Dynamically isolated pylon
    1.
    发明授权

    公开(公告)号:US11530032B2

    公开(公告)日:2022-12-20

    申请号:US16588097

    申请日:2019-09-30

    Abstract: An exemplary tiltrotor aircraft includes a fuselage carrying a wing, a pylon assembly coupled to the wing such that the pylon assembly is rotatable to selectively operate the tiltrotor aircraft between a helicopter mode and an airplane mode, a vibration isolator assembly connected to the pylon assembly and the wing including a first vibration isolator configured to isolate vibration in a vertical plane a second vibration isolator configured to isolate vibration in a lateral plane.

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