Control system for reciprocating displacement pump of solid-liquid rocket engine

A solid-liquid rocket and control system technology, applied in the aerospace field, can solve the problems of high reliability, variable thrust, light weight and fast response of attitude and orbit control engines.

Active Publication Date: 2021-04-02
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of this application is to provide a control system for a reciprocating volumetric pump used in a solid-liquid rocket engine, which can solve the problems in the prior art that cannot simultaneously satisfy the high reliability, variable thrust, light weight, quick response questions

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  • Control system for reciprocating displacement pump of solid-liquid rocket engine
  • Control system for reciprocating displacement pump of solid-liquid rocket engine

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Embodiment Construction

[0045] The technical solutions of the present application will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present application, not all of them. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the scope of protection of this application.

[0046]In the description of this application, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present application and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, use a speci...

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Abstract

The invention relates to the technical field of aerospace, in particular to a control system for a reciprocating type positive displacement pump of a solid-liquid rocket engine. The system comprises astorage mechanism and a liquid pressurizing mechanism; the storage mechanism is used for storing propellant; and the liquid pressurizing mechanism comprises a reciprocating type positive displacementpump, the storage mechanism is communicated with the reciprocating type positive displacement pump, and the reciprocating type positive displacement pump is used for pressurizing propellant and supplying the pressurized propellant to the attitude and orbit control engine mechanism. The liquid pressurizing mechanism is different from a traditional extrusion type or turbine pump pressure type conveying system, a high-pressure gas cylinder and a turbine pump assembly are not used any more, the propellant flowing out of the storage mechanism is pressurized through the light reciprocating type positive displacement pump, and the propellant can have high specific impulse performance.

Description

technical field [0001] The present application relates to the field of aerospace technology, in particular to a control system for a reciprocating displacement pump of a solid-liquid rocket engine. Background technique [0002] The attitude and orbit control engine is an important part of rockets, satellites, and upper-level spacecraft, which can determine the maneuverability of the spacecraft and the accuracy of orbiting. With the continuous development and innovation in the field of aerospace technology, the existing attitude and orbit control engines are mostly solid rocket engines and liquid hydrazine engines. Although the structure of the solid rocket engine is simple, it is difficult to switch on and off many times, so it cannot meet the needs of the upper stage in the future. High maneuverability requirements of spacecraft. The liquid hydrazine engine has a large thrust and can be adjusted by changing the flow rate, but the design is complicated, the technology is cu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/72
CPCF02K9/72
Inventor 蔡国飙李心瞳张源俊周闯魏天放
Owner BEIHANG UNIV
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