Driving mechanism of flapping-wing aircraft and flapping-wing aircraft

Abstract

The invention discloses a driving mechanism of a flapping-wing air vehicle and the flapping-wing air vehicle. The driving mechanism comprises a stander, a swing device, a translation device and a power device, wherein wings are arranged on two sides of the stander; the swing device is arranged on the stander, is connected with the wings and is used for driving the wings to swing; the translation device is arranged on the stander, is connected with the wings and is used for driving the wings to expand and shrink; and the power device is arranged on the stander and comprises a first output end and a second output end which are used for synchronous output, the first output end is connected with the swing device, and the second output end is connected with the translation device. In a use process, the first output end and the second output end of the power device are used for synchronous outputting, namely the swing and the translation are simultaneously carried out, particularly the swingperiods and expansion-shrinkage periods of the wings are accordant, so that the bionic motions of the wings to the flight of birds are realized; and the driving mechanism is simple in structure and good in maneuverability and has a good driving flight effect.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a driving mechanism of an orchid-wing aircraft and the ortho-wing aircraft. Background technique [0002] Along with the development of aircraft technology, the application of flapping wing aircraft is also more and more extensive. Due to the complex flight movements of birds (for example, the wings need to swing up and down while unfolding and retracting), it is very difficult to imitate their movements; most of the existing technologies simply imitate the swing of bird wings, and cannot independently control the expansion and contraction of a single wing And swing stroke, so flight efficiency and maneuverability are not good, are unfavorable for the flight of flapping wing aircraft. Therefore, it is necessary to provide a driving mechanism of a flapping-wing aircraft with simple structure, good maneuverability and high flight efficiency. Contents of the invention [0003] The main p...

AI Technical Summary

Problems solved by technology

[0003] The main purpose of the present invention is to propose a driving mechanism of a flapping-wing aircraft and the flapping-wing aircraft, aiming to solve the problem that the driving mechanism of the flapping-wing aircraft has a complex structure and is not conducive to flying

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