The invention provides a target unmanned aerial vehicle with high maneuverability and wide speed range. The aerial vehicle comprises two fixed main wings arranged on the two sides of the machine body and a pair of V-shaped empennages arranged at the tail of the machine body; the fixed main wings adopt a supercritical wing type, so that the aerodynamic performance of the unmanned aerial vehicle in a transonic speed range can be improved; and the V-shaped empennages are provided with distributed control surfaces, and the functions of a rudder and an elevator can be achieved through mutual cooperation of the control surfaces. By adopting the small V-shaped empennages with the distributed control surfaces and the supercritical fixed main wings, the unmanned aerial vehicle has high maneuverability so as to meet the requirements of different types of flight missions.
本发明提供一种高机动宽速域的靶标无人飞行器。该飞行器包括:设置在所述机体两侧的两个固定主翼,设置在所述机体尾部的一对V型尾翼;所述固定主翼采用超临界翼型,可改善该无人飞行器在跨音速范围内的气动性能;所述V型尾翼具有分布式舵面,可通过舵面之间的相互配合,起到方向舵和升降舵的作用;通过采用带有分布式舵面的小型V尾和超临界固定主翼,所述无人飞行器得以具备较高的机动能力以应对不同类型的飞行任务需要。
Small target unmanned aerial vehicle with high maneuverability and wide speed range
一种高机动宽速域的小型靶标无人飞行器
2021-09-14
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |