Double electromagnet driving micro flapping wing aircraft

A flapping-wing aircraft, driven technology, applied in the field of dual-electromagnetic-driven micro-flapping-wing aircraft, can solve the problems of being unable to cope with the airflow environment, storing potential energy to reduce output power, changing flight attitude control, etc., to increase weight and store less potential energy , the effect of small stiffness

Active Publication Date: 2014-04-09
SHANGHAI JIAO TONG UNIV
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  • Claims
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Problems solved by technology

[0006] For the existing Kunming-style aircraft, such as the aforementioned patent with publication number 102328744A, which adopts an electromagnetic drive method, and the aircraft of the University of Lille, the transmission method adopted requires a certain deformation of the beam structure, which will store potential energy and reduce the output power; and The existing aircraft has only one degree of freedom to drive, and cannot cope with the complex airflow environment and perform variable flight attitude control

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  • Double electromagnet driving micro flapping wing aircraft
  • Double electromagnet driving micro flapping wing aircraft
  • Double electromagnet driving micro flapping wing aircraft

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Embodiment Construction

[0024] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0025] Such as figure 1 As shown, the present embodiment provides a dual-electromagnetic-driven micro-flapping-wing aircraft, including: a transmission mechanism 1, a pair of wing mechanisms 2 and a drive mechanism 3, wherein: a pair of wing mechanisms 2 are symmetrically installed and fixed on the transmission mechanism through dovetail grooves. On both sides of the mechanism 1 , the driving mechanism 3 is hinged and fixed on the first thin plate 13 , the second thin plate 14 , and the third thin...

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Abstract

The invention provides a double electromagnet driving micro flapping wing aircraft which comprises a driving mechanism, a transmission mechanism and wing mechanisms, wherein the driving mechanism consisting of a permanent magnet and two groups of coils drives the connecting rod type transmission mechanism connected by two sets of flexible hinges; the wing mechanisms are installed and fixed on both sides of the transmission mechanism through dovetail grooves, and flap happens along with rotation of a connecting rod at the output end of the transmission mechanism so as to generate lift required by motion of the aircraft. The aircraft provided by the invention has two groups of coils which respectively drive the two wings, and various turning movements and multi-directional linear flight of the aircraft can be realized by respectively adjusting the flapping rule of the two wings.

Description

technical field [0001] The invention relates to the technical field of micro-aircraft, in particular to a dual-electromagnetic-driven micro-flapping-wing aircraft based on a flexible link mechanism. Background technique [0002] Micro-flapping-wing aircraft is a micro-aircraft that is different from fixed-wing and rotary-wing aircraft, and instead imitates birds or insects and uses complex movements of wings to achieve flight. With the development of science and technology in recent years, Micro Aircraft (MAV) is becoming a research hotspot in the scientific and technological circles. In particular, the development of MEMS technology provides the possibility for the processing and manufacturing of small-sized aircraft. The U.S. Defense Advanced Research Projects Agency proposed the basic indicators of micro-aircraft: the size of the aircraft is less than 15cm, the weight is between 10g and 100g, the flight time is 20-60min, and the flight speed is 25-70km / h. Micro-flapping...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/00B64C33/02
Inventor 张卫平张伟柯希俊柴双双邹阳邹才均叶以楠胡楠张正吴凡陈文元
Owner SHANGHAI JIAO TONG UNIV
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