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Fixed-wing aircraft aileron control mechanism and fixed-wing aircraft

An aileron control and fixed wing technology, applied in the field of aircraft, can solve the problems of high assembly and manufacturing costs, complex force transmission lines, long aileron wingspan, etc., and achieve the effects of easy assembly, simple overall structure and saving installation space.

Pending Publication Date: 2022-02-08
浙江省涡轮机械与推进系统研究院
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It is the main control surface of the aircraft, and the rolling moment generated by the pilot's control of the differential deflection of the left and right ailerons can make the aircraft do a rolling maneuver. The wingspan of the aileron is long and the chord is short; Aircraft aileron control structure, complex force transmission lines, high assembly and manufacturing costs

Method used

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  • Fixed-wing aircraft aileron control mechanism and fixed-wing aircraft
  • Fixed-wing aircraft aileron control mechanism and fixed-wing aircraft
  • Fixed-wing aircraft aileron control mechanism and fixed-wing aircraft

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Embodiment Construction

[0034] Below in conjunction with each accompanying drawing, the present invention is described in detail.

[0035] Such as figure 1 , figure 2 , image 3 as well as Figure 5 As shown, a fixed-wing aircraft aileron control mechanism is used to control the rotation of the aileron 1 installed on the fixed wing. The aileron 1 is used to roll the fuselage of the aircraft. The control mechanism includes the axis relative to the fuselage The first control unit and the second control unit are arranged symmetrically, and each of the first control unit and the second control unit includes:

[0036] The driving rod 2 is provided with a connecting seat 3, and the connecting seat 3 is connected with a lower connecting rod 4;

[0037] The flexible shaft 5, the input end of the flexible shaft 5 is connected with the lower link 4 through the lower rocker arm 6, and the output end of the flexible shaft 5 is connected with the torsion bar 7;

[0038] An internal connecting rod 17, which ...

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Abstract

The invention discloses a fixed-wing aircraft aileron control mechanism and a fixed-wing aircraft, wherein the control mechanism comprises a first control unit and a second control unit which are symmetrically arranged relative to the axis of an aircraft body, each of the first control unit and the second control unit comprises a steering column, the steering column is provided with a connecting seat, and the connecting seat is connected with a lower connecting rod; a flexible shaft, wherein an input end of the flexible shaft is connected with the lower connecting rod through a lower rocker arm, and the output end of the flexible shaft is connected with a torsion bar; an internal connecting rod which is located in the fixed wing, one end of the internal connecting rod is connected with the torsion bar, and the other end of the internal connecting rod is connected with an upper rocker arm; an aileron connecting rod, of which one end is connected with the upper rocker arm, and the other end is connected with the aileron. The control mechanism is simple in overall structure, labor-saving in use, convenient to assemble, economical and practical.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to an aileron control mechanism of a fixed-wing aircraft and the fixed-wing aircraft. Background technique [0002] Aircraft aileron refers to a small movable wing surface installed on the outside of the trailing edge of the fixed wing of the aircraft. It is the main control surface of the aircraft, and the rolling moment generated by the pilot's control of the differential deflection of the left and right ailerons can make the aircraft do a rolling maneuver. The aileron has a long span and a short chord; Aircraft aileron control structure, complex force transmission lines, high assembly and manufacturing costs. Contents of the invention [0003] Aiming at the above problems, the present invention proposes a fixed-wing aircraft aileron control mechanism and the fixed-wing aircraft. [0004] The technical scheme adopted by the present invention is as follows: a fixed-wing aircraft aileron...

Claims

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Application Information

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IPC IPC(8): B64C13/30
CPCB64C13/30
Inventor 周凯崔滔
Owner 浙江省涡轮机械与推进系统研究院
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