Abstract: A network for an aircraft including a master device and slave devices connected in daisy-chain arrangement series. Each slave device has a unique identifier. The master transmits polling data packets along the slave devices, each including only one identifier. Polling data packets are transmitted in successive sequences, each including for each slave device only one polling data packet and including the polling data packets in a predetermined order. Each slave device includes a first data interface for connection in an upstream direction, a second data interface for connection in the downstream direction, and a processing unit to compare for each received polling data packet the identifier thereof with the identifier of the respective slave device, and output a response data packet to the master device if the two identifiers match, and forward the polling data packet to the second interface at least if the two identifiers do not match.

Abstract: In order to make available a space-saving sanitary unit having a toilet which offers improved user convenience to persons with restricted mobility, a cabin module for an aircraft is described which has a sanitary unit. The sanitary unit has a toilet cubicle with a toilet. The toilet cubicle is formed by four side walls and the toilet is arranged on a first side wall. A first access door is arranged in a second side wall, which extends transversely to the first side wall and adjoins the first side wall. A surface which is designed to at least partially accommodate a wheelchair is provided as an option within the toilet cubicle. The cabin module is configured to be installed with the second side wall transversely to a direction of flight. The first side wall 18a is aligned with an external wall in the installed state.

Abstract: A ram air channel arrangement for ambient air supply into an aircraft comprises a ram air channel which has a ram air inlet channel and a ram air outlet channel arranged downstream of the ram air inlet channel and in fluid communication with the ram air inlet channel. The ram air channel arrangement further comprises a cabin exhaust air line which is adapted to have cabin exhaust air flow therethrough which has been removed from an aircraft cabin and which cabin exhaust air line is connected to the ram air inlet channel and is adapted to lead the cabin exhaust air into the ram air inlet channel.

Abstract: A decompression assembly for use in an aircraft comprises a cabin lining element, an opening formed in the element, and an air channel arranged adjacent to a rear face of the element and connected to the opening. The air channel is provided with an air outlet which, during normal operation of the assembly, discharges air exiting a cabin region delimited by the element through the opening into an area located between the element and an aircraft outer skin, a first decompression opening, and a first decompression flap which, during normal operation of the decompression assembly, closes the first decompression opening in the air channel and which, in the event of a rapid decompression, opens the first decompression opening to allow a pressure equalization between the aircraft cabin region and the aircraft area located between the cabin lining element and the aircraft outer skin.

Abstract: An apparatus for continuously manufacturing components from fiber-reinforced composites comprises a conveying device, configured to convey a semifinished product containing reinforcing fibers through the apparatus, a forming device, configured to bring the semifinished product into a desired shape, and a press with a first pressing element and a second pressing element arranged opposite the first pressing element. The forming device further comprises a plurality of differently shaped molds that are pressurizable by the press, a mold application station arranged upstream of the press relative to the conveying direction of the semifinished product through the apparatus for applying a mold to a section of the semifinished product, and a mold release station arranged downstream of the press relative to the conveying direction of the semifinished product through the apparatus for releasing the mold from the section of the semifinished product.

Abstract: An aircraft structural component having a skin element, including an inner surface, a multitude of transverse stiffening elements, which lie against the inner surface of the skin element, and a multitude of longitudinal stiffening elements, perpendicular to the transverse stiffening elements against the inner surface of the skin element, wherein between a first and a second transverse stiffening element and also between a first and a second longitudinal stiffening element, a first skin section is defined. An aircraft structural component is provided with the quantity of the longitudinal stiffening elements reduced. A first applied reinforcement includes a core layer having a contour line running along the circumference of the skin element, the first applied reinforcement including a face sheet surrounding the core layer on the side thereof which faces away from the skin element, which face sheet is connected to the skin element along the core layer contour line.

Abstract: A rotary joint includes a socket rod having a socket rod flange with a basically spheroid concave bearing surface at a first end, a housing nut encircling the socket rod and having a threaded wrenching head, and a ball rod having a basically spheroid convex bearing surface and threaded side walls around the bearing surface. A diameter of the threaded side walls of the ball rod corresponds to a diameter of the threaded wrenching head of the housing nut. First guiding tracks are on the concave bearing surface oriented into a first swivelling direction, the socket rod being swivable to the ball rod along the first guiding tracks into the first swivelling direction. Second guiding tracks are on the convex bearing surface and oriented into a second swivelling direction, the socket rod being swivellable to the ball rod along the second guiding tracks into the second swivelling direction.

Abstract: An aircraft antenna assembly has a support element having a first and a second surface on opposite sides, an antenna element arranged on or in the support element, and a sealing device. The first surface and the sealing device are configured such that the antenna assembly is arranged on an outer skin section of an aircraft such that the first surface faces the outer skin section, the sealing device is situated between the support element and the outer skin section, and a cavity is defined by the sealing device, the outer skin section and the first surface. The support element or the sealing device y has a flow channel having a first and a second opening at opposite ends, the flow channel connecting the cavity and the environment and opening into the cavity at the first opening and opening into the environment at the second opening.

Abstract: An adapter for tapping into an aircraft panel network in order to provide support for a wireless flight attendant panel (FAP). The adapter includes first and second connectors to insert into the server-to-FAP connection of the panel network and a third connector configured to connect to a wireless access point. The adapter has a housing to which the first, second and third connector are mounted, wherein the housing accommodates power and data connections between the first and second connectors as well as a panel network access connection line between the first connector and the third connector, thereby enabling connection of the panel network to a wireless access point.

Abstract: A method, system and dispensing head for manufacturing a three-dimensional object by additive manufacturing. The three-dimensional object includes a three-dimensional component. The method provides a substrate and forming layers there-on, each layer formed in a pattern corresponding to a three-dimensional component being manufactured and each layer formed by dispensing a curable material from a nozzle of a dispensing head and subsequently curing the curable material. The three-dimensional object comprises the combination of the substrate and the three-dimensional component, wherein the substrate has a non-planar surface portion and the three-dimensional component is formed on the non-planar surface portion such that it is fixedly secured to the substrate.

Abstract: An aircraft air conditioning system includes an ambient air line connected to an air conditioning system mixer to supply ambient air, and a cabin exhaust air line connectable to an aircraft cabin for being flown through with cabin exhaust air. An ambient air compressor in the ambient air line compresses ambient air in the ambient air line. A refrigerating apparatus includes a refrigerant circuit and a refrigerant compressor in the circuit. The refrigerant circuit is thermally coupled to the ambient air line to transfer heat from ambient air line air to refrigerant circulating in the circuit before the ambient air is supplied to the mixer. A turbine is coupled to the air compressor. A control device controls the air conditioning system wherein in a first operating state the turbine receives air from the ambient air line, and in a second operating state receives cabin exhaust air.

Abstract: A system for moving loads comprising a cargo hold floor with a plurality of guide rails, and a plurality of transport vehicles removably received in the guide rails and being movable along the guide rails and which each comprise a carrier face movable perpendicularly to a surface of the cargo hold floor, between a first and a second operating position. The carrier face is arranged, in its first operating position, such that the transport vehicle received in a guide rail is positionable under a load which is deposited, at least partly, on the surface of the cargo hold floor. In its second operating position, the carrier face is arranged such that it lifts the load off the surface of the cargo hold floor and carries it. In the region of the carrier face, there are provided a plurality of rollers adapted to permit movement of the load parallel to the surface of the cargo hold floor.

Abstract: A galley monument having an integrated display arrangement includes a display; a display holder, by which the display is movably attached to the galley monument, wherein the display holder is designed as a rotary-pivot joint; and a receiving region, into which the display can be pivoted into a stowed state by the display holder; wherein the display can be rotated by the display holder in a state of use in order to set an orientation for use.

Abstract: A device for provision of oxygen masks has a container, which can be closed by a cover, for accommodating one or more oxygen masks, at least one extendable arm having an outer end, and a driving device. The outer end is coupled to at least one oxygen mask. The arm is designed to adopt a storage position, wherein the arm is arranged completely within the container, and an extended position, wherein the outer end is extended out of the container and the arm holds the at least one oxygen mask coupled thereto laterally at a distance from the container. For extension, the driving device is coupled to the arm. The arm has an end piece, on which a wound-up hose can be releasably fixed. A fixing device is formed on the end piece in such a way as to release the wound-up hose when the extended position is reached.

Abstract: Method and system for applying film to a plastic work piece to be cured, including providing a plastic work piece disposed on a surface of a base member, a free region remaining around the plastic work piece, an application frame having a frame housing with a frame opening and a frame edge enclosing the frame opening, and a film suitable for covering a plastic work piece during the curing thereof. Film is applied on the frame edge where the film covers the frame opening, and a lip region of the film is fastened to the frame edge. The application frame can move relative to the plastic work piece, where the plastic work piece passes through the frame opening until the frame edge, the lip region fastened thereto, is placed on the free region, wherein the film is deformed by the plastic work piece and rests against the plastic work piece.

Abstract: An aircraft interior door assembly (10, 20, 30) for selectively increasing usable space within an aircraft lavatory (1) adjacent a passenger doorway area (2) of the aircraft or in the passenger doorway area (2) adjacent the lavatory (1) comprises a door element (12, 22, 32) and a door element supporting structure (13, 23, 33). The door element (12, 22, 32) is rotatably mounted to the door element supporting structure (13, 23, 33) so as to be at least rotatable between first and second closed positions relative to the door element supporting structure (13, 23, 33). The door element (12, 22, 32) has the same configuration in both of its closed positions.

Abstract: A connection system has a first adhesion segment, on which a first connection region is formed, a second adhesion segment, on which a second connection region is formed, and a solidifiable liquid connection substance for connecting the two adhesion segments in a material fit, wherein at least one of the two connection regions is formed flexibly, such that, when the liquid connection substance is introduced between the two connection regions which are opposite one another in an assembly arrangement of the two adhesion segments, a material connection is formed between the two connection regions automatically as a result of the elastocapillary effect via the liquid connection substance.

Abstract: A seat rail cover includes a retaining section, configured to be introduced at least partially into a part of the seat rail, and a cover section, configured to cover the seat rail when the retaining section is introduced into the seat rail. At least the cover section of the seat rail cover is formed in one piece by 3D printing. Geometry, surface texture, color composition and/or color pattern of at least a visible part of the cover section in the installed state of the seat rail cover are matched to a surface and/or a floor covering of a floor element next to a seat rail to which the seat rail cover is connectable. Furthermore, a floor element with a seat rail and a seat rail cover as well as an aircraft with such a floor element. A method for manufacturing a seat rail cover by 3D printing.

Abstract: A foldable seat bench comprises a seat, a seat area and a backrest, and a carrier arrangement comprising a carrier element carrying the seat and at least one leg. The backrest is movable between a deployed position extending at an angle of approximately 70° to 110° relative to the seat area and a stowed position extending at an angle of approximately 0° to 20° relative to the seat area. The leg is foldable relative to the carrier element between a unfolded position and a folded position. The foldable seat bench comprises a first locking mechanism which, in a locking state, is adapted to lock the backrest of the seat in both its deployed position and its stowed position, and a second locking mechanism which, in a locking state, is adapted to lock the leg of the carrier arrangement in both its unfolded position and its folded position.

Abstract: An arrangement for producing a composite material component comprises a bagging configured to seal a receiving space for a semi-finished part against the ambient atmosphere. The bagging is a thermoformed bagging having a shape which, at least in sections, corresponds to a shape of the semi-finished part and which comprises an air-tight outer layer and an inner separation layer. The inner separation layer is configured to allow the bagging to be separated from the composite material component made from the semi-finished part. The arrangement further comprises a vacuum source connected to the receiving space and configured to generate a reduced pressure within the receiving space. The arrangement also comprises a curing apparatus configured to cure a thermoset plastic material either contained in at least one element of the semi-finished part or injected into the receiving space when the semi-finished part is sealed within the receiving space via the bagging.