Forming method of wall-thickness-variable composite skirt

A composite material and molding method technology, applied in the field of composite material molding, can solve the problems of poor molding quality, high demolding cost, high manufacturing cost, etc., and achieve the effects of shortening production cycle, reducing porosity, and improving molding quality

Inactive Publication Date: 2017-06-27
成都联科航空技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to overcome the disadvantages of poor molding quality, easy to cause surface defects, high demoulding cost, and high manufacturing cost of the existing

Method used

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  • Forming method of wall-thickness-variable composite skirt
  • Forming method of wall-thickness-variable composite skirt
  • Forming method of wall-thickness-variable composite skirt

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0059] A method for forming a skirt made of variable wall thickness composite material, comprising the following steps:

[0060] Step 1, respectively prepare section 1 21 and section 2 22 of the blank of component 2 2, and divide section 1 21 into two sections;

[0061] Step 2. First attach the non-porous isolation film 6 on the surface of the member three 8, attach the section one 21 to the outer surface of the member three 8, and at the junction of the two sections of the section one 21, A carbon fiber fabric prepreg 11 is laid on the side in contact with the member three 8, and a release cloth 9 is arranged between the two sections of the section one 21;

[0062] Step 3, attaching the remaining part of the outer surface of the member 3 8 to the section 2 22, and the two ends of the section 22 overlap with the two ends of the section 1 21 respectively;

[0063] Step 4, set a non-porous isolation film 6, an air felt 7 and a vacuum bag 4 on the outside of the blank of the com...

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PUM

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Abstract

The invention discloses a molding method of a composite material skirt with variable wall thickness. The method comprises the following steps: attaching a component to be formed on the outer side of component one, and connecting component two end to end in a ring shape and attaching to the outer side of the component to be formed , set a vacuum bag on the outer side of the whole formed by the component to be formed and the second component and carry out vacuum treatment, put it into an autoclave for curing and molding, and after the forming of the component to be formed is completed, open the second component along the junction. , and then separate the component to be formed from the component 1 to complete the process of demolding, wherein the component 1 is an annular hard component, and the component 2 is a strip-shaped soft component. Compared with the prior art, the combination of the soft mold and the hard mold is beneficial to improve the quality of the surface forming. By disassembling the soft mold, rapid demoulding is realized without destroying the mold, and the mold can be reused, effectively saving the cost of the mold and reducing the manufacturing cost. .

Description

technical field [0001] The invention relates to the technical field of composite material molding, in particular to a molding method of a variable-wall-thickness composite skirt. Background technique [0002] The connection skirt of solid rocket motor is an important part of the engine casing, which is used to realize the connection between the casing stages or the connection of the engine and the main structure of the missile. Due to the high specific strength and specific modulus of composite materials, Therefore, composite connecting skirts are widely used in the connection of rocket or missile main structures. [0003] Composite material skirts often have variable wall thickness, such as flanges at the bottom of the formed part, or sinking bevels, etc. The forming methods of the overall connecting skirt of composite materials include RTM forming process and winding layer forming process. The RTM molding process is to preform the flange and tube body of the composite mat...

Claims

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Application Information

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IPC IPC(8): B29C70/34B29C70/54B29C70/68
CPCB29C70/342B29C70/54B29C70/68B29C70/681
Inventor 杨自燕陈剑李书军孙松强雍坤李波成雪峰赵鹏飞王亚鹏
Owner 成都联科航空技术有限公司
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