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Electronic type command ejection system

An electronic and command technology used in the field of aircraft lifesaving

Inactive Publication Date: 2018-03-02
CHINA AVIATION LIFESAVING INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is: to propose an electronic command ejection system, in order to solve the problem that the previous gas-fired command ejection system must be equipped with explosive bombs, delay bombs and gas pipelines as power, and to solve the problem that the front and rear seats are damaged after the explosive bombs are fired. The influence of the internal pressure of the pipeline reduces the installed weight and improves the use and maintainability
[0005] The advantages of the present invention are: an electronic command ejection system is proposed, in order to solve the problem that the previous gas type command ejection system must be equipped with explosive bombs, delay bombs and gas pipelines, and solve the problem of the front and rear seat pipes after the explosive bombs are fired. Reduce the influence of internal pressure of the road, reduce the installed weight, and improve the use and maintainability

Method used

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  • Electronic type command ejection system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0012] The selector switch 2 is a single-pole double-throw switch, and the front chair start switch 5 and the rear chair start switch 7 are single-pole single-throw switches. Front chair explosive bomb 4 and rear chair explosive bomb 6 are finished parts.

[0013] When the selector switch 2 is in the single state, the front seat ejection controller 1 and the rear seat ejection controller 3 receive the single state signal, the front seat occupant pulls the front seat start switch 5, and the front seat ejection controller 1 outputs ignition to the front seat ignition. Explosive bomb 4, so as to realize the ejection of the front seat out of the cabin; if the rear seat occupant starts the ejection, start the rear seat start switch 7, the rear seat ejection controller 3 outputs ignition to the rear seat explosive bomb 6, thereby realizing the ejection of the rear seat out of the cabin;

[0014] When the selection switch 2 is in the double state, the front seat ejection controller 1...

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PUM

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Abstract

The present invention belongs to the field of aircraft life-saving, and relates to an electronic type command ejection system. The electronic type command ejection system is characterized in that a front chair explosive cartridge and an electrically fired front chair explosive cartridge (4), and a rear chair explosive cartridge and an electrically fired rear chair explosive cartridge (6). The electronic type command ejection system also comprises a front chair ejection controller (1), a front chair enable switch (5), a selective switch (2), a rear chair ejection controller (3) and a rear chairenable switch (7). The present invention provides an electronic type command ejection system to solve the problem that in the prior art, a gas type command ejection system must be equipped with an explosion propagation cartridge, a delay cartridge and a gas pipeline, and to solve the influence on internal pressure of pipelines of the front and rear chairs after the explosion propagation cartridgefired, the installed weight is reduced, and use maintenance is improved.

Description

technical field [0001] The invention belongs to the field of aircraft lifesaving and relates to an electronic command ejection system. Background technique [0002] The command ejection system mainly realizes the automatic control of the sequence and time interval of emergency ejection of the occupants of the two-seater fighter. The system ensures that each crew member is automatically ejected according to a predetermined procedure, and can enable all crew members to eject quickly from the aircraft in the shortest possible time without interfering with each other in the air. In the single state, it is guaranteed that the pilot who initiates the ejection will eject. In the dual state, no matter who initiates the ejection, the rear seat is always ejected first, and the front seat ejects out of the cabin after a delay of about 0.35-0.55s. The active rocket ejection seat command ejection system uses gas as power when it works. The system needs to arrange corresponding pipelines...

Claims

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Application Information

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IPC IPC(8): B64D25/10
CPCB64D25/10
Inventor 李进董立强冯光辉
Owner CHINA AVIATION LIFESAVING INST