The invention discloses a low-speed safety aircraft capable of controlling the flight attitude by an aerodynamic force. The low-speed safety aircraft comprises a flexible aircraft, an engine, a gas compressor, a supply air distributor, vortex chambers, high-pressure gas cells, strip-shaped jet flow seams, helium airbags, a safety cabin and the like. Compressed gas in the gas compressor is ejected to airfoils through the strip-shaped jet flow seams arranged at the transition positions of leading edges and the airfoils of wings to generate a lift force and a push force, and is ejected to airfoils through the strip-shaped jet flow seams arranged at the transition positions of leading edges and the airfoils of a horizontal tail and a vertical tail to generate a wing effect to control the flight attitude. Through the application of a flight control principle and the combination with flexible body-wings, the helium airbags and the safety cabinet, the super-safe low-speed aircraft is formed. The low-speed safety aircraft has the advantages that fuel consumption is reduced greatly; piloting is easy; due to super-strong low-speed safety and controllability, the low-speed safety aircraft can be widely applied to prospecting, shooting, urban road monitoring, aerial advertising and the like; a super entertainment project suitable for the crowds which have firsthand experience of piloting a plane to flight, without pilot licenses, can be further developed.
Low-speed safety aircraft capable of controlling flight attitude by aerodynamic force
2015-07-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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