Seat assembly and passenger seat arrangement

    公开(公告)号:US12054262B2

    公开(公告)日:2024-08-06

    申请号:US17332849

    申请日:2021-05-27

    Inventor: Max Wisniewski

    CPC classification number: B64D11/0639 B64D11/0627 B64D11/0636 B64D11/0693

    Abstract: A seat assembly includes a base structure having at least one of a seat pan shell and a backrest shell, and one or more attachment structures configured to removably couple at least one of the seat pan shell and the backrest shell to a seat surface arrangement or a utility surface arrangement. The base structure is convertible between a passenger seat and a utility element based on the coupling of the seat surface arrangement or the utility surface arrangement, respectively, to the base structure.

    MOVING COCKPIT FOR VEHICLE
    2.
    发明公开

    公开(公告)号:US20240239493A1

    公开(公告)日:2024-07-18

    申请号:US18511395

    申请日:2023-11-16

    Inventor: Ik Keun CHOI

    CPC classification number: B64D11/0639 B64D11/0619

    Abstract: A moving cockpit for a vehicle including a cockpit module provided in an inner front side of the vehicle, a guide rail provided on an inner panel of the vehicle, the guide rail extending in a forward direction and a backward direction relative to the front side of the vehicle, and a cockpit moving unit movably provided on the guide rail, the cockpit configured to move the cockpit module forward and backward in the vehicle.

    AIRCRAFT SEAT WITH NESTED ENERGY ATTENUATION GUIDE SYSTEM

    公开(公告)号:US20240124141A1

    公开(公告)日:2024-04-18

    申请号:US17966413

    申请日:2022-10-14

    CPC classification number: B64D11/0619 B64D11/0639 B64D11/0698

    Abstract: An aircraft seat assembly including stanchions defining elongated guide channels and elongated motion sleds nested in the guide channels and affixed to a seat bucket. An energy absorber implemented as a wire bender assembly is coupled between the stanchions and the motion sled. In use, the elongated guide channels guide motion of the motion sleds and the wire bender assemblies attenuate energy during a dynamic event exceeding a predetermined threshold load value. The elongated interface between the guide channels and motion sleds serve to transfer excessive loading to the seat frame thereby protecting the seat assembly from damage and the occupant from excessive lumbar spinal loads.

    ARRANGEMENT OF AIRCRAFT SEATS
    9.
    发明申请

    公开(公告)号:US20190233116A1

    公开(公告)日:2019-08-01

    申请号:US16265706

    申请日:2019-02-01

    CPC classification number: B64D11/0601 B64D11/0604 B64D11/0639 B64D11/064

    Abstract: An aircraft seat arrangement within an aircraft cabin having a longitudinal axis and two windowed side walls and a central aisle, said arrangement comprising at least two pairs of seats arranged opposite each other along an axis parallel to said longitudinal axis of the cabin, in each pair of seats a window seat being adjacent to a windowed side wall and the other aisle seat being adjacent to said central aisle. Each seat is configured such to perform a reclining movement along a respective reclining axis between a sitting position and an extended position, and vice versa, wherein in said extended position each seat has a maximum extension defined by two points lying on the reclining axis. Each window seat is oriented at a first angle obtained from the intersection of the respective reclining axis with a straight line parallel to the longitudinal axis of the cabin at the first point of maximum extension of the window seat.

Patent Agency Ranking