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公开(公告)号:US20240124118A1
公开(公告)日:2024-04-18
申请号:US17966971
申请日:2022-10-17
Applicant: THE BOEING COMPANY
Inventor: Sami Movsesian , Steven Hillary Sauer
CPC classification number: B64C1/1469 , B64C1/1461 , B64D45/0028
Abstract: 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.
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公开(公告)号:US11926433B2
公开(公告)日:2024-03-12
申请号:US17390392
申请日:2021-07-30
Applicant: Airbus Americas, Inc. , Airbus Operations GmbH
Inventor: John A. Brewster , Thomas Freiwald , Christian Holst
CPC classification number: B64D45/0028 , B64C1/1469 , E05B51/02 , E05B2051/026
Abstract: A time-delay latch for securing a structure in a specified position includes a housing, a fluid chamber contained within the housing for holding fluid, a pin that extends through the fluid chamber and is axially movable within and through the fluid chamber, and a release frame movably secured within the housing. When the pin is in a latched position, the release frame engages with the pin to prevent axial movement of the pin. When the pin is in an unlatched position, the release frame disengages from the pin to allow axial movement of the pin. The axial movement of the pin between the latched position and the unlatched position requires a prescribed duration of time to elapse. During operation, the axial movement of the pin between the unlatched position and the latched position can occur faster than the prescribed duration of time.
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公开(公告)号:US12084164B2
公开(公告)日:2024-09-10
申请号:US17966971
申请日:2022-10-17
Applicant: THE BOEING COMPANY
Inventor: Sami Movsesian , Steven Hillary Sauer
CPC classification number: B64C1/1469 , B64C1/1461 , B64D45/0028
Abstract: 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.
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公开(公告)号:US20230406505A1
公开(公告)日:2023-12-21
申请号:US17752688
申请日:2022-05-24
Applicant: The Boeing Company
Inventor: Christopher B. Singleton , Emmanuel A. Garcia , Joshua Yu-Hu Lee
CPC classification number: B64D11/0023 , B64D45/0028 , B64C1/1469
Abstract: Secondary barriers for aircraft are disclosed. An example secondary barrier includes a plurality of tracks to mount to a first monument in a cabin of an aircraft and a plurality of rods, where respective ones of the rods slidably engage respective ones of the tracks. The secondary barrier includes a panel coupled to respective ends of the rods. The rods to move relative to the tracks between a stowed position and a deployed position. The panel in the deployed position is to interface with a second monument in the cabin opposite the first monument. The rods are to extend between the first monument and the second monument when the secondary barrier is in the deployed position.
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公开(公告)号:US11691711B2
公开(公告)日:2023-07-04
申请号:US17365288
申请日:2021-07-01
Applicant: AIRBUS SAS
Inventor: Thierry Leger , Benoît Salgues
CPC classification number: B64C1/1461 , B64C1/1469 , B64D45/0028
Abstract: A removable barrier and an aircraft including such a removable barrier. The barrier including a panel configured to block at least partly an opening delimited by a frame, a plurality of straps each connected to the panel and each having first and second ends, for each strap, a first connection configured to connect the first end of the strap and a first edge of the frame at least temporarily, a second connection configured to connect the second end of the strap and a second edge of the frame at least temporarily, at least one folded overlength at the level of at least one of the first and second ends of the strap, at least one breakable connection keeping the overlength folded.
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