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Flap switch control device of flight simulator

A technology of flight simulators and control devices, which is applied to simulators, simulators, and instruments for space navigation conditions. The effect of dashboard space

Pending Publication Date: 2018-03-06
哈尔滨翼拟科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The size of the existing flap handle device is too large and too long, causing the central instrument panel to collide with the steering wheel after being installed in the simulated cockpit. To solve this problem, it is necessary to improve the structure of the flap handle device so that it can maintain the original In addition to the function, it becomes compact and meets the installation position relationship between the steering wheel and the central dashboard

Method used

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  • Flap switch control device of flight simulator
  • Flap switch control device of flight simulator
  • Flap switch control device of flight simulator

Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment approach 1

[0024] Specific implementation mode one: combine Figure 1-Figure 3 Describe this embodiment, a flight simulator flap switch control device in this embodiment includes a connecting plate 1, a bottom plate 2, a handle 3, a potentiometer mounting frame 4, a circular potentiometer 5, a rotating support 6, and a handle rod 7. The elastic ball head positioning plunger 10, the rotating disc 11 and the rotating shaft 12, the connecting plate 1 is L-shaped, one side is connected and fixed with the bottom plate 2 with bolts, and the other side is fixed with the instrument panel panel with bolts. The potentiometer mounting frame 4 is installed on the bottom plate 2, the circular potentiometer 5 is mounted on the potentiometer mounting frame 4, the output shaft of the circular potentiometer 5 is inserted into the cylindrical hole of the rotating support 6, and is locked with a jacking screw, and the rotating support 6 is fixed on the rotating disc 11 with bolts, and the rotating disc 11 ...

specific Embodiment approach 2

[0025] Specific implementation mode two: combination Figure 1-Figure 3 To illustrate this embodiment, the rotary shaft 12 of a flap switch control device for a flight simulator in this embodiment is a disk, and the side end surface of the disk is stepped. With such arrangement, under the structure of the stepped disk, the rotation of the rotating disk 11 mounted on the rotating shaft 12 is more sensitive, and the rotation blocking effect is significantly reduced.

specific Embodiment approach 3

[0026] Specific implementation mode three: combination Figure 1-Figure 3 Describe this embodiment, one end of the handle rod 7 described in a flight simulator flap switch control device of this embodiment is installed on the rotating disk 11 through two mechanism bolts 8, and one of the mechanism bolts 8 is covered with a long Spring 13, two short springs 9 are sheathed on the other mechanism bolt 8, and described handle bar 7 is installed on the two mechanism bolts 8, and with long spring 13 and short spring 9 stuck position. In this way, two mechanism bolts 8 are installed on the rotating disk 11, one mechanism bolt 8 is covered with a long spring 13, and one mechanism bolt 8 is covered with two short springs 9; the handle bar 7 is installed on the two mechanism bolts 8 and the long spring 13 and the short spring 9 hold the position; the handle 3 is installed on the outer end of the handle rod 7, since the handle rod 7 is fixed on the mechanism bolt 8, and the mechanism bol...

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Abstract

The invention provides a flap switch control device of a flight simulator, belongs to the technical field of flight simulation driving equipment, and solves the problem that a central instrument panelcollides with a control column after installation in a simulation cabin since the dimension of a conventional flap handle device is over-large and over-long. The device comprises a connection board,a base plate, a handle, a potentiometer mounting rack, a circular potentiometer, a rotary supporting seat, a handle rod, elastic ball positioning plungers, a rotating disc and a rotating shaft, the connection board is connected with the base plate, the potentiometer support is arranged on the base plate, the circular potentiometer is arranged on the potentiometer support, an output shaft of the circular potentiometer is inserted into a cylindrical hole of the rotary supporting seat, the rotary supporting seat is fixed on the rotating disc through a bolt, the rotating disc is rotatably arrangedon the rotating shaft, the rotating shaft is fixed on the base plate, the rotating disc is provided with two elastic ball positioning plungers, one end of the handle rod is arranged above the rotating disc, and the other end of the handle rod is provided with the handle. According to the device, the structure is simple, small and light, and the space of the instrument panel is effectively and reasonably saved.

Description

technical field [0001] The invention relates to a flight simulator flap switch control device, which belongs to the technical field of flight simulation driving equipment. Background technique [0002] Aircraft flight simulator is a typical human-in-the-loop simulation system. It is a flight motion simulation device based on flight kinematics. It integrates virtual reality technology, 3D real-time rendering technology, computer graphics technology, computer interface technology and multimedia, etc. Advanced technology, simulating the flight status, flight environment and flight conditions of the aircraft when performing flight missions, and providing pilots with test and training devices with similar operating loads, vision, hearing, and kinematic sensations. It usually consists of five major parts: simulated cockpit, motion system, visual system, computer system and instructor console. [0003] Flap refers to an airfoil-shaped movable device on the edge of the modern wing....

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G09B9/08
CPCG09B9/08
Inventor 范敏毅
Owner 哈尔滨翼拟科技有限公司