STOWED BLADE PNEUMATIC CLAMP
    2.
    发明申请

    公开(公告)号:US20210078695A1

    公开(公告)日:2021-03-18

    申请号:US16574459

    申请日:2019-09-18

    Abstract: An exemplary aircraft includes a pylon rotatable relative to a wing, a proprotor assembly carried by the pylon, the proprotor assembly have a proprotor blade that is foldable to a stowed position extending substantially parallel to the pylon, and a fluidic clamp positioned with the pylon and configured to grip the proprotor blade when in the stowed position, the fluidic clamp including a first inflatable bladder positioned on a first side of an opening for receiving a portion of a proprotor blade and a pressurized fluid source in fluid connection with the first inflatable bladder.

    ADDITIVE MANUFACTURE PROPROTOR BLADE

    公开(公告)号:US20210101672A1

    公开(公告)日:2021-04-08

    申请号:US16590618

    申请日:2019-10-02

    Abstract: An exemplary proprotor blade assembly includes a structural skin extending spanwise from a root to a tip and along a chord from leading edge to a trailing edge and a structural core positioned inside of the structural skin, the structural skin comprising hex-shaped structures oriented normal to the structural skin.

    STOWED BLADE ACTIVE RESTRAINT
    4.
    发明申请

    公开(公告)号:US20210094683A1

    公开(公告)日:2021-04-01

    申请号:US16585975

    申请日:2019-09-27

    Abstract: An exemplary clamp system for securing a proprotor blade in a stowed position includes a clamp having a pair of opposing pads operable between an open position to receive a portion of a proprotor blade between the pair of opposing pads and a closed position to grip the portion of the proprotor blade with the pair of opposing pads and a rotary actuator in connection with the clamp to operate the clamp between the open and the closed position.

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