an analog signal source/sink (18a, b) for the audio signal (A) in a second operating state (B2), the line (12) is operated as a digital data bus for data (D) in the first operating state (B1) and as an analog signal line for transmitting an analog audio signal (A) from the signal source (18a) to the signal sink (18b) in the second operating state (B2). In a corresponding method, the line (12) is operated as a digital data bus for transmitting data (D) in a first operating state (B1), the line (12) is switched to the second operating state (B2) in order to transmit the audio signal (A), and the audio signal (A) is transmitted from the signal source (18a) to the signal sink (18b) via the line (12).
A transmission arrangement for an aircraft for transmitting data within the aircraft, wherein the aircraft includes an electrical wiring system of coherent lines for providing electric power for loads in the aircraft,
has at least two PLC elements, connectable to a respective one of the lines, for transmitting the data between at least two of the PLC elements via the wiring system, wherein at least one of the PLC elements has at least one filter connection, wherein the filter connection has at least one PLC connection, connectable to a respective one of the lines, and a power connection, connectable to a respective one of the lines, wherein the PLC connection carries power and data and the power connection carries power and is free of data.
In an aircraft having a transmission arrangement and having at least one wiring system, all the lines leading away from a coherent subsection of the wiring system have a PLC element having a filter connection, and the lines leading away are attached to a data-free PLC connection of the filter connection of the PLC element attached thereto such that the subsection of the wiring system is a data-carrying subsection that is delimited from the rest of the wiring system in terms of the data.
A transmission arrangement (2) for an aircraft (4) for transmitting data (D) within the aircraft (4), wherein the aircraft (4) includes an electrical wiring system (6) of coherent lines (8a-k) for providing electric power (E) for loads (10) in the aircraft (4), has at least two PLC elements (12a-g), connectable to a respective one of the lines (8a-k), for transmitting the data (D) between at least two of the PLC elements (12a-g) via the wiring system (6), wherein at least one of the PLC elements (12a-g) has at least one filter connection (20), wherein the filter connection (20) has at least one PLC connection (22a), connectable to a respective one of the lines (8a-k), and a power connection (22b), connectable to a respective one of the lines (8a-k), wherein the PLC connection (22a) carries power and data and the power connection (22b) carries power and is free of data. In an aircraft (4) having a transmission arrangement (2) and having at least one wiring system (6), all the lines (8a-i) leading away from a coherent subsection (34a,b) of the wiring system (6) have a PLC element (12a-g) having a filter connection (20), and the lines (8a-k) leading away are attached to a data-free PLC connection (22a) of the filter connection (20) of the PLC element (12a-g) attached thereto such that the subsection (34a,b) of the wiring system (6) is a data-carrying subsection (34a,b) that is delimited from the rest of the wiring system (6) in terms of the data (D).
H04B 3/56 - Circuits de couplage, blocage ou dérivation des signaux
B64D 41/00 - Installations génératrices de puissance pour servitudes auxiliaires
H04L 12/28 - Réseaux de données à commutation caractérisés par la configuration des liaisons, p. ex. réseaux locaux [LAN Local Area Networks] ou réseaux étendus [WAN Wide Area Networks]
51.
PrOx reactor and fuel cell arrangement comprising PrOx reactor
The invention relates to a PrOx reactor (R) comprising a housing that encloses a reaction space and has a first inlet (E1) for supply of a hydrogenous first gas (G1) to a reaction space, a second inlet (E2) for supply of an oxygenous second gas (G2) to the reaction space and an outlet (A) for discharge of a third gas (G3), wherein there is a multitude of conduits (Kv) extending from the second inlet (E2) into the reaction space, each of which comprises at least one opening (O) for supply of the second gas (G2) to the reaction space.
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
B01J 19/24 - Réacteurs fixes sans élément interne mobile
H01M 8/0668 - Élimination du monoxyde de carbone ou du dioxyde de carbone
B01J 12/00 - Procédés chimiques généraux faisant réagir des milieux gazeux avec des milieux gazeuxAppareillage spécialement adapté à cet effet
C01B 3/58 - Séparation de l'hydrogène ou des gaz contenant de l'hydrogène à partir de mélanges gazeux, p. ex. purification par contact avec des solidesRégénération des solides usés comportant une réaction catalytique
52.
Method of starting-up a fuel cell arrangement and fuel cell arrangement
H01M 8/04223 - Dispositions auxiliaires, p. ex. pour la commande de la pression ou pour la circulation des fluides pendant le démarrage ou l’arrêtDépolarisation ou activation, p. ex. purgeMoyens pour court-circuiter les éléments à combustible défectueux
H01M 8/04302 - Procédés de commande des éléments à combustible ou des systèmes d’éléments à combustible appliqués pendant des périodes spécifiques appliqués pendant le démarrage
H01M 8/04225 - Dispositions auxiliaires, p. ex. pour la commande de la pression ou pour la circulation des fluides pendant le démarrage ou l’arrêtDépolarisation ou activation, p. ex. purgeMoyens pour court-circuiter les éléments à combustible défectueux pendant le démarrage
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
H01M 8/04014 - Échange de chaleur par des fluides gazeuxÉchange de chaleur par combustion des réactifs
C01B 3/32 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par réaction de composés organiques gazeux ou liquides avec des agents gazéifiants, p. ex. de l'eau, du gaz carbonique, de l'air
B01J 23/63 - Métaux du groupe du platine avec des terres rares ou des actinides
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
The invention relates to an evaporator (V) comprising an evaporator body (3) surrounded by an evaporator housing (5) having an inlet (1) for supply of liquid into the evaporator housing (5) and an outlet (6) for discharge of vapour generated,
wherein the evaporator body (3) comprises a multitude of plates (7) arranged flat one on top of another,
wherein there is a liquid distributor (2) for distributing the liquid between the multitude of plates (7) arranged between the inlet (1) and the evaporator body (3),
wherein each of the plates (7) comprises, on a first surface, a liquid distributor structure (10) with distributor conduits (20, 21, 22), an evaporator area (11) and a gas collection structure (12).
The invention further relates to a corresponding fuel cell arrangement.
F28D 9/00 - Appareils échangeurs de chaleur comportant des ensembles de canalisations fixes en forme de plaques ou de laminés pour les deux sources de potentiel calorifique, ces sources étant en contact chacune avec un côté de la paroi d'une canalisation
F28F 3/04 - Éléments ou leurs ensembles avec moyens pour augmenter la surface de transfert de chaleur, p. ex. avec des ailettes, avec des évidements, avec des ondulations les moyens faisant partie intégrante de l'élément
F28F 13/08 - Dispositions pour modifier le transfert de chaleur, p. ex. accroissement, diminution en affectant le mode d'écoulement des sources de potentiel calorifique en faisant varier la section transversale des canaux d'écoulement
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
F22B 1/02 - Méthodes de production de vapeur caractérisées par le genre de chauffage par exploitation de l'énergie thermique contenue dans une source chaude
F22B 3/02 - Autres méthodes de production de vapeurChaudières à vapeur non prévues dans les autres groupes de la présente sous-classe comportant l'emploi d'un fluide énergétique autre que l'eau
F28D 21/00 - Appareils échangeurs de chaleur non couverts par l'un des groupes
F22G 1/00 - Surchauffe de la vapeur caractérisée par la méthode de chauffage
55.
Fuel processor component for a propylene glycol fuel processor and propylene glycol fuel processor
wherein the stacked first and second plates (P1, P2) form at least first cavities (H1) and second cavities (H2), wherein the first inlet (E1) has fluid connection to the first outlet (A1) via first cavities (H1) and the second inlet (E2) has fluid connection to the second outlet (A2) via second cavities (H2).
The invention further relates to a propylene glycol fuel processor.
H01M 8/00 - Éléments à combustibleLeur fabrication
H01M 8/06 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus
C10K 3/00 - Modification de la composition chimique des gaz combustibles contenant l'oxyde de carbone en vue de produire un carburant amélioré, p. ex. un carburant de pouvoir calorifique différent qui peut ne pas contenir d'oxyde de carbone
C10K 3/04 - Modification de la composition chimique des gaz combustibles contenant l'oxyde de carbone en vue de produire un carburant amélioré, p. ex. un carburant de pouvoir calorifique différent qui peut ne pas contenir d'oxyde de carbone par traitement catalytique réduisant le taux d'oxyde de carbone
C10L 1/02 - Combustibles carbonés liquides à base essentielle de composants formés uniquement de carbone, d'hydrogène et d'oxygène
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
H01M 8/0668 - Élimination du monoxyde de carbone ou du dioxyde de carbone
An evaporator comprising an evaporator body (3) surrounded by an evaporator housing (5), wherein the evaporator housing (5) is provided with a feed line (1) for feeding a liquid into the evaporator housing (5) and with an outlet (6) for emitting any vapour produced,
wherein each distributor line (VR) is connected to at least one void (8).
B01J 19/24 - Réacteurs fixes sans élément interne mobile
F28D 9/00 - Appareils échangeurs de chaleur comportant des ensembles de canalisations fixes en forme de plaques ou de laminés pour les deux sources de potentiel calorifique, ces sources étant en contact chacune avec un côté de la paroi d'une canalisation
F28F 9/02 - Boîtes de distributionPlaques d'extrémité
B01B 1/00 - ÉbullitionAppareils à ébullition en vue d'applications physiques ou chimiques
B01D 1/22 - Évaporation par amenée d'une pellicule liquide au contact d'une surface chauffée
The invention relates to a catalyst for the reforming of propylene glycol, comprising a support material (1) and a catalytic constituent (2), wherein the support material (1) is composed of one or more metal oxides, and the catalytic constituent (2) comprises at least one element selected from the following group: Rh, Ru, Pd, Pt and Ni.
C01B 3/32 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par réaction de composés organiques gazeux ou liquides avec des agents gazéifiants, p. ex. de l'eau, du gaz carbonique, de l'air
C01B 3/02 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène
58.
FUEL PROCESSOR COMPONENT FOR A PROPYLENE GLYCOL FUEL PROCESSOR AND PROPYLENE GLYCOL FUEL PROCESSOR
The invention relates to a fuel processor component for a propylene glycol fuel processor, comprising at least one housing (G) having at least two inlets (E1, E2) and two outlets (A1, A2),wherein there is a multitude of first plates (P1) having a first side (S1) and a second side (S2) and second plates (P2) having a third side (S3) and a fourth side (S4) arranged as a stack in the housing (G),wherein the stacked first and second plates (P1, P2) form at least first cavities (H1) and second cavities (H2), wherein the first inlet (E1) has fluid connection to the first outlet (A1) via first cavities (H1) and the second inlet (E2) has fluid connection to the second outlet (A2) via second cavities (H2).The invention further relates to a propylene glycol fuel processor.
C01B 3/32 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par réaction de composés organiques gazeux ou liquides avec des agents gazéifiants, p. ex. de l'eau, du gaz carbonique, de l'air
C01B 3/02 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène
C01B 3/48 - Production d'hydrogène ou de mélanges gazeux contenant de l'hydrogène par réaction de composés organiques gazeux ou liquides avec des agents gazéifiants, p. ex. de l'eau, du gaz carbonique, de l'air par réaction d'hydrocarbures avec des agents gazéifiants suivie par une réaction de la vapeur d'eau avec l'oxyde de carbone
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
The invention relates to an evaporator comprising an evaporator body (3) surrounded by an evaporator housing (5), wherein the evaporator housing (5) is provided with a feed line (1) for feeding a liquid into the evaporator housing (5) and with an outlet (6) for emitting any vapour produced, wherein the evaporator body (3) comprises a multiplicity of plates (7) which are arranged in a planar manner one above another, wherein a void (8) is formed in each case between adjacent plates (7), wherein each of the voids (8) is fluidically connected to the outlet, wherein a liquid distributor is interconnected between the feed line (1) and the evaporator body (3), wherein the liquid distributor branches off from the feed line (1) in the direction of the evaporator body (3) in at least two distributor lines (VR), and wherein each distributor line (VR) is connected to at least one void (8).
The invention relates to a method of starting-up a fuel cell arrangement (1) comprising a fuel processor (2) and a fuel cell (70), wherein the fuel processor (2) comprises the following components: a first evaporator (10), a reformer (20) arranged downstream of the first evaporator (10), a water-gas shift reactor (30), a PrOx reactor (40), a first heat exchanger (11), an afterburner (21) and a startup burner (50), wherein the method comprises the following steps: a) electrically heating a heating arrangement in the fuel processor (2) to heat a first gas (G1), b) heating the components of the fuel processor (2) to a fixed operating temperature by circulating the heated first gas (G1) through at least the first heat exchanger (11) and the afterburner (21), c) catalytically combusting an atomized or evaporated fuel (B) in the startup burner (50) and then afterburning hydrogen in the afterburner (21) for further heating of the first gas (G1) via at least one heat exchanger, d) introducing the fuel (B) into the preheated components of the fuel processor (2) and stopping the catalytic combustion in the startup burner (50), e) starting up at least one reaction in the components of the fuel processor (2), until an exit gas from a PrOx reactor (40) has a given CO content, and f) switching on the fuel cell (70). The invention further relates to a fuel cell arrangement.
H01M 8/04225 - Dispositions auxiliaires, p. ex. pour la commande de la pression ou pour la circulation des fluides pendant le démarrage ou l’arrêtDépolarisation ou activation, p. ex. purgeMoyens pour court-circuiter les éléments à combustible défectueux pendant le démarrage
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
The invention relates to an evaporator (V) comprising an evaporator body (3) surrounded by an evaporator housing (5) having an inlet (1) for supply of liquid into the evaporator housing (5) and an outlet (6) for discharge of vapour generated, wherein the evaporator body (3) comprises a multitude of plates (7) arranged flat one on top of another, wherein there is a liquid distributor (2) for distributing the liquid between the multitude of plates (7) arranged between the inlet (1) and the evaporator body (3), wherein each of the plates (7) comprises, on a first surface, a liquid distributor structure (10) with distributor conduits (20, 21, 22), an evaporator area (11) and a gas collection structure (12). The invention further relates to a corresponding fuel cell arrangement.
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
62.
PROX REACTOR AND FUEL CELL ARRANGEMENT COMPRISING PROX REACTOR
The invention relates to a PrOx reactor (R) comprising a housing that encloses a reaction space and has a first inlet (E1) for supply of a hydrogenous first gas (G1) to a reaction space, a second inlet (E2) for supply of an oxygenous second gas (G2) to the reaction space and an outlet (A) for discharge of a third gas (G3), wherein there is a multitude of conduits (Kv) extending from the second inlet (E2) into the reaction space, each of which comprises at least one opening (0) for supply of the second gas (G2) to the reaction space.
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
The invention relates to a method for producing electric energy by means of a fuel cell system operated using a reformate gas, said method comprising the following steps: preparing a fuel cell system with a first reactor (R1) for converting a fuel (B) into a first combustion gas (BG1) and a second reactor (R2) arranged downstream from the first reactor (R1), comprising a fuel cell surrounded by a protective housing (5), for producing electrical energy, forming a cathode exhaust gas (KA) and an anode exhaust gas (AA); preparing a gas separating device (1), by means of which the at least one partial gas mixture containing the gases CO2, N2 and/or a CO2 and N2 can be separated from the first combustion gas (BG1) or another gas mixture formed therefrom; supplying at least one part of the first combustion gas (BG1) or the other gas mixture formed therefrom to the gas separating device (1); separating the gases N2 or CO2 or the partial gas mixture from the first combustion gas (BG1) or the other gas mixture; supplying the separated gases N2 or CO2 or the separated partial gas mixture as an inert gas into the protective housing (5); and supplying a residual gas enriched with H2 as a second combustion gas (BG2) for operating the fuel cell or another fuel cell.
B64D 41/00 - Installations génératrices de puissance pour servitudes auxiliaires
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
H01M 8/0662 - Traitement des réactifs gazeux ou des résidus gazeux, p. ex. nettoyage
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
The invention relates to a method for producing electric energy by means of a fuel cell system operated using a reformate gas, said method comprising the following steps: preparing a fuel cell system with a first reactor (R1) for converting a fuel (B) into a first combustion gas (BG1) and a second reactor (R2) arranged downstream from the first reactor (R1), comprising a fuel cell surrounded by a protective housing (5), for producing electrical energy, forming a cathode exhaust gas (KA) and an anode exhaust gas (AA); preparing a gas separating device (1), by means of which the at least one partial gas mixture containing the gases CO2, N2 and/or a CO2 and N2 can be separated from the first combustion gas (BG1) or another gas mixture formed therefrom; supplying at least one part of the first combustion gas (BG1) or the other gas mixture formed therefrom to the gas separating device (1); separating the gases N2 or CO2 or the partial gas mixture from the first combustion gas (BG1) or the other gas mixture; supplying the separated gases N2 or CO2 or the separated partial gas mixture as an inert gas into the protective housing (5); and supplying a residual gas enriched with H2 as a second combustion gas (BG2) for operating the fuel cell or another fuel cell.
B64D 41/00 - Installations génératrices de puissance pour servitudes auxiliaires
H01M 8/0612 - Combinaison d’éléments à combustible avec des moyens de production de réactifs ou pour le traitement de résidus avec des moyens de production des réactifs gazeux à partir de matériaux contenant du carbone
H01M 8/0662 - Traitement des réactifs gazeux ou des résidus gazeux, p. ex. nettoyage
B64D 45/00 - Indicateurs ou dispositifs de protection d'aéronefs, non prévus ailleurs
65.
MONITORING MODULE FOR A SEAT OF A PASSENGER AIRCRAFT, MONITORING DEVICE AND PASSENGER AIRCRAFT
A monitoring module (6) for a seat (10) of a passenger aircraft (2), said seat containing at least one element (12a-g) having at least two states (Z1,2), comprises at least one sensor (14a-g) for the element (12a-g) with state information (16) corresponding to the current state (Z1,2), a read-out unit (18) having a communication channel (20) for the state information (16) for the sensor (14a-g) and a communication interface (22) for the state information (16) for a monitoring unit (8) of the passenger aircraft (2). The sensor (14a-g) is a camera or a capacitive seat occupancy sensor. A monitoring device (4) for a passenger aircraft (2) contains monitoring modules (6) and a monitoring unit (8), which is designed for at least two of the monitoring modules (6) jointly. A passenger aircraft (2) contains a monitoring module (6) and/or a monitoring device (4).
A monitoring module (6) for a seat (10) of a passenger aircraft (2), said seat containing at least one element (12a-g) having at least two states (Z1,2), comprises at least one sensor (14a-g) for the element (12a-g) with state information (16) corresponding to the current state (Z1,2), a read-out unit (18) having a communication channel (20) for the state information (16) for the sensor (14a-g) and a communication interface (22) for the state information (16) for a monitoring unit (8) of the passenger aircraft (2). The sensor (14a-g) is a camera or a capacitive seat occupancy sensor. A monitoring device (4) for a passenger aircraft (2) contains monitoring modules (6) and a monitoring unit (8), which is designed for at least two of the monitoring modules (6) jointly. A passenger aircraft (2) contains a monitoring module (6) and/or a monitoring device (4).
The invention relates to a method for inertizing an oxygen-containing first gas present in a protective housing (4) surrounding a fuel cell (1), wherein a prescribed amount of a hydrogen-containing second gas is introduced into the protective housing (4) and at least part of the oxygen present in the first gas is reduced by cold combustion.
H01M 8/04089 - Dispositions pour la commande des paramètres des réactifs, p. ex. de la pression ou de la concentration des réactifs gazeux
A62C 3/16 - Prévention, limitation ou extinction des incendies spécialement adaptées pour des objets ou des endroits particuliers dans les installations électriques, p. ex. chemins de câbles
A62C 3/07 - Prévention, limitation ou extinction des incendies spécialement adaptées pour des objets ou des endroits particuliers dans les véhicules, p. ex. les véhicules routiers
A62C 99/00 - Matière non prévue dans les autres groupes de la présente sous-classe
H01M 8/0662 - Traitement des réactifs gazeux ou des résidus gazeux, p. ex. nettoyage
68.
METHOD AND APPARATUS FOR INERTIZING AN OXYGEN-CONTAINING GAS
The invention relates to a method for inertizing an oxygen-containing first gas present in a protective housing (4) surrounding a fuel cell (1), wherein a prescribed amount of a hydrogen-containing second gas is introduced into the protective housing (4) and at least part of the oxygen present in the first gas is reduced by cold combustion.
H01M 8/0662 - Traitement des réactifs gazeux ou des résidus gazeux, p. ex. nettoyage
H01M 8/04223 - Dispositions auxiliaires, p. ex. pour la commande de la pression ou pour la circulation des fluides pendant le démarrage ou l’arrêtDépolarisation ou activation, p. ex. purgeMoyens pour court-circuiter les éléments à combustible défectueux
H01M 50/541 - Connexion de plusieurs conducteurs ou languettes d’électrodes empilées en forme de plaque, p. ex. barrettes ou ponts de pôles d’électrode pour accumulateurs au plomb
a, b), and/or, in at least one of the projectors (16), a surface region (20) of the projector (16) which is adjacent to the beam opening (18) is in the form of a second luminaire (21) having a second luminous area (22) for emitting light (8), the second luminous area (22) being part of the beam area (6).
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B60Q 3/40 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules spécialement adaptés à des types spécifiques de véhicules
F21W 105/00 - Combinaisons de dispositifs d’éclairage couverts par les groupes
The invention relates to an arrangement (1, 15), comprising a turbomachine (2, 16) with a compressor (3) having an outlet (7), and with a bleed air line (9), through which a leakage flow can flow and which is connected via a controllable valve (8) to the outlet (7) of the compressor (3), for supplying the leakage flow to a unit, characterized in that the unit is designed as a fan (17), jet pump (10) or pump which can be driven by the leakage flow. The invention also relates to a method for operating the arrangement (1, 15).
F02C 6/08 - Ensembles fonctionnels de turbines à gaz délivrant un fluide de travail chauffé ou pressurisé à d'autres appareils, p. ex. sans sortie de puissance mécanique délivrant des gaz comprimés le gaz étant prélevés sur le compresseur de la turbine à gaz
F02C 6/20 - Aménagements des ensembles fonctionnels de turbines à gaz pour l'entraînement des véhicules
F02C 7/22 - Systèmes d'alimentation en combustible
71.
Light program for interior lighting in an aircraft
G06F 19/00 - Équipement ou méthodes de traitement de données ou de calcul numérique, spécialement adaptés à des applications spécifiques (spécialement adaptés à des fonctions spécifiques G06F 17/00;systèmes ou méthodes de traitement de données spécialement adaptés à des fins administratives, commerciales, financières, de gestion, de surveillance ou de prévision G06Q;informatique médicale G16H)
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B60Q 3/74 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet pour l’éclairage général de l’habitacleAgencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet pour l’éclairage général de l’habitacle en combinaison avec un éclairage spécifique, p. ex. des lampes d’habitacle avec des lampes de lecture
72.
ARRANGEMENT COMPRISING A TURBOMACHINE, AND ASSOCIATED OPERATING METHOD
The invention relates to an arrangement (1, 15), comprising a turbomachine (2, 16) with a compressor (3) having an outlet (7), and with a bleed air line (9), through which a leakage flow can flow and which is connected via a controllable valve (8) to the outlet (7) of the compressor (3), for supplying the leakage flow to a unit, characterized in that the unit is designed as a fan (17), jet pump (10) or pump which can be driven by the leakage flow. The invention also relates to a method for operating the arrangement (1, 15).
F02C 6/08 - Ensembles fonctionnels de turbines à gaz délivrant un fluide de travail chauffé ou pressurisé à d'autres appareils, p. ex. sans sortie de puissance mécanique délivrant des gaz comprimés le gaz étant prélevés sur le compresseur de la turbine à gaz
B64D 13/06 - Aménagements ou adaptations des appareils de conditionnement d'air pour équipages d'aéronefs, passagers ou pour emplacements réservés au fret l'air étant climatisé
F02C 9/18 - Commande du débit du fluide de travail par prélèvement, par bipasse ou par action sur des raccordements variables du fluide de travail entre des turbines ou des compresseurs ou entre leurs étages
73.
LIGHT PROGRAM FOR INTERIOR LIGHTING IN AN AIRCRAFT
In a method for producing a light program for controlling lighting in an interior of an aircraft during a flight, a sequence list of phases of the day for a full day is set, wherein a time of day, a phase duration and lighting data for the lighting are assigned to each phase of the day, the appropriate phase of the day is selected from the sequence list as first program section of a flight program on the basis of the local time at which the flight starts and the proportional associated phase duration is assigned to the first program section as section duration, the appropriate phase of the day is selected from the sequence list as last program section of the flight program.
The invention relates to a modular assembly that comprises at least two housing parts (1), in which in each case a circuit board (L) is received, at least one internal connecting means (17), one cover element and one closing element. Each housing part (1) is formed from a base plate (3), a rear wall (5) and side walls (4) that are connected to said rear wall. The housing parts (1) are stacked in such a manner that the side walls (4) combine to form a first (6) and a second complete side wall (7), and that the rear walls (5) combine to form a complete rear wall (8). At least two of the housing parts (1) are stacked in such a manner that the base plate (3) of the one housing part (1) is connected to the side walls (4) of the other housing part (1). The at least one internal connecting means (17) extends in a direction perpendicular to the base plates (3) and connects multiple circuit boards (L) by way of first connectors (18). The cover element lies on the side walls (4) of precisely one housing part (1). The closing element is attached to a front side on the housing parts (1), said front side lying opposite the complete rear wall (8).
A voltage supply device for an aircraft control device having a first and a second main channel arrangement for redundancy and reliability, wherein the voltage supply device has a first and a second output transformer, wherein a first output inductor of the first main channel arrangement is designed as a primary winding of the first output transformer, and the second output inductor of the second main channel arrangement is designed as a primary winding of the second output transformer; and wherein the voltage supply device has at least a first secondary channel arrangement, wherein the first secondary channel arrangement has a first secondary voltage output and a first secondary winding of the first output transformer and a first secondary winding of the second output transformer, wherein the first secondary voltage output is connected to the first secondary windings which are connected in parallel.
H02J 1/12 - Fonctionnement de générateurs à courant continu en parallèle avec des convertisseurs, p. ex. avec un redresseur à arc de mercure
H02M 3/335 - Transformation d'une puissance d'entrée en courant continu en une puissance de sortie en courant continu avec transformation intermédiaire en courant alternatif par convertisseurs statiques utilisant des tubes à décharge avec électrode de commande ou des dispositifs à semi-conducteurs avec électrodes de commande pour produire le courant alternatif intermédiaire utilisant des dispositifs du type triode ou transistor exigeant l'application continue d'un signal de commande utilisant uniquement des dispositifs à semi-conducteurs
G05F 1/253 - Régulation de la tension ou de l'intensité là où la variable effectivement régulée par le dispositif de réglage final est du type alternatif utilisant des transformateurs montés en série ou en opposition comme dispositifs de réglage final les transformateurs comprenant plusieurs enroulements en série entre la source et la charge
H02J 1/00 - Circuits pour réseaux principaux ou de distribution, à courant continu
A light for an interior of a vehicle is provided. The light has two or more light modules. In an installed state, the light modules are mounted on a supporting structure in the vehicle and disposed in series along a profile line. In the installed state, each two adjacent light modules are fixedly attached to each other, such that all light modules that are fixedly attached to each other together form an integral light strip. The light strip has a first region and at least one second region. The first region of the light strip is fixedly attached to the supporting structure. The at least one second region of the light strip is movably supported on the supporting structure.
B60Q 3/78 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet pour créer des bandes lumineuses, p. ex. pour souligner le contour d’éléments d’habillage
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
F21V 21/005 - Soutien, suspension ou fixation des dispositifs d'éclairagePoignées pour plusieurs dispositifs d'éclairage disposés bout à bout, c.-à-d. rails de lumière
F21V 21/34 - Éléments de support déplaçables le long d'un élément de guidage
A light (2) for an interior (6) of a vehicle contains at least two light modules (4a-c) that are disposed in series along a profile line (12) and are mounted on a supporting structure (8) in the vehicle. Each two adjacent light modules (4a-c) are attached to each other in regions (14c). All light modules (4a-c) together form a light strip (17), which is attached to the supporting structure (8) with exactly one first region (14a), wherein a second region (14b) is movably supported on the supporting structure (8). A lighting system (20) contains a supporting structure (8) and the aforementioned light (2).
F21V 21/34 - Éléments de support déplaçables le long d'un élément de guidage
F21S 4/20 - Dispositifs ou systèmes d'éclairage utilisant une guirlande ou une bande de sources lumineuses avec les sources lumineuses maintenues par ou à l'intérieur de supports allongés
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 47/02 - Aménagements ou adaptations des dispositifs de signalisation ou d'éclairage
F21S 4/00 - Dispositifs ou systèmes d'éclairage utilisant une guirlande ou une bande de sources lumineuses
In a wall element for an interior of a vehicle, having a wall area to be illuminated and having an illuminating device which is used to illuminate the wall area, the illuminating device contains a plurality of lighting modules, wherein each of the lighting modules contains a multiplicity of light sources, wherein the lighting module extends straight along a central longitudinal axis and, in the direction of the central longitudinal axis, is placed against identical lighting modules without gaps at the ends, wherein the lighting module in operation has a cone of light which, by using a predefined area that is to be illuminated, extends away from the lighting module and the relative position (R) of which in relation to the lighting module is predefined, is configured in such a way that, on the part of the area that is illuminated by the cone of light, the result is a strip of light extending laterally transversely away from the lighting module, which extends at least over the entire length (L) of the lighting module, along the central longitudinal axis, wherein the wall area is the predefined area to be illuminated.
a,b), the deflection unit (12) can be varied in order to vary the form (Fa,b) and/or the intensity distribution (Ia,b) in the second cone of light.
a,b).
a,b).
B60Q 3/74 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet pour l’éclairage général de l’habitacleAgencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules caractérisés par leur objet pour l’éclairage général de l’habitacle en combinaison avec un éclairage spécifique, p. ex. des lampes d’habitacle avec des lampes de lecture
The invention relates to a modular assembly which comprises at least two housing parts (1), in each of which a circuit board (L) is received, at least one internal connection means (17), a cover element, and a closure element. Each housing part (1) is made of a base (3), a rear wall (5), and lateral walls (4) connected thereto. The housing parts (1) are stacked such that the lateral walls (4) complement each other so as to form a first (6) and a second complete lateral wall (7) and such that the rear walls (5) complement each other so as to form a complete rear wall (8). At least two of the housing parts (1) are stacked such that the base (3) of one housing part (1) is connected to the lateral walls (4) of the other housing part (1). The at least one internal connection means (17) extends in a direction perpendicular to the bases (3) and connects multiple circuit boards (L) via first connections (18). The cover element rests on the lateral walls (4) of precisely one housing part (1), and the closure element is attached to the housing parts (1) on a front face which is opposite the complete rear wall (8).
The invention relates to a modular assembly which comprises at least two housing parts (1), in each of which a circuit board (L) is received, at least one internal connection means (17), a cover element, and a closure element. Each housing part (1) is made of a base (3), a rear wall (5), and lateral walls (4) connected thereto. The housing parts (1) are stacked such that the lateral walls (4) complement each other so as to form a first (6) and a second complete lateral wall (7) and such that the rear walls (5) complement each other so as to form a complete rear wall (8). At least two of the housing parts (1) are stacked such that the base (3) of one housing part (1) is connected to the lateral walls (4) of the other housing part (1). The at least one internal connection means (17) extends in a direction perpendicular to the bases (3) and connects multiple circuit boards (L) via first connections (18). The cover element rests on the lateral walls (4) of precisely one housing part (1), and the closure element is attached to the housing parts (1) on a front face which is opposite the complete rear wall (8).
A voltage supply device having a first and a second main channel arrangement, wherein the voltage supply device has a first and a second output transformer, wherein a first output inductor of the first main channel arrangement is designed as a primary winding of the first output transformer and the second output inductor of the second main channel arrangement is designed as a primary winding of the second output transformer; and wherein the voltage supply device has at least a first secondary channel arrangement, wherein the first secondary channel arrangement has a first secondary voltage output and a first secondary winding of the first output transformer and a first secondary winding of the second output transformer, wherein the first secondary voltage output is connected to the first secondary windings which are connected in parallel.
H02M 3/338 - Transformation d'une puissance d'entrée en courant continu en une puissance de sortie en courant continu avec transformation intermédiaire en courant alternatif par convertisseurs statiques utilisant des tubes à décharge avec électrode de commande ou des dispositifs à semi-conducteurs avec électrodes de commande pour produire le courant alternatif intermédiaire utilisant des dispositifs du type triode ou transistor exigeant l'application continue d'un signal de commande utilisant uniquement des dispositifs à semi-conducteurs dans une disposition auto-oscillante
B64D 41/00 - Installations génératrices de puissance pour servitudes auxiliaires
H02J 1/10 - Fonctionnement de sources à courant continu en parallèle
H02M 1/08 - Circuits spécialement adaptés à la production d'une tension de commande pour les dispositifs à semi-conducteurs incorporés dans des convertisseurs statiques
H05K 10/00 - Dispositions pour améliorer la sécurité de fonctionnement d'un équipement électronique, p. ex. en prévoyant une unité de réserve similaire
Voltage supply systems for supplying control devices for an aircraft are made to be multiply redundant so that the failure of individual operative parts of the voltage supply system does not result in a total failure of the voltage supply and therefore of the control device. The invention addresses the problem of providing a voltage supply device, particularly for an aircraft control device, which functions in an operationally-reliable manner with a manageable number of components. According to the invention, a voltage supply device (4) is proposed which has a first and a second main channel arrangement (6a, b), said voltage supply device (4) comprising a first and a second output transformer (17a, b), a first output inductor (15a) of said first main channel arrangement taking the form of a primary winding (16a) of the first output transformer (17a), and the second output inductor (15b) of the second main channel arrangement (6b) taking the form of a primary winding (16b) of the second output transformer (17b), said voltage supply device (4) having at least one first auxiliary channel arrangement (18a) that comprises a first auxiliary voltage output N1, a first secondary winding (19a) of said first output transformer (17a), and a first secondary winding (19b) of said second output transformer (17b), the first auxiliary voltage output N1 being connected to said first secondary windings (19a, b) which are connected in parallel.
H02J 1/10 - Fonctionnement de sources à courant continu en parallèle
B60L 11/18 - utilisant de l'énergie fournie par des piles primaires, des piles secondaires ou des piles à combustibles
H02M 1/08 - Circuits spécialement adaptés à la production d'une tension de commande pour les dispositifs à semi-conducteurs incorporés dans des convertisseurs statiques
H02J 3/06 - Commande du transfert de puissance entre réseaux connectésCommande du partage de charge entre réseaux connectés
H02J 3/38 - Dispositions pour l’alimentation en parallèle d’un seul réseau, par plusieurs générateurs, convertisseurs ou transformateurs
H02J 7/00 - Circuits pour la charge ou la dépolarisation des batteries ou pour alimenter des charges par des batteries
H02J 7/02 - Circuits pour la charge ou la dépolarisation des batteries ou pour alimenter des charges par des batteries pour la charge des batteries par réseaux à courant alternatif au moyen de convertisseurs
H02M 3/338 - Transformation d'une puissance d'entrée en courant continu en une puissance de sortie en courant continu avec transformation intermédiaire en courant alternatif par convertisseurs statiques utilisant des tubes à décharge avec électrode de commande ou des dispositifs à semi-conducteurs avec électrodes de commande pour produire le courant alternatif intermédiaire utilisant des dispositifs du type triode ou transistor exigeant l'application continue d'un signal de commande utilisant uniquement des dispositifs à semi-conducteurs dans une disposition auto-oscillante
H02M 1/00 - Détails d'appareils pour transformation
a measuring circuit for measuring the instantaneous level of the detector current being connected in the control module in such a manner that, during the switched-off times of the PWM signal, the measuring circuit is connected to the LED lighting module via the signal transmission path such that the instantaneous level of the detector current can be measured using the measuring circuit and a functional state of the LED lighting module can be determined therefrom.
G05F 1/00 - Systèmes automatiques dans lesquels les écarts d'une grandeur électrique par rapport à une ou plusieurs valeurs prédéterminées sont détectés à la sortie et réintroduits dans un dispositif intérieur au système pour ramener la grandeur détectée à sa valeur ou à ses valeurs prédéterminées, c.-à-d. systèmes rétroactifs
A lighting apparatus for an AC voltage supply is provided. A rectifier module of the apparatus converts an AC voltage from the AC voltage supply into a rectified supply voltage. A diode cascade of the apparatus has multiple diode cascade sections connected in series and each having an LED. Each diode cascade section has a connectable bypass device for bypassing the diode cascade section. The diode cascade section is in an illuminated state when the bypass device is deactivated and a dark state when the bypass device is activated. A current source module is provided for stabilizing the cascade current through the diode cascade to a setpoint value. At least one diode cascade section has a control device, which has a switching device for converting the detected illuminated state into a switching signal for reducing the setpoint value.
B60Q 3/02 - Agencement des dispositifs d'éclairage pour l'intérieur des véhicules, leur montage, leur support ou les circuits à cet effet pour éclairage de l'habitacle des passagers ou du conducteur
H05B 33/08 - Circuits pour faire fonctionner des sources lumineuses électroluminescentes
86.
Energy unit, cabin movement and vehicle, as well as a method for supplying the cabin of a vehicle with a process material
The invention relates in particular to an energy unit (1) for producing an operating material on board a vehicle, comprising a fuel cell unit (2) with at least one fuel cell (3) and a mobile storage unit (5), which is formed separately from the fuel cell unit (2), with a store (6) for storing at least one energy source necessary for operation of the fuel cell unit (2). The mobile storage unit (5) and the fuel cell unit (2) can be coupled with one another, wherein, in the state coupled to one another, at least one first terminal (7) of the mobile storage unit (5) is connected to a corresponding second terminal (8) of the fuel cell unit (2) in such a way that at least the at least one energy source can be supplied from the store (6) to the fuel cell (3).
An LED lighting apparatus is provided. The apparatus has an LED luminous unit having multiple plurality LEDs and a switching arrangement. The LED luminous unit has different forward voltages in different switching states. The apparatus also has a control device for driving the LED luminous unit and a current sink device in a normal operating mode, in which the forward voltage and the LED current of the LED luminous unit are adapted to an instantaneous value of a supply voltage. An energy storage module of the apparatus provides a storage voltage and supplies the storage voltage to the LED luminous unit. The control device drives the LED luminous unit and the current sink device in a storage operating mode, such that the forward voltage and the LED current of the LED luminous unit are adapted to an instantaneous value of the storage voltage.
In comparison with thermal light sources, LED lighting has the advantage that it is very small and at the same time commercially available in different colors, so that colored lighting can be produced inexpensively and at the same time in a manner that saves installation space. It is an object of the present invention to equip an LED lighting apparatus with a color mixing functionality that is distinguished by high efficiency and at the same time a small number of components.
An LED lighting device for supplying a main voltage by an AC power supply is provided. The device has a rectifier for producing a rectified AC voltage from the main voltage, an LED light unit having multiple of LEDs and a circuit arrangement, and a control device for controlling the circuit arrangement. The circuit arrangement switches the LEDs to different circuit states, in which the LED light unit has different forward voltages. The control device controls the circuit arrangement, in such a way that the forward voltage of the LED light unit is adjusted to the voltage profile of the rectified AC voltage. The device also has a modelling device for modelling a modelled voltage profile. The control device controls the circuit states based on the modelled voltage profile. The modelled voltage profile is modelled based on measured variables for describing the real voltage profile of the main voltage.
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
35 - Publicité; Affaires commerciales
Produits et services
(1) (a) projection apparatus, namely, LCD projectors, video projectors, slide projectors, sound projections, picture projectors, projection screens; monitors, namely, LED monitors, video monitors, computer monitors; imaging apparatus, namely, cameras, video cameras, web camera, computer scanners; interactive terminals, namely, computers; television monitors; LCD monitors; tablet computer monitors; electric luminescent display panels, namely, computer display screens, liquid crystal displays; touch sensitive computer display and television screens; apparatus for the transmission of images, namely, computer software that allows transmission of graphics to mobile telephones; computer software for image processing; computerized three dimensional picture manipulators; computer central processing units for processing information, data, sound or images; audio mixers; amplifiers, namely, optical amplifiers, power amplifiers, signal amplifiers, sound amplifiers; sound processors; sound mixing apparatus, namely, sound mixers; audio amplifiers; audio processing apparatus, namely, audio transformers, software to control and improve audio equipment sound quality, vibration dampeners for electronic audio equipment; computer programs for editing images, sound and video; software for image and light projection; (b) aeronautical apparatus, machines and appliances, namely, airplane cabins and compartments (1) Advertising the goods and services of others; developing audio and visual promotional campaigns for business for others; advertising services for others in the field of the travel industry; marketing services in the field of arranging for the distribution of the products of others and producing promotional video tapes, video discs, and audiovisual recordings for others
91.
HOUSING FOR ELECTRONIC SYSTEMS AND METHOD FOR THE PRODUCTION THEREOF
An interface circuit (2) for intermediate connection between a logic circuit (6) and a power circuit (8), having a supply connection (10) for connection to a power supply (12), contains two logic connections (14a,b), which are configurable as logic input (24a) or logic output (24b), and two power connections (16a,b), which are configurable as power input (22b) or power output (22a), and a configuration unit (26) for the corresponding configuration, wherein the power input (22b) can be read by the logic output (24b) and the power output (22a) can be driven by the logic input (24a). An interface module (4), having at least two power connections (100a,b), contains at least one interface circuit (2), the power connections (16a,b) of which interface circuit are routed to the power connections (100a,b) of the interface module (4).
G05B 19/05 - Automates à logique programmables, p. ex. simulant les interconnexions logiques de signaux d'après des diagrammes en échelle ou des organigrammes
B64D 41/00 - Installations génératrices de puissance pour servitudes auxiliaires
H02J 13/00 - Circuits pour pourvoir à l'indication à distance des conditions d'un réseau, p. ex. un enregistrement instantané des conditions d'ouverture ou de fermeture de chaque sectionneur du réseauCircuits pour pourvoir à la commande à distance des moyens de commutation dans un réseau de distribution d'énergie, p. ex. mise en ou hors circuit de consommateurs de courant par l'utilisation de signaux d'impulsion codés transmis par le réseau
The present invention relates to an interface circuit for intermediate connection between a logic circuit and a power circuit, having a supply connection for connection to a power supply, contains two logic connections, which are configurable as logic input or logic output, and two power connections, which are configurable as power input or power output, and a configuration unit for the corresponding configuration, wherein the power input can be read by the logic output and the power output can be driven by the logic input.
The present invention further relates to an interface module, having at least two power connections, contains at least one interface circuit, the power connections of which interface circuit are routed to the power connections of the interface module.
H03K 3/00 - Circuits pour produire des impulsions électriquesCircuits monostables, bistables ou multistables
H03K 17/687 - Commutation ou ouverture de porte électronique, c.-à-d. par d'autres moyens que la fermeture et l'ouverture de contacts caractérisée par l'utilisation de composants spécifiés par l'utilisation, comme éléments actifs, de dispositifs à semi-conducteurs les dispositifs étant des transistors à effet de champ
H02M 1/38 - Moyens pour empêcher la conduction simultanée de commutateurs
H03K 19/0175 - Dispositions pour le couplageDispositions pour l'interface
H03K 19/173 - Circuits logiques, c.-à-d. ayant au moins deux entrées agissant sur une sortieCircuits d'inversion utilisant des éléments spécifiés utilisant des circuits logiques élémentaires comme composants
94.
Lighting strip for an aircraft interior and aircraft interior equipment with a plurality of lighting strips
A lighting strip for an aircraft interior is provided. The lighting strip has a connection for a network voltage, a rectifier for rectifying the network voltage into a power supply voltage, and a circuit board extending along a longitudinal extension of the lighting strip. Multiple LEDs are arranged on the circuit board and powered by the power supply voltage. A controllable current sink arrangement, having multiple individual sink devices connected electrically in parallel with one another, is provided for converting electrical energy transported via the connection into heat. The individual sink devices are distributed on the circuit board along the longitudinal extension of the circuit board. The sink devices are controlled by a control apparatus independently from the operative conditions of the LEDs to provide a homogenously distributed thermal profile of the lighting strip.
The invention relates to a reading lamp for installation in a cabin trim element (4) of a vehicle, in particular of an aircraft, comprising
an installation frame (1) having a ring element (2),
a lamp housing (7) having a mating support surface (8), and
a clamping ring (9)
wherein the clamping ring (9) is connected to the installation frame (1) by means of tension spring elements (10), such that the lamp housing (7) is forced against the support surface (6) of the inner surface of the ring element (2) by means of the clamping ring (9) and may be moved with respect to the installation frame (1) in the manner of a ball and socket joint.
09 - Appareils et instruments scientifiques et électriques
12 - Véhicules; appareils de locomotion par terre, par air ou par eau; parties de véhicules
35 - Publicité; Affaires commerciales
Produits et services
Projection apparatus; Monitors; Imaging apparatus; Interactive terminals; Television monitors; LCD monitors; Tablet monitors; Electric luminescent display panels; Touch sensitive electronic screens; Apparatus for the transmission of images; Apparatus for the processing of images; Three dimensional picture manipulators; Central processing units for processing information, data, sound or images; Audio mixing apparatus; Amplifiers; Sound processors; Sound mixing apparatus; Audio amplifiers; Audio processing apparatus; Computer programs for editing images, sound and video; Peripherals adapted for use with computers; Apparatus for the reproduction of images; Software. Aeronautical apparatus, machines and appliances. Advertising; Business promotion services provided by audio/visual means; Advertising services relating to the travel industries; Advertising, marketing and promotional services.
A lighting apparatus, in particular a reading lamp, is provided. The apparatus can be recessed in a trim of a passenger cab of a vehicle, which can be a land vehicle, an aircraft, or a watercraft. The apparatus has a first light-emitting device that is pivotably mounted to a recess-mounting frame, so that a light-emitting direction of the first light-emitting device with respect to the recess-mounting frame is changeable. To simplify the design of the apparatus, a second light-emitting device is mounted to a visible side of the recess-mounting frame. The second light-emitting device at least partially surrounds the first light-emitting device and is fitted to the recess-mounting frame, so that the light-emitting direction of the second light-emitting device is invariable.
B60Q 3/02 - Agencement des dispositifs d'éclairage pour l'intérieur des véhicules, leur montage, leur support ou les circuits à cet effet pour éclairage de l'habitacle des passagers ou du conducteur
B60Q 3/00 - Agencement des dispositifs d’éclairage pour l’intérieur des véhiculesDispositifs d’éclairage spécialement adaptés à l’intérieur des véhicules
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
Housing for at least one electric or electronic device, the housing surrounding a housing interior comprising a storage space, the electric or electronic device being arrangeable in the storage space, the housing comprising a housing upper part, which delimits the housing interior, the housing comprising at least one intermediate ceiling portion, which is arranged in the housing interior below the housing upper part and, together with the housing upper part, encloses at least one intermediate space, the intermediate ceiling portion having at least one cooling air passage, through which cooling air can flow from the storage space into the intermediate space, the housing upper part having at least one cooling air outlet, through which the cooling air can escape outwardly from the intermediate space, wherein the intermediate ceiling portion forms a catching arrangement for dripping water, which infiltrates the intermediate space through the cooling air outlet.
The invention relates to an arrangement having at least one metameric illuminating device (4) which comprises at least a first, second, third and fourth LED (6) and an internal controller (5) for changing the color rendering index of a light produced by additive color mixing of the first, second, third and fourth LED (6) with the aid of a prescribed color, having an external controller (8) for setting a parameter (K) influencing the color rendering index, and having a data transmitting device (7) for transmitting the parameter (K) to the internal controller (5) of the at least one metameric illuminating device (4).
B64D 47/02 - Aménagements ou adaptations des dispositifs de signalisation ou d'éclairage
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
G05F 1/00 - Systèmes automatiques dans lesquels les écarts d'une grandeur électrique par rapport à une ou plusieurs valeurs prédéterminées sont détectés à la sortie et réintroduits dans un dispositif intérieur au système pour ramener la grandeur détectée à sa valeur ou à ses valeurs prédéterminées, c.-à-d. systèmes rétroactifs
A method for controlling the authorization of a person to access a secure area, particularly a cockpit of a passenger aircraft, is provided. According to the method, an access control apparatus for detecting a set of biometric features is provided, which apparatus can be enabled by entering a predetermined access code. The access code is transferred by the person to the access control apparatus. The access control apparatus detects a set of biometric features of the person transferring the access code. The set of biometric features of the person are saved. Access for the person for a predetermined time period is subsequently enabled. Solely verifying the set of biometric features of the person seeking access allows access to be enabled again for the person during the predetermined time period.
G06K 9/00 - Méthodes ou dispositions pour la lecture ou la reconnaissance de caractères imprimés ou écrits ou pour la reconnaissance de formes, p.ex. d'empreintes digitales
G07C 9/00 - Enregistrement de l’entrée ou de la sortie d'une entité isolée
