本发明涉及飞行器技术领域,尤其涉及一种机翼结构和具有该机翼结构的飞行器以及飞行器的运行方法,所述机翼结构的分布式推进器被置入机翼内部并设置了吸气口和吹气口,所述的吸气口和吹气口在全部飞行包线内对机翼的气动性能无减损,其在对机翼进行分布式推进和增升的同时不损失机翼的气动性能,尤其是巡航和滑翔性能。本发明实施例提供的机翼结构比现有技术的推力增升机翼结构在巡航飞行阶段更节能且飞行速度更快。
The invention relates to the technical field of aircrafts, in particular to a wing structure, an aircraft with the wing structure and an operation method of the aircraft. Distributed propellers of the wing structure are arranged in wings and are provided with air suction ports and air blowing ports; the air suction port and the air blowing port do not reduce the aerodynamic performance of the wing in the whole flight envelope, and the aerodynamic performance, especially the cruising and gliding performance, of the wing is not damaged while the wing is subjected to distributed propulsion and lift augmentation through the air suction port and the air blowing port. Compared with a thrust lift augmentation wing structure in the prior art, the wing structure provided by the embodiment of the invention is more energy-saving and higher in flight speed in a cruise flight stage.
机翼结构和飞行器及运行方法
2024-06-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |