Flapping-wing micro aerial vehicle with renewable energy

A micro air vehicle and energy technology, which is applied in the field of micro bionic flapping-wing aircraft and can solve problems such as insufficient power reserve of aircraft

Active Publication Date: 2015-12-09
JILIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides a flapping-wing micro-aircraft with renewable energy to solve the problem of insufficient power reserve in the aircraft

Method used

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  • Flapping-wing micro aerial vehicle with renewable energy
  • Flapping-wing micro aerial vehicle with renewable energy
  • Flapping-wing micro aerial vehicle with renewable energy

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Embodiment Construction

[0022] Including piezoelectric film flapping wing 1, flapping wing bionic support frame 2, flapping wing flexible wing frame 3, control circuit module with built-in micro lithium battery 4, solar power generation film tail 5, motor and transmission mechanism 6, frame body 7 , solar power generation wing film 8; wherein, the flapping wing bionic support frame 2 is connected with the motor and the transmission mechanism 6, and the motor and the transmission mechanism 6 and the control circuit module 4 with a built-in micro lithium battery are all fixed on the frame body 7, through The lead wire connects the micro-lithium battery with the control circuit module 4, the solar power generation film tail 5 is fixedly connected with the frame body 7, the piezoelectric film flapping wing 1 and the solar power generation wing film 8 are respectively connected with the flapping wing flexible wing frame 3, wherein the flapping wing The flexible wing frame 3 is located in the middle, and th...

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Abstract

The invention relates to a flapping-wing micro aerial vehicle with renewable energy, and belongs to micro bionic aerial vehicles. A flapping-wing bionic support frame is connected with a motor and transmission mechanism, the motor and transmission mechanism and a control circuit module with an internal micro lithium battery are both fixed on a vehicle rack body, and a solar power generation film empennage is fixedly connected with the vehicle rack body; piezoelectric film flapping wings and solar power generation wing films are connected with a flapping-wing flexible wing frame which is located in the middle, the piezoelectric film flapping wings are located at the bottommost layer, the flapping-wing flexible wing frame is connected with the flapping-wing bionic support frame, and a power generation part is connected with the control circuit module through a wire. The flapping-wing micro aerial vehicle has the advantages that the structure is novel, optical energy can be converted into electric energy on the basis of a photoelectric effect of the solar films, an electricity charging and generating device made of the two materials is simple and has the advantages of being high in conversion efficiency, small in mass, wide in application range and the like.

Description

technical field [0001] The invention belongs to a miniature bionic aircraft, in particular to a miniature bionic flapping-wing aircraft based on self-generating endurance. Background technique [0002] With the development of the wireless field, the improvement of micro-electromechanical technology, and the continuous deepening of research on micro-aircraft, flapping-wing aircraft have come into people's field of vision more and more, especially because of their small size, light weight, concealment and reliability. The advantages of operability have been paid more and more attention by people, but the energy problem of micro-aircraft has always limited the development of aircraft. The energy and power part is the most basic and important component of micro-aircraft, and has always been the key research direction of researchers. In the existing achievements, the energy and power units often occupy most of the space and mass of the MAV, which greatly limits its carrying capac...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/00B64C33/02B64D27/24
Inventor 刘强潘胜利王翠周晓勤侯强孙厚野李玉强薛迪
Owner JILIN UNIV
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