Flyer
An aircraft and main body technology, applied in the field of aircraft, can solve the problems that light aircraft cannot fly long distances, increase the weight of the aircraft, and fast fuel consumption, etc., and achieve the effects of weight reduction, elimination of safety hazards, and high gas compression rate
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[0014] See attached figure 1 The present invention is mainly composed of a floating plate 1 and a main body 2 of the aircraft. The floating plate 1 is fixed on the top of the main shaft 21. The main shaft 21 passes through a compression cylinder 22 inside the main body 2 and extends out of the main body 2. The piston of the cylinder 22 is fixed on the main shaft. 21 on; the main body 2 is in the shape of a butterfly, and its periphery is provided with a number of air compressors 3. In this embodiment, three air compressors are used: the primary compressor 31, the intermediate compressor 32 and the advanced compressor 33. The exhaust port of the compressor 31 communicates with the intake port of the intermediate compressor 32, and the exhaust port of the intermediate compressor 32 communicates with the intake port of the advanced compressor 33. The engine 4 drives the three disc air compressors to work. The air enters the air storage tank 5 after being compressed step by step.
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