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Ignition safety system of multistage rocket engine and detection method of ignition safety system

A technology for a rocket engine and a safety system, applied in the field of rockets, can solve the problems of poor testability of cable network resources during flight, occupation of detection methods, etc., so as to improve system redundancy and reliability, simplify design complexity, and achieve rapid positioning. Effect

Active Publication Date: 2020-07-10
北京中科宇航技术有限公司
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Problems solved by technology

[0005] The purpose of this application is to provide a multi-stage rocket engine ignition safety system and its detection method to solve the problem that the detection method occupies too much cable network resources and the testability of the flight process is poor

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  • Ignition safety system of multistage rocket engine and detection method of ignition safety system
  • Ignition safety system of multistage rocket engine and detection method of ignition safety system
  • Ignition safety system of multistage rocket engine and detection method of ignition safety system

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Embodiment Construction

[0025] The technical solutions in the embodiments of the present application are clearly and completely described below in combination with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by those skilled in the art without making creative efforts belong to the scope of protection of this application.

[0026] The application relates to an ignition safety system of a multistage rocket engine and a detection method thereof. According to the present application, the problem that the detection method occupies too much cable network resources and the testability of the flight process is poor is solved.

[0027] See figure 2 , is a schematic diagram of the multi-stage rocket engine ignition safety system provided in the embodiment of the present application, including: ground measurem...

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Abstract

The application discloses an ignition safety system of a multistage rocket engine and a detection method of the ignition safety system. The ignition safety mechanism of a multistage rocket engine comprises a ground testing and launching control system, an N-stage ignition safety mechanism and an N-stage intelligent detection combination, wherein the N-stage intelligent detection combination is used for detecting and recording the operating states of corresponding all stages of ignition safety mechanisms, and transmitting the operating states to the ground testing and launching control system;and the ground testing and launching control system is used for detecting the insurance states and the operating states of the ignition safety mechanisms and receiving the recorded operating state ofthe ignition safety mechanisms, detected by the N-stage intelligent detection combination, and according to the insurance states and / or the operating states of the ignition safety mechanisms, detecting the safety states of the ignition safety mechanisms. Through the adoption of the ignition safety system of the multistage rocket engine and the detection method of the ignition safety system disclosed by the invention, all the stages of the ignition safety mechanisms are connected in series, so that the design complexity of a cable network is simplified, and the weight of the cable network is reduced.

Description

technical field [0001] The present application relates to the field of rockets, in particular to an ignition safety system of a multi-stage rocket engine and a detection method thereof. Background technique [0002] Multi-stage rocket engines generally ensure the safety of use by controlling the ignition safety mechanism, prevent accidental detonation of the engine, and ensure the safety of personnel, launch equipment, site facilities and aerospace vehicles. In order to improve the operation and control safety of the ignition safety mechanism, the relay logic mutual exclusion interlocking control principle is generally adopted, and the state of the ignition safety mechanism is divided into an insurance state and a working state, and the two states are logically mutually exclusive. The current detection methods for multi-stage rocket engines are as follows: figure 1 shown. The ground measurement and control system connects the safety status (K1bx, K2bx...KNbx) and working s...

Claims

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Application Information

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IPC IPC(8): F02K9/38F02K9/96
CPCF02K9/38F02K9/96
Inventor 郭文正辛哲奎朱永泉杨毅强
Owner 北京中科宇航技术有限公司
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