SECONDARY BARRIERS FOR USE WITH AIRCRAFT
    1.
    发明公开

    公开(公告)号:US20230406505A1

    公开(公告)日:2023-12-21

    申请号:US17752688

    申请日:2022-05-24

    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.

    TELESCOPING SECONDARY BARRIER SYSTEM
    2.
    发明公开

    公开(公告)号:US20240336370A1

    公开(公告)日:2024-10-10

    申请号:US18295361

    申请日:2023-04-04

    CPC classification number: B64D45/0026 B64D11/0023

    Abstract: A secondary barrier system for an aircraft includes a secondary barrier gate including a telescoping structure is disclosed. The secondary barrier gate may include a plurality of crossmembers, and at least one of the plurality of crossmembers may include a panel treatment. The secondary barrier gate is rotatable between a stowed position and a deployed position and extendable between a retracted length and an extended length. The secondary barrier gate is securable in the stowed position and the deployed position. The secondary barrier gate may be rotatably mounted to a ceiling or within a crown area of the aircraft. The secondary barrier system may also include a stowage latch actuatable to selectively release and/or secure the secondary barrier gate from/in a stowed position and a deployment latch actuatable to selectively release and/or secure the secondary barrier gate from/in one of a retracted length or an extended length.

    GALLEY FOOTSTEP SYSTEMS AND METHODS
    3.
    发明申请

    公开(公告)号:US20180105253A1

    公开(公告)日:2018-04-19

    申请号:US15297454

    申请日:2016-10-19

    CPC classification number: B64C1/24 B64D11/04

    Abstract: A compartment door of a galley within an internal cabin of a vehicle (such as an aircraft) includes a front panel having a front outer surface, and a footstep system secured to the front panel. The footstep system is moveable between a retracted position and an extended support position. The footstep system is vertically oriented in the retracted position. The footstep system outwardly extends and folds to provide a step surface in the extended support position.

    Galley footstep systems and methods

    公开(公告)号:US10450050B2

    公开(公告)日:2019-10-22

    申请号:US15297454

    申请日:2016-10-19

    Abstract: A compartment door of a galley within an internal cabin of a vehicle (such as an aircraft) includes a front panel having a front outer surface, and a footstep system secured to the front panel. The footstep system is moveable between a retracted position and an extended support position. The footstep system is vertically oriented in the retracted position. The footstep system outwardly extends and folds to provide a step surface in the extended support position.

    Rotating Retractable Step System
    5.
    发明申请

    公开(公告)号:US20180118325A1

    公开(公告)日:2018-05-03

    申请号:US15339138

    申请日:2016-10-31

    Abstract: A rotating retractable step system positioned within a cutout of a wall is presented. The rotating retractable step system comprises a foot pedal and a support shaft. The foot pedal is configured to be stowed in a vertical orientation within the cutout of the wall, and to rotate between the vertical orientation and a horizontal orientation. The support shaft is associated with the foot pedal, such that movement of the support shaft extends the foot pedal outwardly away from the cutout, or retracts the foot pedal towards the cutout.

    Secondary barriers for use with aircraft

    公开(公告)号:US12214881B2

    公开(公告)日:2025-02-04

    申请号:US17752688

    申请日:2022-05-24

    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.

    Cart stowage placard enabling plate

    公开(公告)号:US10604258B2

    公开(公告)日:2020-03-31

    申请号:US15233606

    申请日:2016-08-10

    Abstract: A retractable placard system for galley cart storage bays is provided. The placard system includes an outer plate and a placard. The outer plate is mounted with a hinge to a surface of a cart storage bay and is adapted to depend substantially vertically from the surface in a first position and to rotate in a first direction upon contact by a first edge of a half size cart. The placard is mounted to the outer plate. The placard is visible in the bay with the outer plate in the first position and retracted with the outer plate rotated in the first direction to a second position.

    Space saving seating system
    9.
    发明授权

    公开(公告)号:US11117668B2

    公开(公告)日:2021-09-14

    申请号:US16528142

    申请日:2019-07-31

    Abstract: In an example, a seating system includes a seat comprising a chamber, a wall structure adjacent to the seat and defining a compartment, a door insert configured to move within the compartment between a starting position and a retracted position, wherein in the starting position, the door is adjacent to the seat and blocks access to the compartment, and in the retracted position, the door is retracted into the wall structure and provides access to the compartment, a closed channel extending from the chamber and operably connected to the door, and a piston operably coupled to the seat and positioned within the chamber, wherein when a load is applied to the seat, the piston is compressed, moving the door from the starting position to the retracted position, and when the load is removed, the piston is decompressed, causing the door to move from the retracted position to the starting position.

    Space Saving Seating System
    10.
    发明申请

    公开(公告)号:US20210031925A1

    公开(公告)日:2021-02-04

    申请号:US16528142

    申请日:2019-07-31

    Abstract: In an example, a seating system includes a seat comprising a chamber, a wall structure adjacent to the seat and defining a compartment, a door insert configured to move within the compartment between a starting position and a retracted position, wherein in the starting position, the door is adjacent to the seat and blocks access to the compartment, and in the retracted position, the door is retracted into the wall structure and provides access to the compartment, a closed channel extending from the chamber and operably connected to the door, and a piston operably coupled to the seat and positioned within the chamber, wherein when a load is applied to the seat, the piston is compressed, moving the door from the starting position to the retracted position, and when the load is removed, the piston is decompressed, causing the door to move from the retracted position to the starting position.

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