Device and method for detecting one-way reliability of carrier rocket two-out-of-three ignition circuit

An ignition circuit and launch vehicle technology, applied in electronic circuit testing, electrical testing/monitoring, etc., can solve problems such as hidden safety hazards and difficulty in assessing single-circuit reliability, and achieve improved reliability, single-circuit reliability, and automatic The effect of reading

Active Publication Date: 2014-07-02
SHANGHAI SPACEFLIGHT ELECTRONICS & COMM EQUIP RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, there is a problem that the reliability of a single circuit of the three-choice two ignition circuit of the launch vehicle is difficult to assess. Although a failure of a single circuit in the three-choice two ignition circuit will not cause the impact of a wrong ignition command, if the single-circuit fault is not repaired in time, if other If the path fails, there will be a safety hazard

Method used

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  • Device and method for detecting one-way reliability of carrier rocket two-out-of-three ignition circuit
  • Device and method for detecting one-way reliability of carrier rocket two-out-of-three ignition circuit

Examples

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Embodiment 1

[0024] First, a general description of the three-choice two ignition circuit is given, such as figure 1 As shown, the three-choice two ignition circuit includes a three-way ignition PLC (ie figure 1 The ignition PLC 4a, ignition PLC 4b and ignition PLC 4c) and the contactor circuit 5, the three-way ignition PLC are respectively connected to the contactor circuit 5; among them, the ignition PLC is used to receive the ignition command, and output the PLC timing signal after logical judgment ; The contactor circuit 5 is used to receive the three-way PLC timing signal, perform a voting operation of two out of three, and output the final ignition timing signal. Due to the adoption of the output mode of choosing two out of three, even if one ignition PLC fails, the normal output of the ignition timing signal can be guaranteed, and the ignition action of the launch vehicle will not be affected.

[0025] Since the failure of a single circuit in two of the three ignition circuits does...

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PUM

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Abstract

The invention discloses a device for detecting the one-way reliability of a carrier rocket two-out-of-three ignition circuit. The device comprises a testing microcomputer, an instruction simulator and a timing sequence receiving unit, wherein the testing microcomputer is connected with the instruction simulator and the timing sequence receiving unit. The instruction simulator is used for sending a simulated ignition instruction to an ignition PLC. The timing sequence receiving unit is used for receiving a PLC timing sequence signal output by a three-way ignition PLC and an ignition timing sequence signal output by a contactor circuit. The testing microcomputer is used for controlling work of the instruction simulator and work of the ignition PLC, and further used for reading the PLC timing sequence signal and the ignition timing sequence signal from the timing sequence receiving unit and judging whether the timing sequence requirement is met according to a preset judgment method. The device for detecting the one-way reliability of the carrier rocket two-out-of-three ignition circuit has the advantages that the one-way reliability of the two-out-of-three ignition circuit is examined, the timing sequence of the ignition circuit is automatically interpreted, and the use reliability of the two-out-of-three ignition circuit is improved.

Description

technical field [0001] The invention belongs to the technical field of launch vehicle ground equipment, and in particular relates to a detection device and method for evaluating the single-circuit reliability of a launch vehicle's three-select-two ignition circuit. Background technique [0002] At present, there is a problem that the reliability of a single circuit of the three-choice two ignition circuit of the launch vehicle is difficult to assess. Although a failure of a single circuit in the three-choice two ignition circuit will not cause the impact of a wrong ignition command, if the single-circuit fault is not repaired in time, if other If the path fails, there will be a security risk. Therefore, there is an urgent need for a detection device and detection method that can timely evaluate the performance of a single ignition circuit of three selections, so that when a single ignition circuit has a fault, it can be detected in time, thereby improving the reliability of ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01R31/28G05B23/02
Inventor 赵阳魏永国蔡珂
Owner SHANGHAI SPACEFLIGHT ELECTRONICS & COMM EQUIP RES INST
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