The patent of the invention discloses an aircraft with a double-fuselage tandem wing vertical take-off and landing layout, and particularly relates to the technical field of aviation aircrafts. The aircraft with a double-fuselage tandem wing vertical take-off and landing layout comprises two fuselages which are arranged at an interval, and an engine is arranged on each fuselage; a front tandem type wing and a rear tandem type wing which are distributed at an interval are arranged on the two fuselages; an electric tilting rotor wing arranged at one end of the front tandem type wing is also symmetrically arranged on each fuselage; a generator is connected between each electric tilting rotor wing and each engine, the generators are electrically connected with the engines, the rear tandem typewing is provided with a first lift fan located between the two fuselages and a sliding flow rudder located below the first lift fan, and each fuselage is provided with a vertical fin located at one end of the rear tandem type wing. By the adoption of the technical scheme, the problem that an existing aircraft cannot stably and vertically take off and land under severe weather conditions is solved, and the aircraft can fly under extreme weather conditions.
本发明专利公开了一种双机身串列翼垂直起降布局的飞行器,具体涉及航空飞行器的技术领域。一种双机身串列翼垂直起降布局的飞行器,包括两个间隔设置的机身,每个机身上均设有发动机,两个机身上共同设有间隔分布的前串列式机翼和后串列式机翼,每个机身上均还对称设有位于前串列式机翼一端的电动倾转旋翼,电动倾转旋翼与发动机之间连接有发电机,发电机与发动机电连接,后串列式机翼上设有位于两个机身之间的第一升力风扇和位于第一升力风扇下方的滑流舵,每个机身上均设有位于后串列式机翼一端的垂尾。采用本发明技术方案克服了现有的飞行器无法在恶劣天气情况下稳定垂直起降的问题,可用于飞行器在极端天气条件下飞行。
Aircraft with double-fuselage tandem wing vertical take-off and landing layout
一种双机身串列翼垂直起降布局的飞行器
2020-10-20
Patent
Electronic Resource
Chinese
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