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垂直起降飞行器在起降过程和巡航过程中的性能要求不同,为更好地兼顾两种状态下的性能,文章设计了由两个主涵道风扇和一个前涵道风扇组成三角形动力布局垂直升力部件的垂直起降固定翼无人机,通过风力计测出涵道电机喷出的喷流来调整前涵道风扇电机的转速和两个主涵道风扇电机的倾角以达到与该系统相匹配的输出动力,使固定翼无人机从垂直起降过渡到稳定平飞的一个过程。
Vertical take-off and landing aircraft in the take-off and landing process and cruise process performance requirements are different, in order to better take into account the performance of the two states, the article designed by the two main tunnel fan and a front duct fan composed of triangular power vertical Lift vertical component of the vertical landing UAV, measured by the wind turbine jet flow of ducted motor to adjust the front ducted fan motor speed and the two main tunnel fan motor tilt to achieve with the system phase Matching the output power, so that the fixed-wing UAV from vertical to horizontal transition to a stable process.