The invention provides a tilting coaxial double-propeller multi-power duct manned aircraft which is a full-electric manned aircraft, a fly-by-wire control system is adopted in the aspect of flight control, and a flight control module autonomously controls three-pair six-engine coaxial double-propeller power ducts and control surface parts on wings. Through the control mode of combining rudder control and power duct tilting, flight mode conversion such as vertical take-off and landing and horizontal cruise under the unmanned condition is achieved. The manned aircraft is convenient and fast in flight mode conversion and stable in structure, combines the advantages of a fixed wing aircraft on the basis of a multi-duct propeller, has the vertical take-off and landing capacity and high cruising efficiency, is low in take-off and landing site requirement and has high advantages in the fields of low-altitude commuting, short-distance cargo delivery, vaccine transportation and distribution, disaster situation material guarantee and the like.
本发明提供了一种可倾转共轴双桨多动力涵道的载人飞行器,该飞行器为全电动载人飞行器,在飞行操纵方面采用电传操纵系统,由飞行控制模块自主控制三对六发的共轴双桨式动力涵道与机翼上的舵面部件,通过舵控与动力涵道倾转相结合的控制方式,实现在无人驾驶情况下垂直起降、水平巡航等飞行模态转换。该载人飞行器,飞行模态转换便捷,架构稳定,在多涵道螺旋桨的基础上结合固定翼飞行器的优势,兼具垂直起降能力与较高的巡航效率,对于起降场地要求低,在低空通勤、短距货物投递、疫苗运输分配、灾情物资保障等领域具有较强优势。
Tilting coaxial double-propeller multi-power duct manned aircraft
一种可倾转共轴双桨多动力涵道的载人飞行器
2021-12-17
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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