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Remote control coaxial type double rotor wing model helicopter control mechanism

A control mechanism and dual-rotor technology, applied in the field of aircraft, can solve the problems that the control structure is difficult to meet the requirements of different groups of people, and the sensitivity cannot be adjusted.

Inactive Publication Date: 2007-04-11
黄国川
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The control systems of the current remote control coaxial twin-rotor model helicopters are generally set, and their sensitivity cannot be adjusted; The model helicopter control system is required to have high sensitivity; the existing control structure is difficult to meet the requirements of different groups of people

Method used

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  • Remote control coaxial type double rotor wing model helicopter control mechanism
  • Remote control coaxial type double rotor wing model helicopter control mechanism
  • Remote control coaxial type double rotor wing model helicopter control mechanism

Examples

Experimental program
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Embodiment 1

[0013] Shown in Fig. 1 and Fig. 2, the control mechanism of a kind of remote control coaxial type twin-rotor model helicopter of the present invention comprises steering gear 1, lower connecting rod 2, swash plate, outer shaft 8, middle connecting rod 6, lower rotor Said steering gear 1 has two, and the rocking arm of two steering gears forms universal joint with the lower end of lower connecting rod 2 through the spherical body that its end is called ball head 101 respectively, and said swash plate There is a rotating ring 5 and a non-rotating ring 4, the rotating ring is fixed to the inner ring of a bearing, the non-rotating ring is fixed to the outer ring of the same bearing, the rotating ring 5 and the non-rotating ring 4 form a relatively rotatable connection, and the non-rotating ring There are two rocker arms 401 and 402 at an angle of 90° to each other on the 4, respectively controlling the longitudinal and lateral moments of the lower rotor. The two rocker arms are uni...

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PUM

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Abstract

The control mechanism for remotely controlled coaxial double rotary wing model helicopter can meet the requirements for different users to control the model helicopter in different sensitivity, and includes steering engine, lower connecting rod, wobbler with rotating cup and no-rotating cup, oar jig, outer shaft and middle connecting rod. The present invention features that each of the lower connecting rods is connected to 2 or more no-rotating cups and each of the middle connecting rods is connected to 2 or more round heads in the oar jig, so that the present invention has adjustable force arm length of the rocking arm and altered controlling sensitivity. The present invention makes it possible to select different connection position to reach proper control sensitivity.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a control mechanism of a coaxial double-rotor model helicopter. Background technique [0002] The stability of the remote control model helicopter is poor, and it has higher requirements for the control technology, especially compared with the person who has mastered certain control skills, the requirements for the control performance of the remote control model helicopter are quite different; beginners mainly It is to fly the remote control model helicopter smoothly and safely. In order to avoid the slow operation caused by the unskilled control technology, or the flight accident caused by the excessive control action, the sensitivity of the remote control model helicopter is generally set at However, for flight enthusiasts who have already mastered certain control techniques and need to further practice more difficult flight movements, the control performance of the remote con...

Claims

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Application Information

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IPC IPC(8): B64C27/54A63H27/20
Inventor 黄国川
Owner 黄国川
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