Control mechanism for flight simulator

A technology of flight simulator and control mechanism, which is applied in the field of flight simulators, can solve problems such as inability to train aircraft to limit training, and achieve the effects of improving stability, improving training effects, and improving use effects

Pending Publication Date: 2021-12-07
SHANGHAI ZHONGFANG COMP TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Aiming at the deficiencies of the prior art, the present invention provides a control mechanism for flight simulators, which solves the problem that the existing flight simulators cannot train the aircraft to perform extreme training in the case of severe shaking out of control

Method used

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  • Control mechanism for flight simulator
  • Control mechanism for flight simulator
  • Control mechanism for flight simulator

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Embodiment Construction

[0026] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0027] see Figure 1-5 , a control mechanism for a flight simulator in this embodiment includes a vibration mechanism 1 , a buffer mechanism 2 and a rotation mechanism 3 , and both the buffer mechanism 2 and the rotation mechanism 3 are arranged on the vibration mechanism 1 .

[0028] It should be noted that the vibration mechanism 1 in this embodiment is a structure for simulating the severe shaking of the aircraft when it is out of control, the buffer mechan...

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Abstract

The invention relates to a control mechanism for a flight simulator. The control mechanism comprises a vibration mechanism, a buffer mechanism and a rotating mechanism; the buffer mechanism and the rotating mechanism are both arranged on the vibration mechanism; the vibration mechanism comprises a bottom plate, two fixing plates and a driving part located between the two fixing plates are arranged at the top of the bottom plate, a rotating rod is rotationally connected to the front face of each fixing plate, a driven wheel and a disc are fixedly installed on the outer side of each rotating rod, and a connecting rod is hinged to the front face of each disc; a hinge block is hinged to the end, away from the disc, of the connecting rod, and a push rod is fixedly mounted at the top of the hinge block. According to the control mechanism for the flight simulator, through cooperation of the vibration mechanism, the buffer mechanism and the rotating mechanism, limit training can be truly simulated under the condition that an airplane is out of control and violently shakes, the special training requirement of flight simulation is met, and therefore the training effect of the flight simulator is improved.

Description

technical field [0001] The invention relates to the technical field of flight simulators, in particular to a control mechanism for flight simulators. Background technique [0002] In a broad sense, a flight simulator is a machine used to simulate the flight of an aircraft, such as a device that simulates the flight of an aircraft, missile, satellite, spacecraft, etc., can be called a flight simulator, which can reproduce the aircraft and the air environment. In a narrow sense, a simulation device that can be operated is a device that is used to simulate the flight of an aircraft and has a relatively complex structure and relatively complete functions. [0003] At present, pilot students often use flight simulators in the flight training process, but most of the existing flight simulators use multi-angle platforms to achieve multi-angle adjustments to control the attitude of the simulated aircraft, and this method of control simulation can only be controlled according to The...

Claims

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Application Information

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IPC IPC(8): G09B9/08G09B9/10G09B9/12G09B9/20
CPCG09B9/08G09B9/10G09B9/12G09B9/206
Inventor 梁琳叶亮
Owner SHANGHAI ZHONGFANG COMP TECH
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