[특허]Self-supporting cabin structure

Self-supporting cabin structure 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B04C-001/00 B64C-001/06 B64D-011/00
출원번호	US-0420761 (2009-04-08)
등록번호	US-9387920 (2016-07-12)
발명자 / 주소	Graeber, Ulrike Grosse-Plankermann, Peter Paetz, Martin
출원인 / 주소	AIRBUS OPERATIONS GMBH
대리인 / 주소	Ingrassia Fisher & Lorenz, P.C.
인용정보	피인용 횟수 : 0 인용 특허 : 29

초록

A cabin structural unit for attaching cabin installation elements is provided for an aircraft. The cabin structural unit is set up in such a way that a cabin installation element is attachable. The cabin structural unit is implemented as self-supporting and fastenable to an aircraft structure.

대표청구항 ▼

1. A cabin structural unit for attaching cabin installation elements for an aircraft, comprising: at least one first cabin structural segment arranged at a first side of the cabin structural unit to form a first sidewall of the cabin structural unit,at least one second cabin structural segment,and a third cabin structural segment arranged at a second side of the cabin structural unit, the third cabin structural segment forming a second sidewall of the cabin structural unit, the second side of the cabin structural unit located opposite the first side,the at least one second cabin structural segment coupled to the at least one first cabin structural segment to at least partially form a ceiling of the cabin structural unit;a hinge connected to the first cabin structural segment and to the second cabin structural segment such that the cabin structural unit is movable from a folded configuration to an unfolded configuration;a cabin installation element couplable to at least one of the first cabin structural segment and the at least one second cabin structural segment;a loose bearing device including a first rail directly fastened to a floor structure of the aircraft and a second rail directly fastened to the floor structure of the aircraft, the second rail spaced apart from the first rail in a cabin of the aircraft;wherein the cabin structural unit is self-supporting;wherein the at least one first cabin structural segment has a first end section and the third cabin structural segment has a second end section, the first end section received in the first rail and the second end section received in the second rail such that the cabin structural unit is fastened to the floor structure using the loose bearing device and the cabin structural unit is displaceable along a longitudinal axis of the aircraft; andwherein the first cabin structural segment is connected to the second cabin structural segment by the hinge such that the cabin structural unit can be preassembled outside a fuselage of the aircraft, folded together to reduce a distance between the first end section of the first cabin structural segment and the second end section of the third cabin structural segment such that the cabin structural unit in the folded configuration passes through an opening of the fuselage of the aircraft, the cabin structural unit in the folded configuration moved into the fuselage and unfolded. 2. The cabin structural unit of claim 1, further comprising: a plurality of support frames; anda longitudinal stiffening rib,wherein the longitudinal stiffening rib is installed between each of the plurality of support frames, andwherein the longitudinal stiffening rib is adapted for transmitting a force along an aircraft longitudinal axis. 3. The cabin structural unit of claim 1, further comprising a fastener, wherein the cabin installation element is replaceably fastenable to the cabin structural unit using the fastener. 4. The cabin structural unit of claim 1, wherein the cabin installation element is adapted for being formed integrally with the cabin structural unit. 5. The cabin structural unit of claim 1, wherein the cabin installation element is adapted to be installed on the cabin structural unit for transmitting a force flux. 6. The cabin structural unit of claim 1, wherein the cabin structural unit comprises a stiffening face. 7. The cabin structural unit of claim 6, wherein support frames of a plurality of support frames comprising a plurality of support elements, and wherein the plurality of support elements are removably fastenable to one another. 8. The cabin structural unit of claim 7, wherein the plurality of support elements are removably fastenable to one another using a plug-in connection. 9. The cabin structural unit of claim 1, wherein the cabin installation element is selected from the group consisting of toilet units, kitchen units, seat units, design elements, stairway elements, baggage compartments, air provision units or elevator units. 10. The cabin structural unit of claim 1, wherein the cabin structural unit further comprises interface elements; and the interface elements are adapted to connect the cabin installation elements with at least one of the aircraft structure or the floor structure. 11. The cabin structural unit of claim 1, wherein the cabin structural unit is adapted for supporting the aircraft structure. 12. The cabin structural unit of claim 1, wherein at least the first cabin structural segment, second cabin structural segment and third cabin structural segment provide the cabin structural unit to be self-supporting.

이 특허에 인용된 특허 (29)

Young,David A.; Fraker,Richard; Brauer,R. Klaus; Guard,Peter S., Aircraft archway.
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Young,David A.; Fraker,Richard; Brauer,R. Klaus; Guard,Peter S., Aircraft archway.
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Young,David A.; Fraker,Richard; Brauer,R. Klaus; Guard,Peter S., Aircraft archway architecture.
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Young,David A.; Fraker,Richard; Brauer,R. Klaus; Guard,Peter S., Aircraft archway architecture.
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Young,David A.; Fraker,Richard; Brauer,R. Klaus; Guard,Peter S., Aircraft archway architecture.
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Koefinger, Christian; Metzger, Joachim; Auburger, Michael, Aircraft component assembly system.
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Köfinger, Christian; Metzger, Joachim; Auburger, Michael, Aircraft frame element connected to an air-conditioning system.
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Graeber, Ulrike; Grosse-Plankermann, Peter; Pätz, Martin; Becker, Holger, Aircraft having a force transmission element between a cabin structural element and a primary structure.
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Guard,Peter S.; Young,David A., Aircraft interior architecture.
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Pompei Arturo (Rome WA IT) Winters Alden Bernard (Seattle WA), Aircraft interior ceiling panel assembly and attachment apparatus.
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Higgins William R. (Clearwater FL) Pobanz Otto C. (Cincinnati OH), Aircraft interior shell.
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Humphries David R. (Clearwater FL) Fetterhoff Donald C. (St. Petersburg FL) Higgins William R. (Clearwater FL), Aircraft shell module.
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Terwesten Ulrich,DEX, Arrangement for mounting fixtures such as baggage compartments near the ceiling or a passenger cabin, especially in an a.
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Wadey Bryan T. ; Yoerkie ; Jr. Charles A., Cabin interior panel system for reducing noise transmission in an aircraft.
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Manthey Heinz (Hamburg DEX) Glimmann Hans (Horneburg DEX) Tyburski Gustav (Stade DEX) Schultz Holger (Hamburg DEX) Probst Arne (Hamburg DEX) Poppinga Georg (Halstenbeck DEX) Nocon Guenther (Buxtehude, Ceiling luggage compartment combination for the passenger cabin of an aircraft.
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Ritts,Michael A; Davidson,Gregory W; Mills,Christopher J, Collapsible mobile platform interior structure.
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Schwinning, Melanie, Door frame component of cast titanium and structural fuselage part.
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Hart Jack E. (Bellevue WA) Leenhouts Michael J. (Bellingham WA), Extensions for storage bins.
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Koefinger, Christian; Metzger, Joachim; Auburger, Michael, Frame element, storage bin and method for installing a storage bin in an aircraft.
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Schwartz,Bruno; Tanguy,Richard; Quesnel,Jacques; Munch,Francis, Internal arrangement of the walls of the fuselage of an aircraft.
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Ritts, Michael A.; Davidson, Gregory W; Mills, Christopher J., Method for installing a collapsible mobile platform interior structure.
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Guard,Peter S.; Young,David A., Modular archway for an aircraft.
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Mills, Christopher J.; Whalon, Mark W., Modular offset aisle overhead crew rest.
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Bobzien, Phillip J.; Jacoby, Michael D.; Janes, Jeffrey S.; Dowdell, Robert M., Overhead lattice support structure.
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Arnold Alison M. (Island County WA), Removable aircraft floor structure-reinforcing strongback.
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Hart Jack E. (Bellevue WA) Burrows Ralph M. (Bellingham WA) Marquardt Michael E. (Seattle WA), Retrofit luggage bin assembly compatible with existing aircraft bin supports.
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Grosse-Plankermann, Peter; Pätz, Martin; Junge, Philipp, System and method for manufacturing a vehicle cabin.
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Sharma, Ravi; Haas, Daniel D.; Ricks, Theodore K., Thermally controlled fluidic self-assembly.
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White Thomas H. (26325 SE. 39th St. Issaquah WA 98027) Remedios Miguel A. (4900 222nd St. SE. Mountlake Terrace WA 98043), Universal cabin sidewall panel for aircraft.
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IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

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Self-supporting cabin structure 원문보기

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Self-supporting cabin structure 원문보기

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