Manpower-wing-flapping air vehicle

A flapping-wing aircraft and human-powered technology, applied in the field of human-powered flapping-wing aircraft, can solve the problems of large overall weight of the aircraft, energy loss in the transmission process, and complex structure of large-scale manned flapping-wing aircraft

Inactive Publication Date: 2016-06-29
宋兆会
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problems of complex structure of large-scale manned flapping-wing aircraft, heavy overall weight of the aircraft, and serious energy loss in the transmission process; Flying, gliding, turning in the air, landing sports equipment, human flapping wing aircraft

Method used

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  • Manpower-wing-flapping air vehicle

Examples

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Embodiment 1

[0023] See Figure 1-11 , a manpower flapping wing aircraft, including a body 1, a flapping wing 2, a power mechanism 3, a manned device 4, and an empennage 5;

[0024] The body 1 described therein includes: a main bracket 11, a flapping wing connecting portion 12, an axle seat 14, an empennage frame 16, a support rod 17, a fixing frame 13, and a membrane pulling block 15;

[0025] The main support 11 is a straight beam, the flapping wing connection part 12 is arranged on the main support 11, the shaft seat 14 is arranged at the rear of the flapping wing connection part 12, and the empennage frame 16 is arranged at the rear of the main support;

[0026] The support bar 17 is arranged directly below the flapping wing connecting part 12, and the two ends of the support bar 17 are connected with one end of the frame bar 171 and the connecting rod 172, and the other ends of the frame bar 171 and the link bar 172 are connected with the main support 11, and the frame bar 171 is conn...

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Abstract

The invention discloses a manpower-wing-flapping air vehicle. The manpower-wing-flapping air vehicle comprises a body, flapping wings, a power mechanism, a manned device and a tail wing. The power mechanism comprises a driving shaft, a driving connecting frame with the left side and the right side which are symmetrically arranged, driving crank arms and shoes. The flapping wings comprise large arms, small arms and a wing membrane, wherein the large arms, the small arms and the wing membrane are symmetrically arranged in a left-right mode; one ends of elastic pulling locks are fixed to frame rods, and the other ends of the elastic pulling locks are fixed to the middles of large arm bodies. The manned device is fixed to a fixing frame and arranged above the shoes and between two stretchable rods, and comprises an upper-body safety belt and a lower-body safety. A reversing mechanism is a gear reversing mechanism. The tail wing is triangular and is fixed to a tail-wing frame. By means of the manpower-wing-flapping air vehicle, the taking-off movement, flying, gliding, the turning-in-air movement and landing of a single person can be really completely by manpower with the flapping wing technology, the void of the project is filled, and the manpower-wing-flapping air vehicle can be applied to the competitive sports field, the tour and sightseeing field, the person rescue field, the video shooting field and the like.

Description

technical field [0001] The invention belongs to the technical field of sports equipment, and in particular relates to a manpower flapping-wing aircraft. Background technique [0002] At present, the research level of flapping-wing aircraft is increasing day by day. Due to the application in fields such as military rescue, it has gradually developed towards micro-aircraft in recent years, while there are few researches on large-scale flapping-wing aircraft that can carry humans; on the other hand, the existing flapping-wing aircraft Electric or oil-powered drives are mostly used, and there are few researches on flapping-wing aircraft driven entirely by manpower. Electric or oil-powered aircraft need to carry batteries or oil, which increases the load of the aircraft and increases the difficulty of aircraft design; Moreover, the transmission mechanism of the existing manned flapping-wing aircraft is more complicated, and a lot of energy loss can be produced during use; the air...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 宋兆会
Owner 宋兆会
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