Abstract: A connecting element includes a first leg, a second leg and a third leg that are connected to each other and are each disposed at an angle to each other. The first leg includes a first fastening section and the second leg includes a second fastening section. A bending edge is disposed between the first leg and the second leg. The first leg includes at least one supporting section adjacent to the first section in a direction parallel to the bending edge, with the supporting section being connected to the second leg. The second leg forms an extension part in the first direction that is adjacent to the second fastening section, has a free end and is longer than the first fastening section of the first leg. The third leg is connected to the first leg and to the second leg.

Abstract: A supply system is provided that includes, but is not limited to a profile element. The profile element includes, but is not limited to a front wall, a rear wall, and webs between the front wall and the rear wall so that there are ducts within the profile element. The supply system also includes, but is not limited to at least one functional component integrated in at least one of the plurality of ducts.

Abstract: An aircraft galley waste bin extraction unit is disclosed having a first compartment formed by a plurality of walls that conform with walls of the waste bin, an extraction chamber adjoining the first compartment and sharing a common wall, and a platform within the common wall including a hinged bottom edge that allows the platform to pivot into a horizontal position against a rest on an extraction chamber side wall, the deploying of the platform forming a window through which the waste bin can pass through from the first compartment to the extraction chamber. The unit preferably also includes retractable ramp extendable from the platform to a ground surface to guide the waste bin from the extraction unit to the ground.

Abstract: Provided are stowage bin systems for use on aircrafts and other like vehicles. A stowage bin system may include two disjoint supporting panels and a stowage bin bucket disposed between and pivotally supported by these panels after installation. The supporting panels may be attached to vertical frame members and, in some embodiments, to other frame members, such as adjacent vertical frame members or to horizontal frame members. In some embodiments, a supporting panel may include a gusset extending substantially normal to the main surfaces of the panel. The gusset may provide additional rigidity to the panel and, in some embodiments, include one or more open channels for attaching to a horizontal frame member. The supporting panels transfer all loads generated during operation of the aircraft from the stowage bin bucket and to the fuselage or, more specifically, to vertical and other frame members.

Abstract: A passenger service unit (PSU) for a transport vessel has a unitary chassis with a plurality of apertures extending therethrough. Each one of the apertures is independently sized to receive at least one of a plurality of different modules. Each one of the modules includes one or more PSU fixtures having components different from other ones of the plurality of modules. A representative vessel is a passenger aircraft. Representative modules include vent and passenger reading light module, speaker module, passenger oxygen supply module and display module.

Abstract: An aircraft crew rest station includes an overhead crew rest portion including a central deck portion, forward and aft bunk portions, and a central entry vestibule connected between a passenger seating area and the central deck portion. The forward and aft bunk portions include a plurality of adjacent partitioned individual sleeping berths configured in interfitting alternating trapezoid shapes to optimize spatial accommodation of body proportions of crew members in the available aircraft space. The central deck portion includes an emergency escape hatch, a fold-down jump seat, and a fold-down entry door that removably covers a stairway of the central entry vestibule.

Abstract: A monument complex is provided for a rear area of a passenger cabin. The rear contour of the monument complex is adapted to the contour of the bulkhead so that an additional wash basin can be installed without there being any loss of space in the passenger cabin.

Abstract: A method for utilizing a plurality of overhead bins within a passenger cabin of an aircraft. Each overhead bin is partitioned to form multiple storage spaces therein, wherein a number of storage spaces is equal to at least a number of passenger seats within a seat row. Each storage space is designated with a space number to form a numbered space, wherein each space number is the same as an assigned seat number within the seat row. A passenger is assigned a seat number and thus the corresponding numbered space. Access to the numbered space is controlled such that only a cabin crew member or the passenger with the assigned seat number can open and close the numbered space.

Abstract: A compressor for pressurizing a flow of air within an aircraft including an inlet providing the flow of air to the compressor. An outlet provides the flow of air, after pressurization by the compressor, to a chamber of the aircraft. A diffuser assembly is disposed between the inlet and the outlet. The diffuser assembly includes one or more vanes at least partially impeding the flow of air through the diffuser assembly. A backing plate is included having a surface adjacent to the one or more vanes. The surface includes a relief feature that enables air to bypass the one or more vanes. The relief feature has an axial depth of about 0.5% to 2.5% of a width of a flow path through the diffuser assembly or of about 0.5% to 5% of a thickness of a flange of the backing plate. A method of operating a compressor is also included.

Abstract: An aircraft galley including a trolley stowage provided in a main body of the aircraft galley. A wall of the main body includes a first section delimiting the trolley stowage and a second section. The trolley stowage is convertible between a first operational state, wherein the trolley stowage is adapted to accommodate a first number of trolleys, and a second operational state, wherein the trolley stowage is adapted to accommodate a second number of trolleys. The second number of trolleys is greater than the first number of trolleys.

Abstract: An overhead bin for an aircraft comprises a base unit that is designed to fasten the overhead bin to a retaining structure of the aircraft, and a mounting unit that is connected to the base unit. By way of the mounting unit, a stowage space of the overhead bin can be accessed. The base unit provides a first stowage space region, and the mounting unit provides a second stowage space region that together with the first stowage space region forms the stowage space of the overhead bin.

Abstract: A passenger cabin for a means of transport is provided, which comprises an upper passenger deck and a lower passenger deck. The floor of the upper passenger deck comprises a lower and an upper region arranged therebeside, which are interconnected via a step or a ramp. There is an aisle in the lower region. The floor of the lower passenger deck likewise comprises a lower and an upper region arranged therebeside, between which there is a lowered aisle which is arranged so as to be laterally offset from the aisle of the upper passenger deck. The available surfaces of the upper and the lower passenger deck are mirror-symmetrically arranged. In this way, the space available can be used very effectively in order to accommodate more passengers.

Abstract: Embodiments of the present invention provide improved layouts that can increase space on-board aircraft and other passenger transport vehicles. The improved layouts may include two galley sections installed on an aircraft having a centerline and curved outer sidewalls. The first galley section can be positioned so that its longitudinal axis generally aligns with one of the outer sidewalls of the aircraft, and the second galley section can be positioned so that its longitudinal axis generally aligns with the longitudinal axis of the first galley. This can create a space along a rear side of the second galley section. The created space may be used for any number of options.

Abstract: The invention relates to an arrangement of a plurality of oxygen breathing devices, in particular for providing oxygen to passenger or crew of an aircraft, each oxygen breathing device comprising an oxygen source, wherein oxygen is stored, in particular in chemically bound form or compressed form, an oxygen guiding device for guiding oxygen from the oxygen source to a person. According to the invention, an arrangement of a plurality of oxygen breathing devices is provided, wherein a first one of said plurality of oxygen breathing devices further comprises an integrated transmitter comprising a sender adapted for wireless communication with a receiver of a second one of said oxygen breathing devices and a receiver adapted for wireless communication with a sender of said second oxygen breathing device.

Abstract: The invention relates to a system for providing emergency oxygen and therapeutic oxygen in an aircraft, said system having an oxygen source, an oxygen conduction system comprising a second oxygen outlet, a device for providing emergency oxygen comprising a second oxygen inlet, a device for providing therapeutic oxygen, having a first oxygen inlet and a first oxygen outlet. According to the invention, the second oxygen outlet can be coupled to the first oxygen inlet, the first oxygen outlet can be coupled to the second oxygen inlet and the second oxygen outlet can be coupled to the second oxygen inlet.

Abstract: A headrest includes a first part referred to as the lower part, equipped with a connecting unit enabling an adjustable connection of the headrest to the seat back of a pilot seat, and a second part referred to as the upper part, located opposite the lower part, as well as a front face intended to serve as a support surface for the head of a user. A receptacle, connected to the mask, stores an oxygen mask and/or a supply line. The upper part of the headrest forms a hinged cover on the lower part of the headrest and it closes the receptacle. A seat, a cockpit, and an aircraft include such headrest.

Abstract: Embodiments of the present invention provide snack and food dispensers on passenger transport vehicles, particularly aircraft, that will ensure fair distribution of self-serve snacks provided between meals and/or during flight in an organized, systematic, safe, and sanitary manner as well as allow a more accessible means for buying “Food for Purchase” items with less crew dependence for serving.

Abstract: The invention is based on a partition wall in an aircraft, wherein the partition wall comprises a support element and a tension-mounted material. According to the invention, the support element is composed of individually formed system components, and the tension-mounted material is supported by the support element such that an area-shaped partition wall is created in the aircraft.

Abstract: An aircraft cabin is provided that comprises an cabin interior space, a plurality of cabin enclosing surfaces, and a multifunctional support rail. The multifunctional support rail comprises a plurality of rail segments connected to each other forming a continuous rail arrangement. Further a number of first segments are provided as handrail in a first height, and a number of second segments is provided as a support handrail in a second height. The first height is in a waist region of a standing passenger, and the second height is in a shoulder or head region of a standing passenger. Still further, the first segments are connected with the second segments by a number of third segments provided as support handle running in a vertical direction.

Abstract: A decompression assembly (10; 10?) for an aircraft comprises a first cabin lining element (12; 12?) having a boundary area (14; 14?) and a second cabin lining element (20; 20?) having a boundary area (22; 22?), wherein the boundary area (22; 22?) of the second cabin lining element (20; 20?) is disposed at a smaller distance from an aircraft outer skin (24; 24?) than the boundary area (14; 14?) of the first cabin lining element (12; 12?). An air discharge opening (28; 28?) is disposed between the boundary area (14; 14?) of the first cabin lining element (12; 12?) and the boundary area (22; 22?) of the second cabin lining element (20; 20?) for discharging air from a cabin (18; 18?) of the aircraft into an area (30; 30?) of the aircraft located between the cabin lining elements (12, 20; 12?, 20?) and the aircraft outer skin (24; 24?).

Abstract: 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.

Abstract: An aircraft structure is provided with load-bearing hollow structural elements that form an aircraft fuselage. The cavities in the structural elements are designed as air ducts for an air conditioning system of the aircraft. An aircraft is also provided with such an aircraft structure.

Abstract: The present invention is directed to a luggage storage compartment for an aircraft having high ease of operation. Specifically, the luggage storage compartment comprises a housing and a housing container, with a drive device for moving the housing container between an open position O and a closed position C, with a closure apparatus for locking and unlocking the housing container in the closed position C, and with a control device for controlling the drive device, the control device being designed to actuate the drive device so that said drive device in a relief cycle guides the luggage container first into a relief region R and then into the closed position C, the closure apparatus being lockable or unlockable in a relieved state in the relief cycle.

Abstract: A lift assist mechanism is provided for assisting lifting of a movable component that can move between lowered and raised positions relative to a fixed structure. The lift assist mechanism includes a lift assist spring connected to a spring shaft, and an elongated track in which an end of the lift assist spring or an end of the spring shaft are movably engaged. A spring lock restrains movement of the spring shaft when a lift assist is not required, and releases the spring shaft when a lift assist is required.

Abstract: A method and apparatus for reconfiguring a lavatory area. An apparatus comprises a first lavatory area, a second lavatory area, a first door for the first lavatory area, and a second door for the second lavatory area. The first door and the second door are configured to move between an open position and a closed position. A single passageway is present in both the first lavatory area and the second lavatory area when the first door and the second door are in the open position.

Abstract: The invention relates to a cabin system for an aircraft fuselage, having one or more lining components for interior lining, and optionally one or more cabin equipment components, wherein the lining component can be installed either separately or in combination with a further lining component and/or a cabin equipment component under tension in the aircraft fuselage such that a cabin that is under tension in the circumferential direction and attaches to the aircraft fuselage is defined. In this manner a passenger cabin configured as a closed safety cell is created in a fuselage, which is of particular advantage in an aircraft fuselage made of a fiber composite material because no splinters or the like can penetrate the self-supporting passenger cabin in case of damage to the same.

Abstract: An aircraft galley is disclosed having a stand-alone beverage station and a stand-alone food preparation station. Each station is equipped with extendable work decks and integrated equipment for plug and play exchange. The beverage station is equipped with brewing stations and a top loading refuse compartment, and the food preparation station is configured with multiple ovens and refrigeration units. The galley further includes a side refrigeration unit which can be used as a self-service beverage area for passengers, and both stations may further be configured with LED displays for communicating with passengers.

Abstract: A method for displaying information by means of a dual-view-display in a passenger-cabin of an air-/spacecraft, comprising the following steps: providing the dual-view-display on a predetermined portion of the passenger-cabin; providing first information by means of the dual-view-display, in such a way that said information can be perceived from a gangway between rows of seats of the passenger cabin; and simultaneously providing second information, different from the first information, by means of the dual-view-display, in such a way that said information can be perceived from one of the rows of seats. A display device for displaying information in a passenger-cabin of an air-/spacecraft, comprising a dual-view-display which is arranged on a predetermined portion of the passenger-cabin, the dual-view-display being configured to provide first and second information in the above described ways. A passenger-cabin for an air-/spacecraft comprising said display-device.

Abstract: Luggage storage compartment for an aircraft, comprising a housing and a luggage container being mounted pivotably in the housing about a pivot axis A, and being transferrable with a first pivoting motion S1 from a closed position G into an open position Ö and the luggage storage compartment being opened, and being transferrable with a second pivoting motion S2 from the open position Ö into the closed position G and the luggage storage compartment being closed, the luggage storage compartment having a pivoting apparatus, comprising a cable winding device with a winding roll and with a winding medium, the pivoting apparatus comprising a drive device with a drive motor for driving the winding roll, an axis of rotation D of the winding roll running in the same direction as and/or parallel to the pivot axis A of the luggage container.

Abstract: The invention provides a method for adapting a seat row arrangement in an airplane in order to set seat row distances, wherein the currently desired pattern of seat row positions is stored in a control device and wherein the seat rows are mounted on seat tracks (4) extending in the longitudinal direction and can be locked therein against longitudinal movements by a locking mechanism (12, 13) associated with each seat row, wherein each seat row whose position is to be changed is, under control of the control device, unlocked by releasing the locking mechanism for the seat row, is moved automatically on its seat tracks to the predetermined position by operating drive means under the control of the control device, and is locked there on the seat tracks by the control device by actuating the locking mechanism, characterized in that at least one cable (6) which is extending in the longitudinal direction along the cabin is driven by a motor to move back and forth in a manner controlled by the control device, each s

Abstract: A modular integrated galley in a passenger vehicle, including a mounting rack in the form of a vertical wall including upper, middle and lower storage areas, at least one storage slot extending laterally between the middle and lower storage areas for storing a work surface therein, and a latch for ejecting the work surface at least partially from the slot into a position for being further extended into a fully deployed position by a user. An elongate hinge that extends vertically along a mounted edge of the doors and is adapted for allowing the door to move 180 degrees of travel between its closed and open positions is also disclosed.

Abstract: An aircraft has a ventilation system that employs a plurality of nozzles positioned in a cavity between a sidewall of the aircraft cabin and a section of the aircraft fuselage. The nozzles receive a supply of ventilation air and direct jets of air from the nozzles, through the cavity and into the aircraft cabin. The jets of air produced by the nozzles create low-pressure areas in the cavity. At least one return air opening in the cabin sidewall communicates the low-pressure areas with the cabin interior, whereby the low pressure areas draw air from the cabin interior into the cavity where the drawn air is entrained with the jets of air produced by the nozzles. Devices inside the cavity remove suspended impurities from the air drawn into the cavity. In this manner, the ventilation system filters or sanitizes the air drawn through the system.

Abstract: A galley cart is suspended from a rail or track that extends along the length of an aircraft cabin above the aisle and rows of passenger seats of the aircraft. The galley cart is automated to move along the track above the aisle in response to movements of a flight attendant that is serving passengers from the suspended galley cart. The galley cart is provided with open bins for storage of food products, a beverage dispenser that is operable by the flight attendant to dispense a beverage requested by a passenger from a plurality of different beverages available from the suspended cart, and an ice dispenser for serving ice with the beverages requested by the passengers.

Abstract: A shower unit for an aircraft comprises: a shower head, and controls to manually control the water output. A shower enclosure defines a receiving cavity to receive the user. The shower enclosure supports the shower head and the controls for the user to shower in the receiving cavity. The shower enclosure comprises a first door on a first side of the shower enclosure, and a second door on a second side of the shower enclosure to define a passageway through the shower enclosure. The shower unit is adapted to be positioned in the aircraft such that the passageway communicates between two separate zones of the aircraft.

Abstract: A chiller for an aircraft galley is disclosed having a housing defining an interior space, the housing including dividers to segregate the interior space into separate chambers. The chambers are enclosed by a pair of doors on a front of the housing that allow a user to gain access to the chambers, a first door providing access to at least one chamber and a second door providing access to at least one different chamber. A side door is also provided that permits access to at least one chamber, wherein at least one chamber is not accessible through said side door.

Abstract: The invention relates to a display device for an aircraft cabin, comprising a display adapted to display a plurality of stars. A further aspect of the invention is an aircraft cabin comprising such a display device and an aircraft cabin wall compartment comprising a plurality of wall sections and a plurality of light emitting means for individually illuminating each wall section, wherein said wall sections and said light emitting means form such a display device. According to the invention, said display is adapted to display a plurality of stars.

Abstract: The invention relates to an aircraft passenger service arrangement comprising one or more passenger service units for arrangement above a passenger seat, and a fixture member. The passenger service arrangement is characterized in that the fixture member is adapted for directly fixing the passenger service unit to a passenger seat in a defined relationship to each other. Further the invention relates to a seating device comprising an aircraft passenger service arrangement.

Abstract: A monument complex is provided for a rear area of a passenger cabin. The rear contour of the monument complex is adapted to the contour of the bulkhead so that an additional wash basin can be installed without there being any loss of space in the passenger cabin.

Abstract: An aircraft fuselage nose section having a secure access between the cockpit and the passenger cabin, while being compact. For that purpose, the nose section includes a separating mechanism including at least one movable element slidingly movable between: an extended closing position at which the separating mechanism bounds, with the cockpit door, a transition zone between the cockpit and the passenger cabin, and prevents people from passing between the passenger cabin and the transition zone; and a retracted opening position wherein the separating mechanism allows people to pass between the passenger cabin and the transition zone.

Abstract: A storage compartment configuration and an aircraft having a storage compartment configuration according to the invention are proposed. The storage compartment configuration has a storage compartment having a storage space and a suspension. The storage space is designed to receive pieces of luggage. The suspension is used for the attaching the storage compartment to a load-bearing structure of the aircraft. The suspension is designed in such a manner that the storage compartment can be pivoted essentially around a geometrical center point of the storage space.

Abstract: The invention relates to an aircraft comprising: a drainage system for condensation water formed in the aircraft between an upper zone thereof where the condensation water is formed and a lower zone where it is collected, a thermal insulation blanket (16) having two opposite faces, a first face (16a) of which is arranged facing the fuselage. The drainage system includes a drainage duct (18, 24) which extends into the upper zone along the second opposite face (16b) of the insulation blanket and which is connected to a pass-through device (30; 40) for the blanket placed beneath the upper zone. In this way, the drained condensation water passes through the blanket through the pass-through device and then is drained to the lower zone, between the first face of the blanket and the fuselage.

Abstract: An aircraft monument includes an elongate cavity having an open end and a lift apparatus mounted to the monument and adapted for lifting goods along the longitudinal axis of the cavity. The monument is adapted to be mounted on a floor structure of an aircraft separating two compartments of the aircraft from each other such that the open end of the cavity faces the floor structure. The lift apparatus includes a guide means including two straight guide members spaced apart, and extending parallel to the longitudinal axis of the cavity, a conveying means including two conveying members each mounted to a different guide member, a moving means for linearly moving the two conveying members, a control means for controlling the moving means to synchronize the linear movement of the conveying members, and a gripping means secured to the conveying means and adapted for selectively gripping and releasing goods.

Abstract: An aircraft galley, according to one implementation, includes a lighting system having a DC, linear LED task light that is positioned in a groove along the edge of an overhang above the galley's work surface. The task light is oriented downward orthogonally to the cabin floor so as to illuminate a work surface of the galley. In some implementations, the task light is angled so that it illuminates the work surface of the galley in which it is installed, the forward, aft, or cross-aisle opposing galley, if applicable, and the floor.

Abstract: An aircraft nose structure includes a fuselage and a pressuretight bulkhead fixed at its periphery to the fuselage and transversely dividing the fuselage into a pressurized upper zone and an unpressurized lower zone for accommodating retractable nose landing gear. The pressuretight bulkhead includes a floor of the pressurized upper zone, and a substantially flat rear panel extending between a rear edge of the floor and the fuselage. The floor and the rear panel are fixed laterally to the fuselage. The fuselage includes an exterior wall and reinforcing transverse frames to which the exterior wall is fixed. In line with the pressuretight bulkhead, at least some of the transverse reinforcing frames extend along the outline of the pressurized upper zone and constitute members that reinforce the pressuretight bulkhead.

Abstract: An internal wall in an aircraft cabin separates a lavatory and a galley of the aircraft. The internal wall has an intermediate notch that increases a lateral width dimension of the lavatory above the notch and thereby improves the spatial environment of the lavatory.

Abstract: 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.

Abstract: Disclosed herein is a divider utilized to provide part of a visual separation between sections of a passenger cabin of a commercial aircraft, the divider comprising several components. One component is a support arm fixedly connected to the frame of an aircraft above a passenger seat. Another component may be a curtain attached to a lower edge of the support arm and projecting vertically below the support arm. Yet another component may be a rigid view block adjacent the face of the luggage stowage compartment and configured to move therewith such that the view block is adjacent the face of the luggage stowage compartment while the luggage stowage compartment is in a closed position, and repositions with the face of the luggage stowage compartment when the compartment is opened.

Abstract: A separation device is provided for a vacuum toilet system of an aircraft, which makes possible a significantly simpler type of cleaning, which can be done more quickly, of a profile separator. The movably held combination of a wiping device and the profile separator can carry out a relative movement. As a result of mechanical contact between the wiping device and the profile separator the deposits are removed from the profile separator.

Abstract: An aircraft area comprises at least one main aisle which extends along a longitudinal axis of an aircraft cabin, a door aisle which extends, substantially perpendicularly to the at least one main aisle, along a transverse axis of the aircraft cabin between a first and a second aircraft door, and an aircraft monument which is arranged substantially centrally in the door aisle.

Abstract: An aircraft monument for installation in an aircraft cabin including a first functional module, the first functional module including a side wall for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module and/or from a region of the aircraft monument adjacent to the first functional module. The side wall is movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module.