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Ornithopter and method of controlling ornithopter

A flapping-wing aircraft and flying-wing technology, applied in aircraft, helicopters, motor vehicles, etc., can solve the problem of light weight of flapping-wing aircraft without considering the double-side drive structure, and achieve an increased flapping range, fewer gear teeth, and improved performance. The effect of flutter efficiency

Pending Publication Date: 2021-01-15
BIONIWINGS BEIJING TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, it has not been considered to start with the bilateral drive structure itself to realize the lightweight of the flapping wing aircraft

Method used

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  • Ornithopter and method of controlling ornithopter
  • Ornithopter and method of controlling ornithopter
  • Ornithopter and method of controlling ornithopter

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Embodiment Construction

[0076] The technical solutions of the present disclosure will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present disclosure, but not all of them. Based on the embodiments in the present disclosure, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present disclosure.

[0077] Unless otherwise defined, the technical terms or scientific terms used in the present disclosure shall have the usual meanings understood by those skilled in the art to which the present disclosure belongs.

[0078] The flapping-wing aircraft according to the embodiments of the present disclosure will be described in detail below with reference to the accompanying drawings.

[0079] figure 1 A schematic diagram showing the overall structure of the flapping-wing aircraft (1) according to an embodim...

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Abstract

The invention relates to an ornithopter and a method for controlling the same. The ornithopter comprises a gear transmission assembly (100), a power source (200), and a flying wing (300). The gear transmission assembly (100) is arranged on a fuselage of the ornithopter and comprises a first gear (101) and a second gear (102) which are symmetrically arranged along the center line of the ornithopterand engaged with each other on the matching side; the power source (200) comprises a first power source (201) and a second power source (202), and the first power source (201) and / or the second powersource (202) provide / provides power for the gear transmission assembly (100) so as to drive the first gear (101) and the second gear (102) to do reciprocating motion; and a flying wing (300) directlyconnected to the first gear (101) and the second gear (102) so as to move up and down within an angular range when the first gear (101) and the second gear (102) reciprocate.

Description

technical field [0001] The present disclosure relates to the field of aircraft, and more particularly, to an orchid-wing aircraft and a method for controlling the ortho-wing aircraft. Background technique [0002] In recent years, aircraft have been favored by more and more people, especially flapping wing aircraft, because of their small size, weak noise, and good concealment, they have great application prospects in civil and military applications. and development space. [0003] At present, two sets of transmission mechanisms usually drive the wings on the left and right sides to flutter up and down. This double-sided driving method is not only complex in structure, but also takes up a relatively large space, which makes the size of the transmission mechanism larger, which brings great difficulties to the weight reduction of the flapping wing aircraft. For the lightweight of the flapping wing aircraft, more attention has been paid to the improvement of the fuselage stru...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C33/02
CPCB64C33/02
Inventor 刘迎建侯涛李治国段宇刘静
Owner BIONIWINGS BEIJING TECH CO LTD
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