A solid rocket motor nozzle assembly connection sealing structure

A technology for engine nozzles and solid rockets, which is applied to rocket engine devices, machines/engines, mechanical equipment, etc. It can solve problems such as temperature shock resistance, high impact, and limited structural space, and achieve high connection strength and connection reliability. High, simple processing effect

Active Publication Date: 2020-01-31
HUBEI INST OF AEROSPACE CHEMOTECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In particular, it provides a connection method with high reliability, simple and compact structure, and simple processing technology to solve the connection structure of nozzle components such as limited structural space, large impact, high weather resistance, and temperature shock resistance performance requirements.

Method used

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  • A solid rocket motor nozzle assembly connection sealing structure
  • A solid rocket motor nozzle assembly connection sealing structure
  • A solid rocket motor nozzle assembly connection sealing structure

Examples

Experimental program
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Embodiment Construction

[0016] figure 1 Among them, the present invention includes a nozzle housing 1, a sealant 2 for sealing the connection gap, a retaining ring 3 for connection and fixing, and a nozzle expansion section 4 for limiting the throat liner and converting energy. The stop ring 3 is placed in the concave annular installation groove and the limit groove corresponding to the nozzle expansion section 4, the sealant 2 is basically evenly applied on the corresponding surface of the nozzle expansion section 4, and then the stop ring 3 and The corresponding thread of the nozzle housing 1 enables the nozzle expansion section 4 to be firmly connected to the rear section of the nozzle housing 1, and enables the sealant 2 applied on the nozzle expansion section 4 to be evenly distributed on the corresponding curved surface , to fill up the corresponding curved surfaces of the nozzle housing 1 and the nozzle expansion section 4 that need to be sealed. During the installation and docking process of...

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Abstract

The invention relates to a connecting sealing structure of a nozzle assembly of a solid rocket engine. The spray pipe expansion section is a cylindrical structure with an inner cavity in a trumpet shape, a first step, a second step and a third step are sequentially arranged on the outer surface of the spray pipe expansion section, the spray pipe shell is sleeved outside the spray pipe expansion section, the inner cavity of the spray pipe shell is provided with a first step groove, a second step groove and a third step groove, the first step groove and the second step groove, and the third stepis matched, a sealant is arranged between the first step of the nozzle expanding section and the first step groove of the nozzle shell, the second step part of the spray pipe expansion section is provided with a concave annular installation groove, and the retaining ring is arranged in the concave annular mounting groove and forms a thread pair with the spray pipe shell. The structure can be applied to the connection of almost all small solid rocket engine nozzle assemblies, in particular, to address such limitations as structural space, it is desirable to withstand higher impact and higher weatherability, the nozzle assembly connecting structure with the problems of temperature shock resistance performance requirement and the like provides a high reliability. the structure is simple andcompact, and the processing technology is simple and convenient.

Description

technical field [0001] The invention relates to a small solid rocket motor nozzle assembly connection and sealing structure, which is used for the connection and sealing of the small solid rocket motor nozzle and belongs to the field of solid rocket motor structure design. Background technique [0002] The nozzle expansion section of small solid rocket motors is generally made of non-metallic materials, which not only plays a role in positioning and fixing the throat liner, but also plays a role in heat insulation and sealing, and also plays a role in improving the energy conversion efficiency of the engine. [0003] The nozzle assembly is a key component of the solid rocket motor, and the fixing of the nozzle assembly, the sealing of the body and the sealing of the joint between the nozzle assembly and the engine are the most important. For the design of small solid rocket motors, due to the limited envelope size, installation space and mass of the nozzle assembly, the conn...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K9/97
Inventor 余小波王鹍鹏邓康清朱雯娟王相宇向进杨育文罗国芳田献林李颖
Owner HUBEI INST OF AEROSPACE CHEMOTECHNOLOGY
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