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Solid engine ignition circuit with ignition redundancy

A technology of solid motor and ignition circuit, which is applied in the direction of rocket motor devices, machines/engines, mechanical equipment, etc., to achieve the effect of improving reliability

Inactive Publication Date: 2020-10-16
南京云睿航天科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a solid engine ignition circuit with redundant ignition, which is used to solve the safety protection of the existing solid engine ignition heads for daily storage and transportation and the electrical protection before use

Method used

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  • Solid engine ignition circuit with ignition redundancy

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Embodiment 1

[0019] see figure 1 , a solid engine ignition circuit with redundant ignition heads, the ignition circuit includes a first relay U1, a second relay U2, a first triode Q1, a first resistor R1, a capacitor C1, a first diode D1, Safety switch S1, first ignition head DHT, second transistor Q2, second diode D3, second resistor R2, third resistor R3, third transistor Q3, second ignition head DHTB, fourth and third Diode Q4, fourth diode D4 and fourth resistor R4;

[0020] The first relay U1 includes two paths, each path includes a common terminal G, a normally closed terminal C and a normally open terminal H; the positive pole of the coil power supply terminal of the first relay U1 is connected to the first triode Q1 Collector, the negative pole of the coil power supply end of the first relay U1 is grounded; both ends of the coil of the first relay U1 are connected to the first diode D1, and the conduction direction of the first diode D1 points to the coil of the first relay U1 Th...

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PUM

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Abstract

The invention discloses a solid engine ignition circuit with ignition redundancy. The solid engine ignition circuit comprises a first relay, a second relay, a first triode, a first resistor, a capacitor, a first diode, a safety switch, a first ignition head, a second triode, a second diode, a second resistor, a third resistor, a third triode, a fourth triode, a fourth diode and a fourth resistor;two ends of a coil of the first relay are connected with the first diode, and the current flow direction of the first diode points to the positive pole of the power supply end of the coil of the firstrelay; the normally closed end of a first path of the first relay is connected with the power supply positive pole of the first ignition head; the common end and the normally closed end of the firstpath of the first relay are connected with two ends of the safety switch; the normally open end of the first path of the first relay is connected with the normally open end of a second path; and the common end and the normally closed end of the second path of the first relay are connected with two ends of the first ignition head. The issues of safety protection for daily storage and transportationof an existing solid engine ignition head and electrical protection before use are solved.

Description

technical field [0001] The invention belongs to the technical field of solid engine safety ignition circuits, and in particular relates to an ignition redundant solid engine ignition circuit. Background technique [0002] At present, due to the advantages of solid motors in transportation and storage, they are widely used in various rockets, guided bombs, missiles and various individual weapons. Since solid motors are explosive substances, the ignition head of solid motors is electrically sensitive. Most of the existing solid motors have safety protection design. For large solid motors, they are often designed with mistriggered flameout devices. For small solid motors, most of the methods used are to store the two ends of the ignition head of the solid motor. It is kept in a conduction state during transportation to realize protection against abnormal discharge. [0003] However, there are potential safety hazards in the existing design of safety protection circuits for sma...

Claims

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Application Information

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IPC IPC(8): F02K9/95F02K9/38
CPCF02K9/38F02K9/95
Inventor 不公告发明人
Owner 南京云睿航天科技有限公司