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Preparation method for mold of carbon fiber composite integrated shell structure

A composite material and shell structure technology, applied in the aerospace field, can solve problems affecting the performance of stratospheric airships, large connection discreteness, and welding difficulties, and achieve the effects of reducing mold costs, simple process, and high production efficiency

Inactive Publication Date: 2016-09-14
EAGLES MEN AERONAUTIC SCI & TECH GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The carrying load of stratospheric satellites directly affects the degree of advancement of stratospheric satellites. Therefore, the weight reduction project of the hoisting truss and the connected shell structure of the aerostat is imminent. At present, the truss structures are all made of carbon fiber reinforced resin-based composite materials, and The connection between the metal shell structure and the stratospheric satellite truss structure is discrete, welding is difficult, the weight is heavy, and the electrical corrosion between the carbon fiber truss and the shell affects the performance of the stratospheric airship.

Method used

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  • Preparation method for mold of carbon fiber composite integrated shell structure
  • Preparation method for mold of carbon fiber composite integrated shell structure
  • Preparation method for mold of carbon fiber composite integrated shell structure

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Embodiment Construction

[0038] The following will be combined with Figure 1-7 And embodiment the present invention is described in further detail.

[0039] A method for preparing a carbon fiber composite material integrated shell structure mold according to the present invention comprises the following steps;

[0040] Step 1: According to the structural design requirements of the carbon fiber composite integrated shell, a mold is made, which includes a male mold and a female mold;

[0041] like figure 2 The shown carbon fiber composite material integrated shell structure, the length, width, and height are 500*200*300mm respectively, and the shell thickness is 2.5mm, including a bottom surface 8, two side surfaces 9 and two front and rear surfaces 10, the bottom surface 8 and the The included angle between the side surfaces 9 is 90°, the included angle between the bottom surface 8 and the front and rear surfaces 10 is 90°, and the included angle between the side surfaces 9 and the front and rear s...

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Abstract

A preparation method for a mold of a carbon fiber composite integrated shell structure includes the following steps that firstly, the mold is manufactured according to dimension requirements of the carbon fiber composite integrate shell structure, wherein the mold comprises a male mold body and a female mold body; secondly, the male mold body is assembled; thirdly, carbon fiber preimpregnated cloth is cut according to the layering manner of the carbon fiber composite integrated shell structure; fourthly, the surface of the female mold body and the surface of the male mold body are cleaned with alcohol, and a mold release agent is sprayed; fifthly, the carbon fiber preimpregnated cloth is laid on the surface of the male mold body; sixthly, the female mold body is assembled, and the female mold body is attached to the inner portion of the completely-laid shell structure; seventhly, a spliced female mold cavity is filled with iron sand; eighthly, the mold for a carbon fiber composite integrated shell is packaged through a vacuum bag, and vacuum pumping is conducted; ninthly, the whole mold subjected to vacuum pumping is sent into an autoclave through a transport vehicle to be solidified; and tenthly, the solidified mold is taken out of the autoclave, and the carbon fiber composite integrated shell structure is obtained.

Description

【Technical field】 [0001] The invention provides a carbon fiber composite material integrated shell structure mold making and preparation method, belonging to the field of aerospace technology. 【Background technique】 [0002] In recent years, various countries are conducting research on stratospheric airship technology. Stratospheric airship is a new type of low-cost, low-energy stratospheric aircraft, which can serve as an important existence in the stratosphere to provide communication support, and plays a very important role in both military and civilian applications. In view of the application advantages of stratospheric airships such as long time in space, large load capacity, high cost-effectiveness, good stealth performance, and strong survivability, major aerospace countries have successively formulated stratospheric airship project plans, and actively carried out feasibility studies and key technologies. Research and flight test. With the continuous progress of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B29C70/44B29C70/46B29C70/54
CPCB29C70/443B29C70/46B29C70/54
Inventor 王立峰彭钜锴张丽娇
Owner EAGLES MEN AERONAUTIC SCI & TECH GRP
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