STRUCTURAL ASSEMBLY FOR AN AIRCRAFT
    1.
    发明公开

    公开(公告)号:US20240308650A1

    公开(公告)日:2024-09-19

    申请号:US18673749

    申请日:2024-05-24

    摘要: A structural assembly for an aircraft having pairs of main gantries distributed in the longitudinal direction, two transverse panels fixed to the front and the rear of the pairs of main gantries to together define a compartment for a landing gear of the aircraft, at least one pair of secondary gantries between the main gantries, at least one crossmembers parallel to the transverse panels and that straddles at least one secondary gantry, and, for each secondary gantry and each crossmember straddling the secondary gantry, a connecting rod mounted to be able to freely rotate, via a first end, on a lower part of the crossmember and, via a second end, on an outer lateral part of the secondary gantry. Such an arrangement reduces the vertical bulk of the structural assembly.

    STRUCTURAL ASSEMBLY FOR AN AIRCRAFT
    2.
    发明公开

    公开(公告)号:US20230148389A1

    公开(公告)日:2023-05-11

    申请号:US17983782

    申请日:2022-11-09

    IPC分类号: B64C25/16 B64C25/14 B64C25/04

    CPC分类号: B64C25/16 B64C25/14 B64C25/04

    摘要: A structural assembly for an aircraft having pairs of main gantries distributed in the longitudinal direction, two transverse panels fixed to the front and the rear of the pairs of main gantries to together define a compartment for a landing gear of the aircraft, at least one pair of secondary gantries between the main gantries, at least one crossmember parallel to the transverse panels and that straddles at least one secondary gantry, and, for each secondary gantry and each crossmember straddling the secondary gantry, a connecting rod mounted to be able to freely rotate, via a first end, on a lower part of the crossmember and, via a second end, on an outer lateral part of the secondary gantry. Such an arrangement reduces the vertical bulk of the structural assembly.

    Structural assembly for an aircraft

    公开(公告)号:US12017756B2

    公开(公告)日:2024-06-25

    申请号:US17983782

    申请日:2022-11-09

    摘要: A structural assembly for an aircraft having pairs of main gantries distributed in the longitudinal direction, two transverse panels fixed to the front and the rear of the pairs of main gantries to together define a compartment for a landing gear of the aircraft, at least one pair of secondary gantries between the main gantries, at least one crossmember parallel to the transverse panels and that straddles at least one secondary gantry, and, for each secondary gantry and each crossmember straddling the secondary gantry, a connecting rod mounted to be able to freely rotate, via a first end, on a lower part of the crossmember and, via a second end, on an outer lateral part of the secondary gantry. Such an arrangement reduces the vertical bulk of the structural assembly.