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Storage and supply device for rocket engine igniter

A rocket engine and supply device technology, applied to rocket engine devices, machines/engines, jet propulsion devices, etc., can solve problems such as inability to realize liquid supply management, inability to achieve gas-liquid isolation of igniting agent and pressurized gas, and inability to replace them

Active Publication Date: 2021-12-14
北京天兵科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The ignition guide is installed in the fuel pipeline system, and the capacity is the dose used for one ignition; the isolation and sealing device is a welded structure, which cannot be replaced after use
The above characteristics determine that the ignition duct can only be used for an engine system that starts once; at the same time, the ignition duct cannot realize the gas-liquid isolation of the ignition agent and the pressurized gas, and cannot realize the liquid supply management under complex overload conditions

Method used

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  • Storage and supply device for rocket engine igniter
  • Storage and supply device for rocket engine igniter
  • Storage and supply device for rocket engine igniter

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Embodiment Construction

[0031] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in combination with specific embodiments and with reference to the accompanying drawings. It should be understood that these descriptions are exemplary only, and are not intended to limit the scope of the present invention. Also, in the following description, descriptions of well-known structures and techniques are omitted to avoid unnecessarily obscuring the concept of the present invention.

[0032] The structural composition of the present invention includes: shell assembly 1, metal bellows assembly 2, gas path isolation assembly 3, liquid path isolation assembly 4, gas path filling valve 5, liquid path filling valve 6, filter 7, gas path Redundant sealing joint 8 and redundant sealing joint 9 of liquid circuit.

[0033] The shell assembly 1 includes a shell column section 1-1, a gas path head 1-2, and a liq...

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Abstract

The invention relates to a rocket engine igniter storage and supply device, which mainly includes a shell assembly, a metal bellows assembly, a gas path isolation assembly and a liquid path isolation assembly. The igniter is a strong chemically active substance, and its storage and use require oxygen and water to isolate the environment. The present invention uses a metal shell, a metal diaphragm box, a gas path and a liquid path isolation diaphragm to realize the sealed storage of the igniter liquid; during the supply process of the igniter , the metal diaphragm box is used as a management element to ensure complete gas-liquid isolation, and the metal diaphragm box can be reused many times; the gas path and liquid path isolation diaphragms are connected to the module housing with redundant sealing joints, which can not only be reliably sealed, but also It can be easily replaced; the addition and discharge valve is used for the filling of igniter liquid and positive pressure inert gas packaging, and the pressure sensor is used to monitor the pressure of the air cavity in the module to ensure a positive pressure safe storage environment. Through the above features, the safe and reliable storage of the ignition agent liquid can be realized, and it has the characteristics of multiple supply and reusable use.

Description

technical field [0001] The invention relates to the technical field of liquid rocket engines, in particular to a rocket engine igniter storage and supply device. Background technique [0002] For rocket engines with a combination of liquid oxygen and hydrocarbon propellants, since the propellant combination cannot spontaneously ignite, a special ignition system is required for engine ignition. Ignition starting with a self-igniting igniter has been widely proven to be a reliable, compact and efficient ignition scheme. Its main working principle is: install a special container pre-filled with igniting agent in the engine fuel pipeline system, press the pressurized gas to squeeze the igniting agent into the engine combustion chamber, the igniting agent and liquid oxygen undergo a spontaneous combustion reaction, and then organize fuel injection. Into the mixed combustion, to achieve ignition. The storage and supply module of igniter is an important part of the ignition syste...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K9/44F02K9/50F02K9/60
CPCF02K9/44F02K9/50F02K9/605
Inventor 沈涌斌田伟枫康永来朱正辉
Owner 北京天兵科技有限公司