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A rotating flapping wing thrust generating device with a spring

A generating device and thrust technology, which is applied in the field of rotating flapping wing thrust generating devices with springs, can solve the problems of high fatigue strength requirements of flapping wing materials, low efficiency, and non-directional adjustment of the direction of lift, etc.

Inactive Publication Date: 2016-02-17
丁霞
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The traditional flapping wing aircraft relies on the crankshaft linkage mechanism to drive the flapping wings, and the flapping wings flutter up and down to generate lift. The efficiency is low, and the direction of the lift is not adjusted in any direction, and the fatigue strength of the flapping wing material is high.

Method used

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  • A rotating flapping wing thrust generating device with a spring
  • A rotating flapping wing thrust generating device with a spring

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Embodiment Construction

[0008] now attached figure 1 And attached figure 2 The present invention is illustrated by way of example.

[0009] A rotating flapping wing thrust generating device with a spring is composed of a main shaft 1, a rotating arm 2, a flapping wing 3, a wing shaft 4, a spring 5 and a hook 6; one end of the main shaft 1 is connected with the fuselage of a flapping wing aircraft through a bearing, and the rotating One end of the arm 2 is vertically fixed to the other end of the main shaft 1, and the other end of the rotating arm 2 is vertically fixed to one end of the wing shaft 4. The wing shaft 4, the rotating arm 2 and the main shaft 1 are in the same plane to form a crank, and the wing shaft 4 The other end of the flapping wing 3 is connected to the root of the flapping wing 3 through a bearing and is close to the leading edge of the flapping wing 3; 3 is fixed at the intersection of the end chord line and the trailing edge, and the other end of the spring 5 is connected to t...

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PUM

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Abstract

The invention relates to a rotary flapping wing thrust generation device provided with a spring, belonging to the technical field of aircrafts. The rotary flapping wing thrust generation device consists of a main shaft, a rotary arm, a flapping wing, a wing shaft, the spring and a hook, wherein a crank is formed by the main shaft, the rotary arm and the wing shaft; one end of the spring is fixedly connected with the flapping wing, and the other end of the spring is connected with a machine body by the hook. The flapping wing is driven to rotate along the circumference by an engine, and the air is flapped to generate thrust, so that the rotary flapping wing thrust generation device is high in efficiency and lower in requirement on the fatigue strength of material; the rotary flapping wing thrust generation device is simple in structure and more convenient in thrust direction adjustment, and can be used as a thrust device of the aircraft.

Description

technical field [0001] A rotary flapping wing thrust generating device with a spring belongs to the technical field of aircraft, and in particular relates to a thrust generating device for an aircraft. Background technique [0002] The traditional flapping wing aircraft relies on the crankshaft linkage to drive the flapping wings, and the flapping wings flutter up and down to generate lift. The efficiency is low, and the direction of the lift is not adjusted in any direction, and the fatigue strength of the flapping wing material is high. Contents of the invention [0003] The purpose of the present invention is to overcome the above-mentioned defects of traditional flapping-wing aircraft, and to invent a highly efficient rotatable flapping-wing thrust generating device similar to rolling wings. [0004] A rotating flapping-wing thrust generating device with springs, which is composed of a main shaft, a rotating arm, a flapping wing, a wing shaft, a spring and a hook; one ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C33/00
Inventor 王志成
Owner 丁霞