A lavatory monument configured to be positioned in an aircraft interior that includes an enclosure that includes first, second, third and fourth walls, and defines a lavatory interior, a first lavatory compartment that includes a first urinal unit positioned therein, and a second lavatory compartment that includes a second urinal unit positioned therein. The first lavatory compartment includes a first door and the second lavatory compartment includes a second door. A divider wall separates at least a portion of the first lavatory compartment from at least a portion of the second lavatory compartment. The first door is positioned on one of the first or second walls and the second door is positioned on one of the first or third walls.
A lavatory monument configured to be positioned in an aircraft interior that includes an enclosure that includes first, second, third and fourth walls, and defines a lavatory interior, a first lavatory compartment that includes a first urinal unit positioned therein, and a second lavatory compartment that includes a second urinal unit positioned therein. The first lavatory compartment includes a first door and the second lavatory compartment includes a second door. A divider wall separates at least a portion of the first lavatory compartment from at least a portion of the second lavatory compartment. The first door is positioned on one of the first or second walls and the second door is positioned on one of the first or third walls.
An aircraft overhead storage bin assembly that includes a housing, a door pivotably attached to the housing and a bucket pivotably connected to the housing that cooperates with the housing to define a bin interior. The housing includes a front, a back, and an upper storage section defined therein. The upper storage section includes an upper storage section opening that communicates the upper storage section with an exterior of the housing. The door pivotably attached to the housing and is movable between an open and a closed position. In the closed position the door closes the upper storage section opening. The bucket is positioned below the upper storage section and is pivotable with respect to the housing between an open position and a closed position.
A virtual control system that includes a control unit, a gesture recognition device, and a hologram generation device. The hologram generation device is configured to generate a hologram in a first volume of space. The gesture recognition device is configured to recognize a proper gesture within the first volume of space. The control unit is configured to send a signal to a component to be controlled when the gesture recognition device recognizes the proper gesture.
G03H 1/00 - Procédés ou appareils holographiques utilisant la lumière, les infrarouges ou les ultraviolets pour obtenir des hologrammes ou pour en obtenir une imageLeurs détails spécifiques
A baggage management system for a vehicle that includes a storage bin that defines a bin interior, a baggage monitoring system associated with the storage bin, and a display member associated with the storage bin. The baggage monitoring system is configured to monitor the positioning of baggage within the bin interior and the display member is configured to provide baggage positioning information to passengers.
Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.
A toilet assembly that includes a shroud portion, a main body portion extending generally forwardly from the shroud portion, and first and second intermediate protrusions extending generally forwardly from the bowl portion. The main body portion includes a bowl portion that includes a bottom and a top. The top includes an upper surface that defines a seat adjacent surface. The first and second intermediate protrusions are located vertically between the top and the bottom of the bowl portion and are configured such that a user can position their feet thereon.
A47K 17/02 - Supports pour le corps, autres que les sièges, pour les cabinets, p. ex. poignées, dossiers, repose-piedsAccessoires pour les cabinets, p. ex. tables pour lire
A47K 13/24 - Éléments ou parties constitutives non couverts dans les groupes ou sans rapport avec ces groupes
A panel assembly that is configured to be secured to a frame that includes a panel having a top and a bottom, a first bracket assembly and a second bracket assembly. The first bracket assembly includes a first pivot member and a first bracket. One of the first bracket and first pivot member is secured to the panel and the other is configured to be secured to the frame. The first bracket includes a slot defined therein that includes a throat and a pivot opening. The throat is defined between first and second throat surfaces and the throat is narrower than the pivot opening. The second bracket assembly includes a second pivot member and a second bracket. One of the second bracket and second pivot member is secured to the panel and the other is configured to be secured to the frame. The second bracket includes a pivot opening.
A hose mounting assembly that includes a mounting member having a base and a main body portion. The main body portion includes first and second ends, a curved tie tunnel defined therethrough, and a curved mounting surface. The base includes a first connection opening defined therethrough.
F16L 3/137 - Supports pour tuyaux, pour câbles ou pour conduits de protection, p. ex. potences, pattes de fixation, attaches, brides, colliers entourant pratiquement le tuyau, le câble ou le conduit de protection comportant un élément entourant pratiquement le tuyau, le câble ou le conduit de protection l'élément consistant en une bande flexible
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B65D 63/00 - Éléments d'emballage flexibles allongés, p. ex. courroies pour lier ou pour soutenir des objets
F16L 3/08 - Supports pour tuyaux, pour câbles ou pour conduits de protection, p. ex. potences, pattes de fixation, attaches, brides, colliers entourant pratiquement le tuyau, le câble ou le conduit de protection
F16L 3/12 - Supports pour tuyaux, pour câbles ou pour conduits de protection, p. ex. potences, pattes de fixation, attaches, brides, colliers entourant pratiquement le tuyau, le câble ou le conduit de protection comportant un élément entourant pratiquement le tuyau, le câble ou le conduit de protection
F16L 3/123 - Supports pour tuyaux, pour câbles ou pour conduits de protection, p. ex. potences, pattes de fixation, attaches, brides, colliers entourant pratiquement le tuyau, le câble ou le conduit de protection comportant un élément entourant pratiquement le tuyau, le câble ou le conduit de protection et s'étendant le long de la surface de fixation
F16L 3/233 - Supports pour tuyaux, pour câbles ou pour conduits de protection, p. ex. potences, pattes de fixation, attaches, brides, colliers spécialement adaptés pour supporter un certain nombre de tuyaux parallèles séparés par un espace pour un faisceau de tuyaux ou un ensemble de tuyaux disposés les uns à coté des autres en contact mutuel au moyen d'une bande flexible
11.
PIVOT BIN WITH LIFT ASSIST ASSEMBLY AND METHOD OF USE THEREOF
A method of pivoting an aircraft storage bin that includes a bucket that pivots with respect to an upper housing. The method includes pivoting the bucket from a closed position to an intermediate position and placing weight that exceeds a predetermined weight threshold in the bucket, thereby causing the bucket to move to an open position. Movement of the bucket to the open position causes a lift assist unit to activate. A first end of the lift assist unit is connected to the bucket and a second end of the lift assist unit is connected to the upper housing. The method also includes pivoting the bucket from the open position to the closed position. The lift assist unit provides assistance as the bucket is pivoting from the open position to the closed position.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
A47B 46/00 - Meubles à tiroirs, étagères ou rayonnages ayant une ou plusieurs surfaces susceptibles d'être amenées en position d'utilisation par extension ou pivotement
B60R 5/00 - Compartiments, à l'intérieur du véhicule, principalement destinés ou suffisamment spacieux pour loger des malles, des valises ou des objets analogues
A door latch assembly configured to be used in an aircraft lavatory door. The door latch assembly includes a housing that includes a housing interior, a switch member operatively associated with the housing that is rotatable between a first position and a second position, and a locking bolt that is movable linearly between an unlocked position and a locked position. Rotation of the switch member from the first position to the second position moves the locking bolt from the unlocked position to the locked position.
E05B 41/00 - Serrures à indication visible de la position de verrouillage ou de déverrouillage
G08B 5/02 - Systèmes de signalisation optique, p. ex. systèmes d'appel de personnes, indication à distance de l'occupation de sièges utilisant uniquement une transmission mécanique
G09F 7/14 - Caractéristiques structurelles des éléments portant ou formant les symboles
G09F 11/04 - Dispositifs d'affichage d'information variable, dans lesquels l'information complète est fixée d'une manière permanente sur un support mobile qui l'amène en position de présentation les éléments de présentation étant fixés à des organes animés d'un mouvement de rotation, p. ex. tambours, axes les éléments étant fixés à des disques animés d'un mouvement de rotation
G09F 19/04 - Moyens de publicité ou de présentation non prévus ailleurs comportant des organes de présentation mobiles fonctionnant par l'ouverture ou la fermeture de portes, p. ex. porte de magasin
A divider assembly that includes a main body portion having a lower section and an upper section and a removable panel having front and back surfaces. The upper section tapers in width in an upward direction and the main body portion includes front and back surfaces. The removable panel is removably secured to the upper section on the front surface of the main body portion.
A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a latch assembly that includes a striker assembly and a hook assembly, and a cable that extends between the paddle button assembly and the latch assembly. Movement of the button from the home position to the actuation position moves the cable, thereby disengaging the hook assembly and the striker assembly.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
E05B 53/00 - Fonctionnement ou commande des serrures par transmissions mécaniques, p. ex. à distance
E05C 1/12 - Dispositifs d'immobilisation avec pênes se déplaçant de façon rectiligne avec action d'une clenche avec poignée de manœuvre ou organe équivalent se déplaçant autrement que rigidement avec la clenche
An aircraft storage bin that includes an upper housing and a bucket that cooperate to define a bin interior. The bucket is movable with respect to the upper housing between open and closed positions and includes a bottom and right and left side panels. The bottom includes lower and upper surfaces and right and left outer edges. The right and left side panels each include a first section having a first transverse width, a second section having a second transverse width, and a transition section that is located between the first and second sections. The second transverse width is less than the first transverse width. At least a portion of the second section of each of the side panels is received in a slot defined in the upper surface of the bottom of the bucket, such that the right and left side panels extend upwardly from the bottom.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
F16B 5/00 - Jonction de feuilles ou de plaques soit entre elles soit à des bandes ou barres parallèles à elles
F16B 12/12 - Jointure des meubles ou objets similaires, p. ex. masquée de l'extérieur par chevilles, boulons, tenons, brides, clips ou dispositifs similaires pour éléments de meubles non métalliques, p. ex. en bois, en matériau plastique
A non-transitory machine-readable medium of a computing device storing an application for simulating the loading of an airframe. The application includes an airframe input module that receives an airframe file having a seat having a seat location and a bin having a bin location and a bin dimensions. The application further includes a passenger profile input module that receives a passenger profile file having a list of passenger profiles, a passenger selection module that selects a passenger from the list of passenger profiles and associates the passenger with the seat, a bag selection module that selects a bag profile from a bag profile file and associates it with the passenger, a bag placement module that simulates placing the bag into the bin based on the bin dimensions, bin location, and bag profile, and an output module that outputs and stores a simulation output associating the bag and the bin.
B60R 5/02 - Compartiments, à l'intérieur du véhicule, principalement destinés ou suffisamment spacieux pour loger des malles, des valises ou des objets analogues disposés à l'avant du véhicule
B64D 11/06 - Aménagements ou adaptations des sièges
B64F 1/30 - Installations au sol ou installations pour ponts d'envol des porte-avions pour l'embarquement ou le débarquement des passagers
G06F 17/30 - Recherche documentaire; Structures de bases de données à cet effet
G09B 9/08 - Simulateurs pour l'enseignement ou l'entraînement pour l'enseignement de la conduite des véhicules ou autres moyens de transport pour l'enseignement du pilotage des aéronefs, p. ex. bancs d'entraînement au pilotage sans visibilité
G09B 9/10 - Simulateurs pour l'enseignement ou l'entraînement pour l'enseignement de la conduite des véhicules ou autres moyens de transport pour l'enseignement du pilotage des aéronefs, p. ex. bancs d'entraînement au pilotage sans visibilité avec des moyens de simulation des forces générées par le vol ou par les moteurs sur l'occupant de l'aéronef
A switch system that includes a switch assembly with a housing having a bottom surface that includes a latch pocket defined therein. The latch pocket includes a top surface and the housing defines an interior that includes either a magnetic switch or a magnet disposed therein. One of the magnetic switch or magnet is positioned adjacent the top surface of the latch pocket in the other is associated with the distal end of latch bolt. The system also includes a latch bolt. When the latch bolt is in the unlatched position it is not received in the latch pocket, the magnetic switch is in the first state and an electrical component is in a first state. When the latch bolt is in the latched position it is received in the latch pocket, the magnetic switch is in the second state and the electrical component is switched to a second state.
An aircraft storage bin that includes an upper housing, and a bucket movable with respect to the upper housing between a closed position and an open position. The upper housing and the bucket cooperate to define a bin interior. The bucket includes a bottom and first and second opposing side walls. The bottom of the bucket includes an outer surface, an inner surface, a front edge, and first and second protrusions protruding into the bin interior. The first protrusion defines a first luggage engaging surface and the second protrusion defines a second luggage engaging surface.
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
A47B 46/00 - Meubles à tiroirs, étagères ou rayonnages ayant une ou plusieurs surfaces susceptibles d'être amenées en position d'utilisation par extension ou pivotement
An aircraft partition system that includes a first partition assembly having an attachment assembly configured to be secured to a first seat track, and a divider wall having first and second opposing sides and extending upwardly from the attachment assembly, where the divider wall is movable with respect to the carriage structure
A toilet module attachment assembly that includes a retainer member that is adapted to be secured to a wall. The retainer member includes a wall attachment flange and a press fit portion extending generally inwardly from the wall attachment flange. When the retainer member is secured to a wall a channel is defined between the wall and the press fit portion. The attachment assembly also includes a seal member that includes a bulge portion that is received in the channel of the retainer member.
A47K 17/02 - Supports pour le corps, autres que les sièges, pour les cabinets, p. ex. poignées, dossiers, repose-piedsAccessoires pour les cabinets, p. ex. tables pour lire
A computerized system for determining the design layout of an aircraft. The system includes an input module configured to receive a first input data indicating a first value of a first parameter, a first feature database that includes a plurality of feature settings, a feature search module configured to search the first feature database and select a feature setting based on the first value of the first parameter, a central database that includes a plurality of rules governing a design layout of a fuselage, and an optimizing module in communication with the central database and configured to generate an optimal design layout based on the selected feature setting.
A personal service unit pod assembly configured to be positioned in the interior of an aircraft. The personal service unit pod assembly includes a personal service unit pod and a panel positioned directly above and affixed to the personal service unit pod. The pod includes a housing with a lens assembly and a pod interior, a first reading light positioned within the pod interior and configured to shine light below the bottom of the housing, and cabin lighting positioned in the housing and configured to shine light through the lens assembly and above the housing. The panel includes connectors that are configured to secure the personal service unit pod assembly to a component within the aircraft.
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
23.
PIVOT BIN ASSEMBLY WITH MINIMAL FORCE REQUIRED FOR CLOSING
An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge, first and second opposing side walls extending upwardly from the bottom and a center of gravity. The bucket pivots about a pivot axis with respect to the upper housing between an open position and a closed position. The center of gravity of the bucket is positioned below the pivot axis when the bucket is in the closed position.
A47B 46/00 - Meubles à tiroirs, étagères ou rayonnages ayant une ou plusieurs surfaces susceptibles d'être amenées en position d'utilisation par extension ou pivotement
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
B64D 13/00 - Aménagements ou adaptations des appareils de conditionnement d'air pour équipages d'aéronefs, passagers ou pour emplacements réservés au fret
24.
CEILING PANEL ASSEMBLY AND MOUNTING SYSTEM THEREFOR
A module for mounting within a ceiling panel assembly. The module includes an upper mounting frame that includes a main body portion that defines a central opening, a lower mounting frame that is at least partially received in the central opening of the upper mounting frame, and a latch assembly. The main body portion of the upper mounting frame includes a flange extending outwardly therefrom. The lower mounting frame is pivotable with respect to the upper mounting frame between a first position and a second position. The latch assembly is associated with a first end of the upper mounting frame and the lower mounting frame. When the latch assembly is released the lower mounting frame pivots from the first position to the second position.
A door for an aircraft includes a first panel divisible into at least two first slats that are releasably connected to one another, a first tensioning cable attached between the at least two first slats, and a first tensioner connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.
A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly, and a first cable that extends between the paddle button assembly and the first latch assembly. Movement of the button from the home position to the actuation position moves the first cable, thereby disengaging the first hook assembly and the first striker assembly.
A method of positioning a monument within an aircraft. The method includes positioning first and second tracks having first and second carriages thereon on the floor. The first and second carriages are initially in a first position. The method includes positioning a floor of a first monument section with a first fitting on the carriage of the first track, positioning a floor of a second monument section with a second fitting on the carriage of the second track, moving the first and second monument sections with the carriages to a second position, aligning the first fittings with a connection point on the aircraft floor, raising the floors of the first and second monument sections and removing the first and second tracks, lowering the floors of the first and second monument sections, securing the first and second fittings to the connection points associated therewith.
A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side. The first and second sides are opposite to one another and the third and fourth sides are opposite to one another. The first lavatory defines a first lavatory interior and includes a first toilet therein and the second lavatory defines a second lavatory interior and includes a second toilet therein.
An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge and first and second opposing side walls extending upwardly from the bottom and pivots about a pivot axis with respect to the upper housing between an open position and a closed position. When the storage bin is installed in an aircraft, a first horizontal distance is defined between a first vertical line that extends through the pivot axis and the front edge of the bucket when the bucket is in the closed position, and a second horizontal distance is defined between the first vertical line and the front edge of the bucket when the bucket is in the open position. The first horizontal distance is greater than the second horizontal distance.
An aircraft lounge assembly that includes an enclosure having a rear wall, first and second side walls and a forward wall that cooperate to define a seating area. The lounge assembly also includes first and second seats positioned in the seating area, and a first dividing wall positioned between the first and second seats. The first dividing wall divides the seating area into a first seat section and a second seat section. The front wall includes a shared entrance space defined therein. A first seat path is defined between the shared entrance space and the first seat section and a second seat path is defined between the shared entrance space and the second seat section.
A toilet module attachment assembly that includes a retainer member that is adapted to be secured to a wall and a seal member. The retainer member includes a wall attachment flange and a press fit portion extending generally inwardly from the wall attachment flange. When the retainer member is secured to a wall a channel is defined between the wall and the press fit portion. The seal member includes a receiving portion having a groove defined therein and a bulge portion that is received in the channel of the retainer member.
A47K 11/00 - Cabinets sans chasse d'eauUrinoirs sans chasse d'eauPots de chambreChaises avec vase de toilette ou spécialement adaptées pour être utilisées avec une cuvette de toilette
B64D 11/00 - Arrangements pour passagers ou équipageInstallations de postes de pilotage non prévues ailleurs
A door module for a vehicle lavatory that includes a bi-fold door having a first panel and a second panel each having an inner surface and an outer surface. The first and second panels are pivotably connected together by a living hinge. The living hinge includes a hinge member that extends between first and second securing members, wherein the first securing member extends along and is attached to an inner edge of the first panel and the second securing member extends along and is attached to an inner edge of the second panel.
A fastener system that includes a female fastener assembly with a housing having a channel defined therein and a switch member movable within the channel between removing and fastening positions. The switch member includes a receiver portion having a post opening defined therein and a switch portion. The housing includes a lower opening. The post opening includes a removing portion that is aligned with the lower opening when the switch member is in the removing position and a fastening portion that is aligned with the post opening when the switch member is in the fastening position. The system also includes a male fastener assembly having a post with a slot therein. The post is received through the lower opening in the housing and the post opening so that the slot is aligned with the channel. The slot receives a portion of the receiver portion when the switch member is in the fastening position.
A panel assembly that includes a core having first and second opposing major surfaces, a first laminate skin secured to the first major surface of the core, a second laminate skin secured to the second major surface of the core, and at least a first layer of polyimide aerogel incorporated into one of the first laminate skin or the second laminate skin.
A method of bonding a first corrugated sheet and a second corrugated sheet to provide a honeycomb core assembly. The first corrugated sheet includes a plurality of lower node regions and the second corrugated sheet includes a plurality of upper node regions. The method includes applying a radio frequency activatable adhesive to one or both of a first lower node region of the first corrugated sheet and a first upper node region of the second corrugated sheet, positioning the first corrugated sheet adjacent to or in contact with the second corrugated sheet at the first upper node region and the first lower node region, and exposing the radio frequency activatable adhesives to a radio frequency to activate the radio frequency activatable adhesive, such that the first corrugated sheet is bonded to the second corrugated sheet.
B21D 47/00 - Fabrication d'éléments ou d'ensembles structurels rigides, p. ex. de structures en nid d'abeilles
B32B 3/00 - Produits stratifiés comprenant une couche ayant des discontinuités ou des rugosités externes ou internes, ou une couche de forme non planeProduits stratifiés comprenant une couche ayant des particularités au niveau de sa forme
B31D 3/02 - Fabrication d'articles de structure alvéolaire, p. ex. de panneaux d'isolation de réseaux en nids d'abeilles
B23K 13/00 - Soudage par chauffage au moyen d'un courant haute fréquence
A bracket that includes a main body portion having a first portion and a second portion that form a first angle therebetween. The first portion includes opposing front and rear surfaces and the second portion includes opposing upper and lower surfaces. The first portion includes a fastener opening defined therethrough, the second portion includes an insert feature extending from the lower surface, and the second portion includes at least one adhesive opening defined therethrough.
A door for an aircraft includes a first panel (58) divisible into at least two first slats (64-70) that are releasable connected to one another, a first tensioning cable (100) attached between the at least two first slats, and a first tensioner (124) connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.
A door for an aircraft includes a first panel (58) divisible into at least two first slats (64-70) that are releasable connected to one another, a first tensioning cable (100) attached between the at least two first slats, and a first tensioner (124) connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.
A lavatory monument assembly configured to be positioned in the interior of a vehicle. The lavatory monument assembly includes an enclosure that defines a first lavatory interior and includes at least a front wall and first and second side walls extending rearwardly from the front wall. The first lavatory interior includes a urinal positioned therein. The lavatory monument assembly also includes a first storage compartment positioned in the first lavatory interior. The first storage compartment includes a first storage door that is movable between an open position and a closed position. The front wall includes a first lavatory door that is movable between a closed and an open position and provides access to the first lavatory interior.
An aircraft monument that includes an enclosure with an enclosure interior,a compartment with a compartment interior positioned in the enclosure interior, and a stowable seat assembly disposed in the compartment. The compartment includes at least a first vertically oriented wall. The seat assembly includes a chair assembly with a back portion and a seat portion pivotably connected to the back portion along a seat pivot axis such that the seat is pivotable between closed and open positions. The chair assembly is movable between a stowed position where the seat pivot axis extends generally parallel to the first wall and the chair assembly is positioned in the compartment interior, and a deployed position where the seat pivot axis extends generally perpendicular to the first wall and the chair assembly is positioned outside of the compartment interior.
A computerized system for optimizing the design layout of an aircraft configured to execute, by at least one processor, the instructions of one or more software modules stored on a nonvolatile computer readable medium, the system comprising a first software module configured to receive input from a user regarding number of seats; a second software module configured to receive input from a user regarding seat pitch; a third software module configured to receive input from a user regarding meal service; a fourth software module configured to receive input from a user regarding beverage service; a fifth software module configured to comprise a listing of all possible combinations of all aircraft interior layout configurations for an aircraft. The sixth software module uses the inputs from one or more of the first, second, third, or fourth software modules to determine and create an output of the one configuration that takes up the least amount of seat space, weighs the least, and contains the most amount of aircraft cabin storage space. A seventh software module graphically displays the output of the sixth software module.
A modular lavatory monument assembly configured to be positioned in the interior of an aircraft. The modular lavatory monument assembly includes first, second, third and fourth walls that cooperate to form an outer shell that defines a lavatory interior. The fourth wall includes an alcove extending outwardly therefrom. The assembly also includes a sink module positioned in the alcove, a mirror module positioned above the sink module in the alcove, and a door positioned on one of the second or third walls.
A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.
A lighting assembly that includes an outer housing defining an outer housing axis, an inner housing defining an inner housing axis and a light member positioned in the inner housing. The outer housing includes a front surface having a front opening and an inner surface that defines an adjustment cavity having a truncated spherical shape. The inner housing has a truncated spherical shape and is at least partially received within the adjustment cavity. The inner housing defines a light recess therein and includes a front cover having an aperture defined therein. The front cover at least partially defines the light recess. The light member defines a light axis. The light axis and the inner housing axis are not co-axial and not parallel and form an angle therebetween. The inner housing is adjustable between a home position and a plurality of adjustment positions.
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
A partition configured to be positioned within an aircraft. The partition includes a first divider assembly that includes a first wall portion having a first jamb member secured to an inboard surface thereof and a first door hingedly connected to the first jamb member. The first jamb member includes first lighting that illuminates the first door, and the first door is movable between a stowed position and a deployed position. The partition also includes a second divider assembly that includes a second wall portion having a second jamb member secured to an inboard surface thereof and a second door hingedly connected to the second jamb member. The second jamb member includes second lighting that illuminates the second door, and the second door is movable between a stowed position and a deployed position. The second door is spaced apart from the first door.
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
A partition configured to be positioned within an aircraft. The partition includes a first divider wall having a first wall portion and a first divider assembly. The first divider assembly includes a first lighted member and first lighting for illuminating the first lighted member. The partition also includes a second divider wall that is spaced apart from the first divider wall. The second divider wall includes a second wall portion and a second divider assembly that includes a second, lighted member and second lighting for illuminating the second lighted member.
A graphics display module that includes a frame with a front portion and a rear portion that cooperate to secure a lighted panel having a front surface and a rear surface therebetween. The front portion defines a central opening through which the front surface of the lighted panel can be viewed. The front portion and rear portion cooperate to define a channel that includes lighting disposed therein that is configured to back light the lighted panel.
G09F 13/04 - Enseignes, tableaux ou panneaux éclairés de derrière l'illustration
G09G 3/36 - 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 utilisant des cristaux liquides
A lavatory monument assembly that includes an enclosure having at least a front wall and that defines an enclosure interior, and a divider wall that extends rearwardly from the front wall. The divider wall includes a divider door that is movable between closed and open positions. In the closed position the divider door divides the enclosure interior into a first lavatory' interior and a second lavatory interior. The front wall includes a first and second lavatory doors that are each movable between closed and open positions and provide access to the first lavatory interior and second lavatory interiors respectively. The front wall also includes a vertically extending center post. The second lavatory door is hinged!y connected to the center post, and the center post and the second lavatory door are slidable to a stowed position when the second lavatory door is in the open position.
A modular monument assembly configured to be positioned in an aircraft that includes an enclosure that includes a first module and a second module, and a circulation system that is adapted to receive water from a water source. The circulation system includes a circulation line for circulating water, a water heater, a circulation pump, first and second faucets and first and second lines that are in fluid communication with the first and second faucets. The first faucet is positioned in the first module and the second faucet is positioned in the second module.
A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of rib members formed, therein that extend inwardly. The rib members include an inner surface and an outer surface. A plurality of panel portions are defined between the plurality of rib members. The panel portions include an inner surface and an outer surface. The inner surface of the rib members are secured to the inner surface of the first panel, and the inner surface of the panel portions is spaced apart from the inner surface of the first panel to define at least first and second cavities.
A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated, with the first side panel and the bucket, and a second pivot mechanism operatively associated, with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along and are rotatable about a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.
A lavatory monument assembly configured to be positioned in the interior of an aircraft that includes first, second, third and fourth walls that cooperate to define a lavatory interior, a door positioned on one of the first, second, third and fourth wails that allows access to the lavatory interior, and a toilet positioned within the lavatory interior. The toilet defines a first vertical plane that bifurcates the toilet and is positioned such that the first vertical plane is not parallel to the first wall. At least the first wall is pivotal between a stowed position and an expanded position.
A damping mechanism that includes a housing with an inner circumferential surface defined by an assembly outer race, an axle shaft that is rotatable with respect to the housing, and a transmission assembly operatively associated with the axle shaft and disposed within the housing. The transmission assembly includes an assembly intermediate race. A fluid space that includes fluid therein is defined between the assembly intermediate race and the inner circumferential surface of the assembly outer race. A vane is disposed between the assembly intermediate race and the inner circumferential surface of the assembly outer race. The vane includes a restriction space defined therein.
A galley monument assembly that is configured to be positioned in the interior of an aircraft. The galley monument assembly includes a lower storage section that is adapted to receive at least one trolley cart and that includes a vertically oriented rear wall and two opposing side walls. The lower storage section defines a first storage depth. The galley monument assembly also includes an upper storage section that defines a second storage depth. The second storage depth is deeper than the first storage depth.
A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and. a panel positioned above and connected, to the PSU pod. The PSU pod includes at least first and second reading lights positioned, within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.
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 monument assembly configured to be positioned in the interior of an aircraft that includes a galley module, a first lavatory module and a second lavatory module. The galley module is positioned between the first and second lavatory modules, and the first lavatory module and the galley module share a first inboard dividing wall that includes at least a first non-vertical wall section.
A damping mechanism that includes a housing having fluid disposed therein and an inner circumferential surface, an axle shaft that is rotatable with respect to the housing, and a first vane having a distal end and being pivotally associated with the axle shaft. When the axle shaft rotates in a first direction, the first vane pivots to a deployed position, and when the axle shaft rotates in a second direction, the first vane pivots to a stowed position. A first clearance is defined between the distal end of the first vane and the inner circumferential surface of the housing when the first vane is in the deployed position, and a second clearance is defined between the distal end of the first vane and the inner circumferential surface of the housing when the first vane is in the stowed position. The second clearance is greater than the first clearance.
A lavatory monument assembly configured to be positioned in the interior of an aircraft that includes a first wall and a second wall that are generally parallel to one another, and the second wall is longer than the first wall The lavatory monument assembly further includes a third wall and a fourth wall, and the third wall and the fourth wall generally are perpendicular to the first wall and the second wall, and the third wall and the fourth wall connect to the first wall and the second wall to form a lavatory interior.
An aircraft that includes a cabin that has a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positioned fore of the first class section, an economy class section positioned in the interior and aft of the first class section, and a longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section. An economy class passenger that enters through the first door travels down the second aisle to enter the economy class section and never enters the first class section.
A passenger seating arrangement for an aircraft cabin that includes first and. second adjacent columns of at least two seats that define a first longitudinally extending center axis that extends approximately parallel to a longitudinal axis of the aircraft cabin. The seats in the first column face away from and form an angle with the first axis of between about 1 ° and about 44°, and the seats in the second column face away from and form an angle with the first axis of between about 1 ° and about 44°. Each seat in the first column is staggered fore of a seat in the second column.
A lounge assembly configured to be positioned in the interior of an aircraft. The lounge assembly includes a first seat shell configured to at least partially surround a passenger seat, and an overhead storage bin assembly. The overhead storage bin assembly includes first and second posts configured to be secured to a floor of the aircraft, and an overhead bin housing supported by the first and second posts. The overhead bin housing includes at least a first overhead storage bin that is positioned generally above the first seat shell.
A pod assembly for use in an aircraft that includes a seat with a seat bottom and a seat back, a shell that at least partially surrounds the seat, and a bed associated with the shell. The bed is movable between a stowed position and a deployed position where the bed is generally flat. The bed is supported by the shell in the deployed position.
A bin assembly that includes a bin housing and a bin that is pivotal between an open and a closed position within the bin housing. The bin housing includes a forward bulkhead panel, aft bulkhead panel and an aft housing panel that includes a rigid valence panel having one of a latch striker or a latch assembly secured thereto. The rigid valence panel has opposite ends that are secured to the forward and aft bulkhead panels. The bin includes an aft wall, a forward wall, a bin bottom and the other of a latch striker or a latch assembly secured to the bin bottom, thereby defining a latching location. A downward load in the bin is distributed from the latching location, along the rigid valence panel and to the aft and forward bulkhead panels.
Tubular bodies (106, 108) for use in frames for seats of vehicles such as aircraft are described. A tube (302) can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.
Fittings (10) configured primarily, although not necessarily exclusively, for connection, to- aircraft seat tracks (T) are detailed. The fittings may engage multiple openings (38) of a seat track concurrently. No rotation of a fitting need occur when connecting it to a track. Instead, if desired the fitting need move only linearly.
The present invention provides a beverage maker having an in-line heating assembly (12) for heating water to make hot beverages such as coffee and tea. The heating assembly defines a flow path (14) that runs past a plurality of heaters (16) for heating water to a desired temperature. In this manner, the beverage maker heats water as it travels, alleviating the need for a water tank or vessel, resulting in increased savings in weight and size, as well as reducing brew time. Additionally, an optical sensor assembly (80) is provided to detect when a serving container of the beverage maker has a prescribed capacity of liquid within it. The sensor assembly includes at least one light source (82) aligned to shine into the container and at least one detector (86) aligned to detect light reflected off the liquid surface within the container. A drainage assembly (70) is also provided that can drain liquid through either a connector port into an airplane's wastewater system or through a drainage port into a drainage sump.
A47J 31/34 - Appareils à préparer le café dans lesquels l'eau chaude passe sous pression à travers le filtre avec de l'eau chaude sous pression d'un liquide
A47J 31/44 - Éléments ou parties constitutives des appareils à préparer des boissons
brevets
