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公开(公告)号：US20240328207A1
公开(公告)日：2024-10-03
申请号：US18599508
申请日：2024-03-08
发明人： Benedikt KIRCHER
CPC分类号： E05B63/14 , B64D11/003 , E05B47/0002 , E05B65/00 , E05B51/02
摘要： A latch mechanism for a lid of an overhead stowage compartment. The latch mechanism comprises a plurality of locking members, and a plurality of latches. Each latch is configured to engage one of the locking members, wherein the plurality of latches is configured to be mounted into a bottom of the overhead stowage compartment, and wherein the plurality of locking members is associated with a single lid of the overhead stowage compartment.
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公开(公告)号：US20240262505A1
公开(公告)日：2024-08-08
申请号：US18432120
申请日：2024-02-05
IPC分类号： B64D11/00
CPC分类号： B64D11/003
摘要： A moving object includes a seat installed on a floor of a passenger cabin, and a storage portion provided below the seat and capable of storing baggage of a passenger seated on the seat. At least a part of the storage portion is located below a floor surface of the passenger cabin.
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公开(公告)号：US20240217661A1
公开(公告)日：2024-07-04
申请号：US18189372
申请日：2023-03-24
申请人： B/E Aerospace, Inc.
IPC分类号： B64D11/00
CPC分类号： B64D11/003
摘要： An overhead stowage bin is disclosed herein. The overhead stowage bin includes a top panel, a bottom panel, a back panel, and a plurality of side panels configured to define a volume to stow luggage, a door configured to close the stowage bin, and a window disposed within the door, the window configured to transition between an opaque state and a transparent state.
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公开(公告)号：US20240199212A1
公开(公告)日：2024-06-20
申请号：US18590349
申请日：2024-02-28
申请人： MHI RJ Aviation ULC
发明人： Michel Rheaume , Elio Ruggi
IPC分类号： B64D11/00
CPC分类号： B64D11/003
摘要： An overhead luggage bin includes: a bucket including side walls and a belly wall defining a luggage bin interior, a door displaceable between open and closed positions, and a bullnose extending along a forward edge of the belly wall; a hinge bracket fixedly mounted to one of the side walls, the hinge bracket extending between a lower portion mounted to the bullnose and an upper portion having a pivot; and a door displacement mechanism mounted to the door and mounted to the pivot of the hinge bracket, to displace the door to the open position. The hinge bracket has a rear mounting extending between the upper portion and the lower portion, the rear mounting mounted to a forward edge of said one of the side walls of the bucket.
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公开(公告)号：US11975837B2
公开(公告)日：2024-05-07
申请号：US17619201
申请日：2021-03-26
发明人： Alexander Weng , Felix Helfrich , Holger Warner , Benedikt Kircher , Johanna Roestel , Efe Kolcak
CPC分类号： B64D11/003 , B64F5/00
摘要： A vehicle region with a roof section of a primary structure and with two luggage compartments. One of the luggage compartments comprises a detachable luggage compartment flap and a luggage compartment top, which forms the upper boundary of a part of a luggage space. A detachable fastening device can rotatably fasten the luggage compartment flap on the luggage compartment. A front edge of the luggage compartment top is at a distance from an end point in an intermediate space above a luggage compartment, to which end point a side of a ceiling panel is movable, the distance being greater than or equal to a width of the ceiling panel. Methods for installing and removing a ceiling panel above two luggage compartments are provided, wherein the ceiling panel is guided at least partially through a luggage space of a luggage compartment when the luggage compartment flap has been removed.
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公开(公告)号：US11945588B2
公开(公告)日：2024-04-02
申请号：US17867904
申请日：2022-07-19
申请人： THE BOEING COMPANY
IPC分类号： B64D11/00
CPC分类号： B64D11/003 , B64D2231/025
摘要： A vehicle includes an internal cabin, a plurality of stowage bin assemblies within the internal cabin, a plurality of passenger service units (PSUs) within the internal cabin, and an emergency oxygen system within the internal cabin. The plurality of stowage bin assemblies are uncoupled (for example, separate and distinct) from one or both of the plurality of PSUs or the emergency oxygen system. In an example, the plurality of stowage bin assemblies are uncoupled from the emergency oxygen system. In another example, the plurality of stowage bin assemblies are uncoupled from the plurality of PSUs. In another example, the plurality of stowage bin assemblies are uncoupled from both the plurality of PSUs and the emergency oxygen system.
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公开(公告)号：US20230407688A1
公开(公告)日：2023-12-21
申请号：US17845611
申请日：2022-06-21
申请人： GOODRICH CORPORATION
发明人： Brandon Lee , Aaron J. Roberts , Michael Schuh
CPC分类号： E05C3/12 , B64D11/003
摘要： A bidirectional latching device for securing a cargo in a vehicle may have a latch catch assembly and a latch head. The latch catch assembly may selectably engage with the latch head. When engaged with the latch head, the latch catch assembly may lock the latch head in position to resist movement and the latch head may secure the cargo in the vehicle. When disengaged from the latch head, the latch catch assembly may release the latch head and the latch head may move to a stowed position. The latch catch assembly may lock the latch head to resist movement in one or more directions of movement. The latch head may be shaped to secure the cargo in the vehicle in at least two directions. Thus, cargo may be secured more efficiently by requiring a reduced number of latch devices because the disclosed latch device is bidirectional.
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公开(公告)号：US11767117B2
公开(公告)日：2023-09-26
申请号：US17142918
申请日：2021-01-06
发明人： Enoch Morishima
CPC分类号： B64D11/003 , B64D11/06 , B64D2011/0046
摘要： A room for an aircraft cabin is a hollow box shaped room and installed in the aircraft cabin. The room includes a floor wall portion that is configured to face a seat of the cabin, a side wall portion that extends from the floor wall portion in a direction away from the seat and has an opening portion for entering and leaving the room, a ladder portion extending in a direction toward the seat from a periphery of the opening portion, and a ceiling wall portion that extends to couple the floor wall portion and the side wall portion and has an engagement structure with an inner wall of the cabin.
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公开(公告)号：US20230271691A1
公开(公告)日：2023-08-31
申请号：US17901249
申请日：2022-09-01
发明人： Paolo CAVARERO , Michael MOSLER , Martin HENTSCHEL
CPC分类号： B64C1/067 , B64D11/003 , B64D2011/0046
摘要： A cabin module for an aircraft comprises a section which has an upward-facing surface in an installed state of the cabin module, wherein the upward-facing surface of the section comprises an integrated drainage channel. An aircraft furthermore comprises at least one such cabin module.
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公开(公告)号：US20230150673A1
公开(公告)日：2023-05-18
申请号：US17527493
申请日：2021-11-16
申请人： The Boeing Company
发明人： Steven Ellis Rhynard , Joe Files
CPC分类号： B64D11/003 , B64C7/00
摘要： An assembly configured to be mounted within an interior of a vehicle. The assembly includes a monument wall configured to be mounted in the interior of the vehicle. A panel is configured to attach to a support structure above the monument wall with the panel having a first edge and a second edge. A latch configured to be mounted to the panel between the first edge and the second edge. A pull member is attached to the panel and comprises an elongated member attached to the latch and a handle. A translating hinge is configured to be mounted to the second edge of the panel to provide for translating and pivoting movement of the panel within an access area between the monument wall and the support structure to connect and disconnect the panel from the support structure.
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