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Expansion device and construction method for solid rocket motor charge

A technology of solid rockets and motors, which is applied in the direction of rocket motor devices, machines/engines, jet propulsion devices, etc., can solve problems such as air inclusions, and achieve the effects of ensuring construction quality, easy operation, and easy hoisting

Active Publication Date: 2021-06-18
HUBEI SANJIANG AEROSPACE JIANGHE CHEM TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The invention provides an expansion and tightening device and a construction method for solid rocket motor charging, which solves the problems of manual operation and air entrainment after the solid rocket motor large-diameter round tank drug blocks are bonded in pieces.

Method used

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  • Expansion device and construction method for solid rocket motor charge
  • Expansion device and construction method for solid rocket motor charge
  • Expansion device and construction method for solid rocket motor charge

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Embodiment Construction

[0024] The present invention will be further described below in conjunction with the examples, but the protection scope of the present invention is not limited to the scope expressed in the examples.

[0025] Such as Figure 1-4 As shown, a kind of expansion and tightening device for solid rocket motor charging includes a plurality of support plates 1, the support plates 1 are arranged vertically and form a circle, and there is a gap between two adjacent support plates, and each support plate The upper part and the lower part of the inner wall of the plate are respectively connected with at least one strut 8, and the center of the circle surrounded by the support plate 1 is provided with a fixed plate 2, which is arranged horizontally, and the center of which is vertically penetrated by a shaft sleeve 3, and the two ends of the shaft sleeve The first connecting plate 4, the second connecting plate 5 and the cylinder 6 are symmetrically arranged, and the output rod of the cylin...

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Abstract

The invention discloses a tensioning device and a construction method for charge of a solid rocket motor. The device includes a plurality of support plates, the support plates are arranged vertically and form a circle, and gaps are arranged between adjacent two support plates , the upper part and the lower part of the inner wall of each support plate are respectively connected with at least one support rod, and the center of the circle surrounded by the support plates is provided with a fixed plate. The first connecting plate, the second connecting plate and the cylinder are symmetrically arranged, and the output rod of the cylinder passes through the second connecting plate and the first connecting plate in turn and is fixed with the shaft sleeve; There is a fixing ring, and one end of the strut is connected with the support plate, and the other end is connected to the fixing ring. The device solves the problems of manual operation and air entrainment after the large-diameter round tank drug blocks of the solid rocket motor are bonded in pieces.

Description

technical field [0001] The invention belongs to the technical field of rocket motor charging, and relates to process equipment, in particular to a tensioning device and a construction method for solid rocket motor charging. Background technique [0002] In the past, there are two types of charge in the expansion structure of solid rocket motors, namely the screw expansion device and the taper sleeve expansion device. The screw expansion device is composed of a barrel section and a support plate assembly. Uniformly distributed threaded holes are designed on the barrel section. Manually operate the screw to respectively contact the support plate assembly with the drug column to bond the drug column to the shell; the taper sleeve expansion device mainly It is composed of taper sleeve, fixed plate, moving plate, screw, etc. The taper sleeve has uniform grooves, and the screw rod connects the fixed plate and moving plate, and the expansion and tightening is realized through the t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K9/24
CPCF02K9/24
Inventor 邱奇陈永钊刘美珍高运平司学龙陈文杰程山鄂鹏飞张浩吴玲玲柳青郑振兴张志强张斌
Owner HUBEI SANJIANG AEROSPACE JIANGHE CHEM TECH