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Actuating mechanism for flight simulator

A technology of flight simulation and actuators, applied in the field of flight simulation, can solve the problems of real feeling discount, etc., and achieve the effect of low simulation site requirements, low production cost, and small volume

Inactive Publication Date: 2019-04-12
NINGXIA UNIVERSITY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The flight experience generally brought by such flight simulators is very limited, and the real experience is greatly reduced

Method used

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  • Actuating mechanism for flight simulator
  • Actuating mechanism for flight simulator

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0035] The executive mechanism of the four-degree-of-freedom flight simulator of the present invention can complete the action requirements of the cockpit's climb, dive, yaw, and rotation roll. degrees, which in turn are the vertical movement and rotation along the vertical axis, and the forward and backward rotation and left and right rotation along the horizontal axis, as follows.

[0036] Action 1 (cockpit 4 moves up and down along the vertical axis): the hydraulic cylinder 132 of the lifting control and lowering device 1 is stretched, so that the two support rods 131 of the lifting bracket 13 rotate along the hinge point, driving the fixed base 11 and the lifting platform 12 The sliding shaft d in the shaft slot b of the shaft slides to both sides respectively, so that the lifting platform 12 is lifted horizontally, and the lifting platform 12 can carry the yaw device 2, the rotating device 3 and the cabin 4 to move up and down along the vertical axis.

[0037] Action 2 (r...

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Abstract

The invention discloses an actuating mechanism for a flight simulator. The actuating mechanism consists of a lifting device, a yaw mechanism, a rotating device and a cockpit, wherein the lifting device consists of a fixed base, a lifting platform and a lifting support; the yaw mechanism consists of a yaw shaft, a U-shaped bracket and a pitch driving shaft; the yaw shaft is arranged on the liftingplatform of the lifting device; the U-shaped bracket is fixedly arranged on the yaw shaft; the rotating device consists of a cross U-shaped bracket and a rotary driving shaft; the cross U-shaped bracket is arranged on the U-shaped bracket of the yaw device in a hinging manner and is in driving fit arrangement with the pitch driving shaft of the yaw device; the cockpit is arranged on the cross U-shaped bracket of the rotating device in a suspended manner, is hinged to the cross U-shaped bracket and is in fixed driving fit arrangement with the rotary driving shaft of the rotating device. The actuating mechanism has the advantages of simple operation, narrow activity range, no occupied space and low requirement on simulation sites; the actuating mechanism can finish climbing, diving, yawing and whole-cycle rotary turning of the control cabin and has high training comprehensive realistic intensity.

Description

technical field [0001] The invention belongs to the technical field of flight simulation, and in particular relates to an actuator of a flight simulation device. Background technique [0002] With the rapid development of the aerospace industry, the replacement of aircraft is accelerating, which puts forward higher requirements for the ability and quality of flight personnel, and also leads to a substantial increase in the cost of flight training. In order for the pilot to control the flight as soon as possible, the training of the flight personnel must be stepped up. The flight simulator is a device that can simulate the real flight status of the aircraft on the ground. It is not restricted by any site, environment, weather, air traffic control and many other factors. It can ensure the personal safety of the flight experiencer and the safety of the flight equipment. Make it an immersive real experience. [0003] Utilize flight simulation device to carry out training and b...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/12
CPCG09B9/12
Inventor 宿友亮刘墨迪王春秀慕松张南
Owner NINGXIA UNIVERSITY
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