公开(公告)号：EP3873809B1

公开(公告)日：2024-09-11

申请号：EP19880495.7

申请日：2019-10-29

IPC分类号： B64D11/06 ,  B64C1/14 ,  B64D11/00

CPC分类号： B64D11/0601 ,  B64D11/0023 ,  B64C1/1423

公开(公告)号：EP4375188A1

公开(公告)日：2024-05-29

申请号：EP23210015.6

申请日：2023-11-15

申请人： The Boeing Company

发明人： WORRASANGASILPA, Brian Danai ,  McINTOSH, Darren Carl ,  BURTON, Noah Hunter ,  HOLLAND, Liam ,  YOUNG, Christopher Kerry ,  COX, Kendall Marie ,  NGUYEN, Travis Hoang ,  MEHLOS, James Paul

IPC分类号： B64D11/02 ,  B64D11/00

CPC分类号： B64D11/02 ,  B64D11/0023

摘要： A lavatory (12) includes a partition wall (28) movable along a defined path between a deployed position in which the partition wall (28) divides the lavatory (12) into two discrete areas (18, 22) and a stowed position that defines a combined area (30) in place of the two discrete areas (18, 22). The partition wall (28) translates along the defined path between the deployed position and the stowed position.

公开(公告)号：EP3495269B1

公开(公告)日：2024-05-15

申请号：EP19152621.9

申请日：2017-03-27

IPC分类号： B64D11/06 ,  B64D11/00

CPC分类号： E05Y2900/50220130101 ,  B64D11/0023 ,  E06B3/5072 ,  E06B3/509 ,  E05D15/1005 ,  E05D15/58 ,  B64D11/0606 ,  B64C1/1438 ,  E05Y2900/21220130101 ,  E06B3/4654

公开(公告)号：EP4361022A1

公开(公告)日：2024-05-01

申请号：EP23205395.9

申请日：2023-10-24

申请人： Gulfstream Aerospace Corporation

发明人： Thornton, Sean ,  Toler, Brian

IPC分类号： B64C1/10 ,  B64D11/00 ,  B60R21/02

CPC分类号： B64D11/0023 ,  B64C1/10

摘要： A partition including, but not limited to, a first body comprising a planar, foldable material. The partition further comprises a plurality of flat substrates resistant to folding. The partition further comprising an adhesive. The substrates are adhered to the first body by the adhesive and arranged in a repeating pattern that defines a plurality of columns and rows. Each column and each row is spaced apart from its neighbor, thus defining longitudinal gaps between the columns and lateral gaps between the rows. The first body folds laterally along the longitudinal gaps in an accordion-like manner and contemporaneously folds longitudinally along the lateral gaps in an accordion-like manner. The partition contracts both laterally and longitudinally when first body contemporaneously folds laterally and longitudinally. The partition extends both laterally and longitudinally when the first body contemporaneously unfolds laterally and longitudinally.

公开(公告)号：EP4357239A1

公开(公告)日：2024-04-24

申请号：EP23193114.8

申请日：2023-08-24

申请人： The Boeing Company

发明人： MOVSESIAN, Sami ,  SAUER, Steven Hillary

IPC分类号： B64C1/14 ,  B64D11/00 ,  B64D11/02

CPC分类号： B64C1/143 ,  B64D11/02 ,  B64C1/1469 ,  B64D11/0023

摘要： An internal cabin of a vehicle includes a vehicle control area. A first door is coupled to the vehicle control area. The first door is moveable between a first open position and a first closed position. An aisle extends between the vehicle control area and a passenger seating area. A forward section of the aisle is disposed between a first monument and a second monument. A second door is disposed within the aisle between the first monument and the second monument. The second door is moveable between a second open position and a second closed position. A privacy vestibule is defined between the second door in the second closed position, the first monument, the second monument, and the vehicle control area.

公开(公告)号：EP2920067B1

公开(公告)日：2018-05-30

申请号：EP13850470.9

申请日：2013-09-30

申请人： Honda Patents & Technologies North America, LLC

发明人： HARTER, Eugene, Petit ,  HAMILTON, Michael, T.

IPC分类号： B64C1/14 ,  B64D11/00

CPC分类号： B64C1/1438 ,  B64D11/0023

摘要： A door assembly for an aircraft includes a partition panel disposed laterally within a fuselage of the aircraft and a descender panel moveably secured to a lower end of the partition panel for selectively closing an aisle opening defined below the partition panel. The door assembly further includes a handle disposed on the partition panel that is operatively connected to the descender panel through a link mechanism such that rotation of the handle is translated into movement of the descender panel to move the descender panel between a retracted position and a deployed position.

公开(公告)号：EP3277577A1

公开(公告)日：2018-02-07

申请号：EP16712329.8

申请日：2016-03-29

申请人： Lufthansa Technik AG

发明人： PFINGSTEN, Kai-Christoph ,  REIFFERSCHEID, Moritz

IPC分类号： B64C1/18 ,  B64D11/00 ,  B64C1/00

CPC分类号： B64C1/18 ,  B64C2001/009 ,  B64D11/0023

摘要： The invention relates to a device for equalizing a pressure difference for an aircraft, comprising - a planar separating wall (1), which is fixed to the aircraft and separates a first space (2) from a second space (3) in respect of flow, wherein - the separating wall (1) has a flow opening (4) that connects the first and second spaces (2, 3) in respect of flow, and - a decompression flap (5), which closes the flow opening (4), wherein - an attachment of the decompression flap (5) to the separating wall (1) is designed to allow a detachment motion of the decompression flap (5) when a predetermined pressure gradient between the first and second spaces (2, 3) is exceeded such that a flow connection exists between the first and the second spaces (2, 3), wherein - a safety apparatus (6) that limits the detachment motion of the decompression flap (5) is provided, wherein - the safety apparatus (6) comprises an energy absorption apparatus (7).

公开(公告)号：EP2708467A3

公开(公告)日：2017-11-01

申请号：EP13184546.3

申请日：2013-09-16

申请人： The Boeing Company

发明人： Scown, Stephen Lee ,  Wilcynski, Paul Joseph ,  Nix, Jeffrey ,  Spane, Marc Anton

IPC分类号： B64D11/02

CPC分类号： B64D11/02 ,  B64D11/0023

摘要： A method and apparatus operating a moveable partition (228, 406). The moveable partition (228, 406) is configured for use with a first lavatory (128) and a second lavatory (130). The moveable partition (228, 406) is further configured to separate the first lavatory (128) and the second lavatory (130) into separate spaces (304, 306) within a fixed perimeter (132) for the first lavatory (128) and the second lavatory (130) when the moveable partition (228, 406) is in a first configuration. The moveable partition (228, 406) is further configured to define a single space (310) within the fixed perimeter (132) when the moveable partition (228, 406) is in a second configuration (426). The moveable partition (228, 406) is connected to a door (408) for the first lavatory (18) in the second configuration (426).

公开(公告)号：EP2396224B1

公开(公告)日：2017-10-04

申请号：EP10703644.4

申请日：2010-02-09

申请人： Airbus Operations GmbH ,  B/E Aerospace (UK) Ltd

发明人： BECKER, Horst ,  STEIN, Hartmut ,  WESSELS, Anja ,  DETISI, Mark ,  MORRIS, Richard

IPC分类号： B64D11/04

CPC分类号： B64D11/04 ,  B64D11/0023 ,  B64D11/02 ,  B64D2011/0046 ,  Y02T50/46

公开(公告)号：EP3173331A1

公开(公告)日：2017-05-31

申请号：EP15197105.8

申请日：2015-11-30

申请人： Airbus Operations GmbH

发明人： Holst, Stefan ,  Schaefer, Bastian ,  Wengorra, Anna

IPC分类号： B64D11/00

CPC分类号： B64D11/00 ,  B64D11/0023 ,  B64D11/0698 ,  B64D2011/0046 ,  B64D2011/0092 ,  Y02T50/46

摘要： A cover panel for a core panel of a structural aircraft component includes a protection cover having an outer shape corresponding to the outer shape of the core panel and including at least one cutout aperture, and at least one fabric panel mounted to the protection cover and covering the at least one cutout aperture.

摘要翻译： 用于结构飞行器部件的核心面板的覆盖面板包括保护盖，其具有与核心面板的外部形状相对应的外部形状并且包括至少一个切口孔，以及至少一个织物面板，该至少一个织物面板安装到保护盖并覆盖 该至少一个切口孔。