Single-degree-of-freedom flapping-wing mechanism capable of simulating spatial motion track

A technology of space movement and degree of freedom, applied in the field of flapping wing mechanism, can solve the problems of miniaturization and complex structure of flapping wing aircraft

Active Publication Date: 2018-10-12
TIANJIN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, most of the flapping wing mechanisms developed at present use planar crank rocker mechanisms, which can only realize two-dimensional flapping up and down, or need to add som

Method used

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  • Single-degree-of-freedom flapping-wing mechanism capable of simulating spatial motion track
  • Single-degree-of-freedom flapping-wing mechanism capable of simulating spatial motion track
  • Single-degree-of-freedom flapping-wing mechanism capable of simulating spatial motion track

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Embodiment Construction

[0025] The technical solutions of the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0026] like Figure 1~5 As shown, a single-degree-of-freedom flapping wing mechanism that can realize spatial motion trajectory includes a support frame 1, a transmission system 2, a frame 3 and two sets of space four-bar mechanisms 4; the frame 3 is fixed on the support frame 1, and the transmission System 2 is mounted on support frame 1 and rack 3 (see figure 1 ); fixed output shaft 209 on the frame 3, transmission system 2 drives output shaft 209 to rotate by gear transmission; As an embodiment of the present invention, as figure 2 As shown, the transmission system 2 includes a driving motor 201, a motor shaft gear 202, a double gear 203, a first gear 204, a second gear 205, a crown gear 206, a first transmission shaft 207, a second transmission shaft 208 and an output shaft 209 ; The first transmission shaft ...

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Abstract

The invention discloses a single-degree-of-freedom flapping-wing mechanism capable of simulating a spatial motion track. The single-degree-of-freedom flapping-wing mechanism comprises a supporting frame, a transmission system, a frame and two sets of space four-bar mechanisms, wherein the frame is fixedly arranged on the supporting frame; the transmission system is arranged on the supporting frameand the frame; an output shaft is fixedly arranged on the frame; the transmission system drives the output shaft to rotate through gear transmission; two sets of the space four-bar mechanisms are symmetrically arranged at two ends of the output shaft; each space four-bar mechanism comprises a crank, a connecting bar and a rocker bar; one end of each crank is fixedly arranged at one end head of the output shaft; the other end of each crank is connected with a connecting bar through a steering universal joint; one end of each rocker bar and a connecting bar form a revolute pair; the other end of each rocker bar is a free end; meanwhile, each rocker is connected with the frame through a ball pair. The single-degree-of-freedom flapping-wing mechanism provided by the invention has simple structure and high transmission efficiency, and can realize simulation of the 8-shaped spatial motion track of insect wings under the condition of single-degree-of-freedom driving.

Description

technical field [0001] The invention relates to a flapping-wing mechanism of a flapping-wing aircraft, in particular to a single-degree-of-freedom flapping-wing mechanism capable of realizing a space movement track. Background technique [0002] The wingspan of the micro-aircraft is within 15cm, the weight is not more than 100g, the flight speed is 10-20m / s, and the flight time is 20-60min; it should have real-time imaging, navigation and communication transmission capabilities. Obtaining enemy information and other military fields, as well as civilian fields such as post-disaster rescue, exploration and detection, and aerial photography, all have huge application prospects. [0003] Aircraft are generally divided into fixed-wing aircraft, rotary-wing aircraft and flapping-wing aircraft. The development of fixed-wing and rotary-wing aircraft has reached a relatively mature stage, but when the size of the aircraft drops to the order of 10cm, the aerodynamic performance and f...

Claims

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Application Information

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IPC IPC(8): B64C33/02B64C33/00
CPCB64C33/00B64C33/02
Inventor 李君兰从梦磊刘鑫生陈焱
Owner TIANJIN UNIV
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