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Simulated aircraft large-angle turning control device

A control device and large-angle technology, applied in simulators, simulators of space navigation conditions, transportation and packaging, etc., can solve problems such as easy swings and poor simulation effects, and achieve accurate rotation measurement, low cost, and simple structure Effect

Inactive Publication Date: 2018-05-18
安徽英釜航空科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the force provided by the spring changes greatly, and the handwheel is prone to swing when it is reset, and the simulation effect is poor

Method used

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  • Simulated aircraft large-angle turning control device

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Embodiment Construction

[0013] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0014] as attached figure 1 The shown control device for simulating large-angle turns of an aircraft according to the present invention includes a frame body 1, a rotating shaft 2, an upper gear 3, a rotating disc 4, connecting bolts 5, wing plates 6, potentiometers 7, and fixing flanges 8 , hand wheel 9, connecting plate 10, lower gear 11, rotating ball 12, reset damping rod 13, telescoping rod 14, base 15 and mounting hole 16, the upper end of the frame body 1 is fixedly connected with the rotating disc 4 through the rotating shaft 2 ; The upper gear 3 is installed near the end of the rotating shaft 2; the rotating disk 4 is connected with the fixed flange 8 through the connecting bolt 5; a handwheel 9 is installed on the outer surface of the fixed flange 8; The lower edge of the rotating disk 4 is provided with a wing plate 6; the...

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Abstract

The invention relates to a simulated aircraft large-angle turning control device. An upper end of a frame body is fixedly connected with a rotating disc through a rotating shaft; an upper gear is mounted near the end of the rotating shaft; the rotating disc is connected with a fixed flange through connecting bolts; a hand wheel is mounted on the outer side of the fixed flange; a wing plate is provided at the lower edge of the rotating disc; a connection plate is fixedly mounted on the wing plate; a potentiometer is mounted on the upper end of the connection plate; a lower gear is connected tothe input end of the potentiometer; the upper gear and the lower gear are meshed together; the lower end of the frame body is equipped with a rotating ball; the lower end of the rotating ball is fixedwith a reset damper rod; the reset damper rod is provided with a telescopic rod; the lower end of the telescopic rod is fixedly provided with a base; and the base is provided with mounting holes. Thetechnical solution of the present invention can provide the simulated aircraft large-angle turning control device with convenient disassembly and assembly, low cost, smooth change of damping force, and good simulation effect.

Description

technical field [0001] The invention relates to the technical field of flight simulation machinery, in particular to a large-angle turning control device for simulating an aircraft. Background technique [0002] The flight simulation equipment is to make the driver's driving experience high-fidelity. In terms of visual senses, it simulates the external situation of the aircraft, so that the pilot can judge the attitude, position, altitude, speed and weather of the aircraft, and play a role in driving. The effect of personnel training and training, reduce training costs, and speed up training. When an aircraft taxis on the ground, it turns by changing direction with its steering wheels, usually the front wheels. The tires on the landing gear of the aircraft are in contact with the ground, the main landing gear plays the role of support and rolling and sliding, and the front landing gear plays the role of balance and steering. The pilot operates the steering hand wheel and c...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/28
CPCG09B9/28
Inventor 徐舒青
Owner 安徽英釜航空科技有限公司
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