摘要:
The invention relates to a device for creating an individually delimited zone (25) of a passenger cabin (1) in a means of transportation for at least one passenger seat (2). The device comprises a modular cabin element (10) which is attached to fixed guide rails (12) of the passenger seat (2) by way of quick release fasteners (11) so that the position of the element can be varied. Said cabin element (10) is allocated a pull-out, fixable sliding screen (17d) forming a flexible partition element, which extends from the underside of the hat rack (19) or the PSU panel (20) or the contour of the ceiling and in the lateral area in addition to the sidewall lining (31) of the passenger cabin (1) up to the modular cabin element (10), and by means of which an individually delimited zone (25) can be created.
摘要:
The present invention relates to a support device of cabin elements in an airplane. According to an exemplary embodiment of the present invention, a support device is provided into which a threaded bushing (7) can be screwed into a fastening element (6) in order to adjust the distance in z-direction of the airplane. Thus, a stepless adjustment is made possible in an advantageous way.
摘要:
The invention relates to an arrangement for dividing a space into a plurality of areas, said arrangement comprising at least one frame (4) with at least one fixing means (8) for holding the frame (4) in corresponding frame receiving elements, and at least one foldable defining means (6). The frame (4) is formed in such a way that the arrangement essentially fits onto at least one wall of the space when it is fixed, the foldable defining means (6) being able to be held on the frame (4) and preventing an air flow between adjacent areas of the space separated by the arrangement. The arrangement according to the invention enables a thermal separation of two adjacent areas of a space, that can each be air-conditioned differently, without forming an area containing air which is a mixture from two regions at different temperatures.
摘要:
The invention relates to a lightweight construction element, preferably a lightweight construction element for fastening partitions in airplane inner chambers having mounting points (2, 3) for fixing the lightweight construction elements in the airplane interior and a holding element (4) for the detachable fastening of a partition. With the objective of providing a lightweight construction element for fastening partitions, wherein said element not only has a lightweight design, but also has a design that offers the design engineer maximum design freedom, it is proposed according to the invention that the mounting points (2, 3) and the holding element (4) are connected to each other for the distribution of forces by way of laminate cups (5, 6, 7) forming the outer contour of the lightweight construction elements.
摘要:
An architectural archway (40) for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits (42, 44, 46, 48, 50), between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft.
摘要:
L'invention se rapporte à une cloison (2) pour aéronef destinée à séparer une partie cargo d'un cockpit ou d'un compartiment passager de cet aéronef, cette cloison (2) comportant une structure ondulée (30), définissant une pluralité d'ondulations (38) à section sensiblement en oméga s'étendant dans un sens de la hauteur de la cloison, cette dernière comprenant également un ou plusieurs éléments raidisseurs (60). L'invention concerne également un aéronef comportant au moins une telle cloison (2).