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公开(公告)号:US20170233070A1
公开(公告)日:2017-08-17
申请号:US15256140
申请日:2016-09-02
CPC分类号: B64C29/02 , B64C3/56 , B64C9/00 , B64C27/57 , B64C39/024 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0088 , G05D1/0858
摘要: One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.
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公开(公告)号:US10287013B2
公开(公告)日:2019-05-14
申请号:US15256140
申请日:2016-09-02
摘要: One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.
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