发明名称 VERTICAL TAKE-OFF AND LANDING AIRCRAFT
摘要 A vertical take-off and landing aircraft comprises an aircraft body (6), a main thrust device (7) that provides a main thrust for the aircraft, and a posture control device. The posture control device comprises multiple posture alignment units (2) for adjusting rolling and pitching postures of the aircraft. The posture alignment unit comprises blades driven by a motor (3). By means of the aircraft of the present invention, the mechanical structure is simplified in the aspect of posture adjustment and the manufacturing difficulty and maintenance cost are reduced.
申请公布号 WO2016004852(A1) 申请公布日期 2016.01.14
申请号 WO2015CN83450 申请日期 2015.07.07
申请人 WU, JIANWEI 发明人 WU, JIANWEI
分类号 B64C29/00 主分类号 B64C29/00
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