The invention discloses an active wing assembly based on airflow control and an aircraft, the active wing assembly comprises wings arranged in pairs and active airflow generating devices arranged on the wings, the active airflow generating devices comprise upper active airflow generating devices and lower active airflow generating devices, and the upper active airflow generating devices and the lower active airflow generating devices are respectively arranged corresponding to the upper surfaces and the lower surfaces of the wings; the flowing directions of gas generated by the upper active gas flow generating device and the lower active gas flow generating device are both in the longitudinal direction of the wing; lift force and descent force are obtained through the speed difference of airflow flowing through the upper surface and the lower surface of the wing, no special requirement for the wing section (longitudinal section structure) exists, and the design and machining difficulty of the wing is greatly simplified; the difference of thrust is formed through the exhaust speed difference of the airflow generating devices of the wings on the left side and the right side, the superposition of the steering effect and the heeling effect of the aircraft can be achieved, the turning radius of the aircraft can be greatly reduced, and high operability and high maneuverability superior to those of the prior art are achieved.
本发明公开了一种基于气流控制的主动机翼总成及飞行器,包括成对设置的机翼和设置于机翼的主动气流发生装置,主动气流发生装置包括与所述机翼的上表面和下表面对应分别设有的上主动气流发生装置和下主动气流发生装置,上主动气流发生装置和下主动气流发生装置所产生的气体流动方向均在机翼的纵向;本发明利用流经机翼上下表面的气流速度差获得升力以及下降力,对于翼型(纵向剖面结构)无特殊要求,大大简化机翼的设计和加工难度;通过左右两侧机翼的气流发生装置的排气速度差形成推力的不同,可以实现飞机的转向和侧倾,两种效应的叠加,可以大大减小飞机的转弯半径,实现超越现有技术的高可操作性和高机动性。
Active wing assembly based on airflow control and aircraft
基于气流控制的主动机翼总成及飞行器
2023-08-15
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT WING AND CONTROLLABLE AIRFLOW MODIFICATION DEVICE ADJUSTMENT METHOD
European Patent Office | 2017
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