Swivel Locking System
    72.
    发明公开

    公开(公告)号:US20240253530A1

    公开(公告)日:2024-08-01

    申请号:US18633079

    申请日:2024-04-11

    CPC classification number: B60N2/08 B60N2/14

    Abstract: A swivel locking system for preventing swiveling of a seat frame includes a locking pin and a series of pulleys along with a housing attached to a swivel plate. The locking pin is located in the housing and is biased to be extended downwardly through an aperture in the swivel plate and retracted from the aperture via a cable. The seat frame is able to be swiveled when the locking pin is retracted from the aperture, thereby unlocking the seat frame from a bottom support.

    Aircraft Skin Alignment System and Method with Edge Indexing

    公开(公告)号:US20240239517A1

    公开(公告)日:2024-07-18

    申请号:US18413903

    申请日:2024-01-16

    CPC classification number: B64F5/10 B64C1/12

    Abstract: An aircraft skin alignment system includes a support structure to support one or more aircraft skins, a puller tool, and a clamp tool; the puller tool having a base, the base supporting a holding mechanism to releasably engage with a first aircraft skin and a pulling mechanism to apply a pulling force to the first aircraft skin when the first aircraft skin is engaged with the holding mechanism; and the clamp tool having a body supporting an edge locator; the puller tool is to pull the first aircraft skin such that a first edge of the aircraft skin abuts the edge locator, the edge locator preventing the first edge from being pulled past the edge locator; and tool holes can be drilled into the first aircraft skin such that the tool holes are aligned based on an edge index due to a position of the edge locator.

    Drip edge on galley work surface
    75.
    外观设计

    公开(公告)号:USD1031338S1

    公开(公告)日:2024-06-18

    申请号:US29811196

    申请日:2021-10-12

    Abstract: FIG. 1 is a perspective view of the drip edge on galley work surface showing our new design;
    FIG. 2 is a front view of the drip edge on galley work surface of FIG. 1;
    FIG. 3 is a back view of the drip edge on galley work surface of FIG. 1;
    FIG. 4 is a left view of the drip edge on galley work surface of FIG. 1;
    FIG. 5 is a right view of the drip edge on galley work surface of FIG. 1;
    FIG. 6 is a top view of the drip edge on galley work surface of FIG. 1;
    FIG. 7 is a bottom view of the drip edge on galley work surface of FIG. 1;
    FIG. 8 is a perspective view of the drip edge on galley work surface of FIG. 1 in a stowed configuration;
    FIG. 9 is a front view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
    FIG. 10 is a left view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
    FIG. 11 is a right view of the drip edge on galley work surface of FIG. 1 in the stowed configuration;
    FIG. 12 is a perspective view of the drip edge on galley work surface of FIG. 1 in a deployed configuration;
    FIG. 13 is a front view of the drip edge on galley work surface of FIG. 1 in the deployed configuration;
    FIG. 14 is a left view of the drip edge on galley work surface of FIG. 1 in the deployed configuration; and,
    FIG. 15 is a right view of the drip edge on galley work surface of FIG. 1 in the deployed configuration.
    In FIGS. 1-15, broken lines indicate environmental structure that forms no part of the claimed design.

    Electrical Adapter for Fire Suppression Bottle

    公开(公告)号:US20240165441A1

    公开(公告)日:2024-05-23

    申请号:US18515904

    申请日:2023-11-21

    CPC classification number: A62C3/08 A62C37/04

    Abstract: A system for establishing an auxiliary electrical connection for an igniter configured to puncture a fire bottle. The system having an adapter configured to conceal an electrical connection of the igniter and electrically couple the concealed electrical connection to the auxiliary connection. The auxiliary connection preventing an improper connection being made to the igniter by having a different connection size than the electrical connections on the igniter.

    Cell Level Fusible Link for a Lithium Ion Battery

    公开(公告)号:US20240154257A1

    公开(公告)日:2024-05-09

    申请号:US18502204

    申请日:2023-11-06

    CPC classification number: H01M50/516 H01M10/0525 H01M50/534 H01M50/581

    Abstract: A battery system includes a first battery cell; a second battery cell positioned adjacent to the first battery cell; and a fusible link connecting the first battery cell to the second battery cell. The fusible link having a first tab connected to and extending from the first battery cell; a second tab connected to and extending from the second battery cell; and a connection connecting the first tab to the second tab; the connection is to release the first tab from the second tab upon being heated to a threshold temperature; and releasing the first tab from the second tab protects the first battery cell from thermal runaway conditions of the second cell.

    Electric Aircraft
    78.
    发明公开
    Electric Aircraft 审中-公开

    公开(公告)号:US20240132212A1

    公开(公告)日:2024-04-25

    申请号:US18483338

    申请日:2023-10-08

    CPC classification number: B64C39/08 B64D27/02

    Abstract: An electric aircraft includes a forward wing and an aft wing both located on a top side of a fuselage and both having an upward dihedral angle. The forward wing has a straight or slightly forward-swept leading edge. The aft wing has a swept leading edge. A plurality of propeller engines are located on a leading-edge side of the forward wing. A single propeller engine may be located on a top side of an aft end of the fuselage; alternatively, a plurality of propeller engines are located on the aft wing on either its leading or trailing edge. The propeller engines are each powered by an electric motor. An unobstructed cargo door is located on a side of the fuselage, aft of the forward wing.

    Doorway Side Guide System
    79.
    发明公开

    公开(公告)号:US20240034470A1

    公开(公告)日:2024-02-01

    申请号:US18360900

    申请日:2023-07-28

    CPC classification number: B64D9/003

    Abstract: A doorway side guide system includes a base mechanically coupled with a bottom portion of a doorway. A mounting member is rotatably coupled to the base via a hinge for rotating between a deployed position and a stowed position. A contact member is mechanically coupled with the mounting member via a pivot such that the contact member is configured to rotate about the pivot. The contact member extends outside of the doorway in the deployed position for guiding cargo through the doorway and for protecting a doorframe of the doorway.

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