发明名称 High Performance VTOL Aircraft
摘要 The present disclosure relates to a high performance Vertical Takeoff and Landing (VTOL) aircraft for executing hovering flight, forward flight, and transitioning between the two in a stable and efficient manner. The VTOL aircraft provides a highly stable, controllable and efficient VTOL aircraft. The preffered comprises: (1) a pusher propeller configuration with strategic placement which maximizes the effective use of thrust, (2) four propellers which allow for the highly-controllable and mechanically simple control methods used in multirotor aircraft, (3) electric motors which create mechanically simple, lightweight and reliable operation, (4) and a tandem wing configuration which is stable, controllable and efficient in both hovering and forward flight. The VTOL aircraft is capable of full runway, short runway or vertical takeoffs or landings, having unobstructed forward view for camera and sensor placement; and providing a compact, mechanically simple and low-maintenance VTOL aircraft design.
申请公布号 WO2016028358(A2) 申请公布日期 2016.02.25
申请号 WO2015US34069 申请日期 2015.06.03
申请人 JUAN, CRUZ_AYOROA 发明人 JUAN, CRUZ_AYOROA
分类号 B64C29/00 主分类号 B64C29/00
代理机构 代理人
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