ROCKET-TURBINE-POWERED VTOL AIRCRAFT

    公开(公告)号:US20210284332A1

    公开(公告)日:2021-09-16

    申请号:US17196643

    申请日:2021-03-09

    Abstract: A vertical-takeoff-and-landing (“VTOL”) aircraft including a non-VTOL aircraft equipped for forward takeoff and flight and a modular boom system interoperably coupled to the non-VTOL aircraft. The modular boom system includes a first modular boom and a second modular boom. The first modular boom includes a first rocket-turbine engine. The first modular boom is mounted to a first wing of the non-VTOL aircraft. The second modular boom includes a second rocket-turbine engine. The second modular boom is mounted to a second wing of the non-VTOL aircraft.

    STOWED BLADE PNEUMATIC CLAMP
    3.
    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.

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