COMPOSITE TWIN BEAM MAIN LANDING GEAR FOR AN AIRCRAFT

    公开(公告)号:US20200377202A1

    公开(公告)日:2020-12-03

    申请号:US16426357

    申请日:2019-05-30

    申请人: CTLP, LLC

    IPC分类号: B64C25/62 F16F1/28 F16F1/30

    摘要: A main landing gear assembly for an aircraft has an upper beam and a lower beam. The proximal ends of the upper and lower beams are each connected to a trunnion assembly that is mounted on the fuselage or wing of the aircraft. The distal ends of the upper and lower beams are each affixed to an axel support structure on which a main wheel of the landing gear assembly is mounted. In the gear assembly, the upper beam and the lower beam are coplanar and act together, in combination, to accommodate a planar flexure of the gear assembly during aircraft takeoffs and landings.

    Composite twin beam main landing gear for an aircraft

    公开(公告)号:US11279474B2

    公开(公告)日:2022-03-22

    申请号:US16426357

    申请日:2019-05-30

    申请人: CTLP, LLC

    摘要: A main landing gear assembly for an aircraft has an upper beam and a lower beam. The proximal ends of the upper and lower beams are each connected to a trunnion assembly that is mounted on the fuselage or wing of the aircraft. The distal ends of the upper and lower beams are each affixed to an axel support structure on which a main wheel of the landing gear assembly is mounted. In the gear assembly, the upper beam and the lower beam are coplanar and act together, in combination, to accommodate a planar flexure of the gear assembly during aircraft takeoffs and landings.

    COMPOSITE TWIN BEAM MAIN LANDING GEAR FOR AN AIRCRAFT

    公开(公告)号:US20210316845A9

    公开(公告)日:2021-10-14

    申请号:US16426357

    申请日:2019-05-30

    申请人: CTLP, LLC

    IPC分类号: B64C25/62 F16F1/28 F16F1/30

    摘要: A main landing gear assembly for an aircraft has an upper beam and a lower beam. The proximal ends of the upper and lower beams are each connected to a trunnion assembly that is mounted on the fuselage or wing of the aircraft. The distal ends of the upper and lower beams are each affixed to an axel support structure on which a main wheel of the landing gear assembly is mounted. In the gear assembly, the upper beam and the lower beam are coplanar and act together, in combination, to accommodate a planar flexure of the gear assembly during aircraft takeoffs and landings.