Pylon Restraint System
    1.
    发明申请

    公开(公告)号:US20210094678A1

    公开(公告)日:2021-04-01

    申请号:US16584448

    申请日:2019-09-26

    Abstract: In an embodiment, a rotorcraft includes an airframe; a main rotor transmission; one or more brackets mounting the main rotor transmission to the airframe, longitudinal axes of the one or more brackets being substantially parallel with a longitudinal axis of the rotorcraft; and one or more restraints mounting the main rotor transmission to the airframe, the one or more restraints being mounted at an angle non-orthogonal to the longitudinal axis of the rotorcraft and a lateral axis of the rotorcraft.

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