Simulation aeroengine starting switch

A technology for starting switches and aircraft engines, which is applied in the field of flight simulation, can solve problems such as increasing costs, and achieve the effects of reducing external dimensions, improving authenticity, and good integration effects

Pending Publication Date: 2018-07-24
哈尔滨莱特兄弟飞行技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, there is no simulation engine start switch specially used for simulating the real engine start switch in the market. Basically, it is used by combining multiple existing switches, which results in the diversification of the used parts and the large size. , also increases the cost, so it is imperative to develop a low-cost engine start switch for flight simulators

Method used

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  • Simulation aeroengine starting switch
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  • Simulation aeroengine starting switch

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Embodiment Construction

[0025] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.

[0026] The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0027] Such as Figure 1-Figure 6 Shown, a kind of simulated aircraft engine starting switch comprises a cuboid-shaped hollow frame surrounded by housing 20, upper mounting plate 3, and lower mounting plate 21, pressing and pulling assembly, rotating assembly, limit assembly, solenoid valve 18 and wave band The switch assembly, the pressing and pulling assembly is connected to the rotating assembly through the upper mounting plate 3, the band switch assembly is connected to the rotating assembly passing through the lower mounting plate 21, the rotating assembly, the limit assembly and the solenoid valve 18 are all arranged in a hollow frame, the pressing and pulling assembly drives the ...

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Abstract

The invention provides a simulation aeroengine starting switch comprising a cuboid type hollow framework formed by a housing, an upper mount plate and a lower mount plate, a press-pull assembly, a rotary assembly, a limit assembly, a solenoid valve and a wave band switch assembly; the press-pull assembly penetrates the upper mount plate and is connected with the rotary assembly; the wave band switch assembly penetrates the lower mount plate and is connected with the rotary assembly; the rotary assembly, the limit assembly and the solenoid valve are respectively arranged in the hollow framework; the press-pull assembly drives the rotary assembly to rotate; the limit assembly is arranged on the periphery of the rotary assembly; the limit assembly limits the rotation of the rotary assembly; the solenoid valve controls the limit assembly to / not to limit the rotation of the rotary assembly, and fixed on the lower mount plate. The simulation aeroengine starting switch is compact in layout, small in size, good in simulation effect, and can realize manual and automatic reset dual-function.

Description

technical field [0001] The invention belongs to the technical field of flight simulation, in particular to a simulation aircraft engine start switch. Background technique [0002] In recent years, with the continuous development of the aviation market, the demand for simulation simulators has also increased. If a flight simulation simulator wants to simulate an aircraft realistically, the engine start switch is an essential part. At present, there is no simulation engine start switch specially used for simulating the real engine start switch in the market. Basically, it is used by combining multiple existing switches, which results in the diversification of the used parts and the large size. , also increases the cost, so it is imperative to develop a low-cost engine start switch for flight simulators. Contents of the invention [0003] In view of this, the present invention aims to propose a simulated aircraft engine start switch, which has a compact structure and layout,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01H19/10H01H19/14H01H19/03H01H3/20
CPCH01H19/10H01H3/20H01H19/03H01H19/14
Inventor 吕洪亮付强
Owner 哈尔滨莱特兄弟飞行技术有限公司
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