Method for forming supersonic vortex flying saucer rotor wing vertical-lift bird-lift dual-purpose aircraft

Abstract

The invention discloses a method for forming a supersonic vortex flying saucer rotor wing vertical-lift bird-lift dual-purpose aircraft, and aims to provide a novel multifunctional comprehensive aircraft which has all the advantages of a helicopter and also has the advantages of a fixed-wing aircraft. The aircraft integrates the advantages and functions of helicopters, rotorcrafts and fixed-wing aircrafts, and the method can also be called as an all-round aircraft forming method. In order to solve the technical problem, the technical scheme adopted by the invention is as follows: the aircraftconsists of five parts, namely a supersonic vortex generator, flying saucer rotors, rotor power, bird lift power and a fixed wing type aircraft body. The method comprises the first step of modifying the rotors of an existing helicopter, the second step of additionally arranging the supersonic vortex generator on the upper portion of the flying saucer rotors, the third step of modifying the power and shape of the original rotor wing helicopter into the power for driving the flying saucer rotors and the shape of the fixed wing aircraft body, and the fourth step of arranging bird lifting power, namely bilaterally symmetrical power capable of tilting independently, at the front part of the aircraft body.

Description

[0001] Technical field [0002] The present invention relates to a kind of composition method of aircraft, a kind of composition method of rotor helicopter, especially a kind of composition method of flying saucer rotor plus supersonic vortex as power wing vertical take-off and landing, horizontal flight helicopter, namely The invention discloses a constitutional method of a supersonic vortex flying saucer rotor helicopter and a dual-purpose aircraft. Background technique [0003] The concept and theory of the construction method of the supersonic vortex flying saucer rotor helicopter and bird-lift dual-purpose aircraft of the present invention are derived from the concepts and theories of the prior art air vortex, rotor helicopter, flying saucer and tilting power aircraft. [0004] The flying saucer rotor concept comes from the theory and concept of prior art rotor helicopters. There is a stall zone around the rotor head of the prior art rotary wing helicopter and cannot pro...

AI Technical Summary

Problems solved by technology

[0007] Existing helicopters have the disadvantages of relatively slow speed, poor maneuverability and low flying altitude

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