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Size accuracy control method for large-sized low-density long fiber needle structure

A technology for structural size and precision control, which is applied in the direction of textiles, papermaking, non-woven fabrics, etc., can solve the problems of difficult dimensional precision control and easy deformation in the molding process, so as to improve rigidity, controllable dimensional precision, and solve the problems of easy deformation Effect

Active Publication Date: 2019-06-28
BEIJING SATELLITE MFG FACTORY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to overcome the deficiencies of the prior art, and to provide a method for controlling the dimensional accuracy of large-sized low-density long-fiber needle-punched structures, so that the thermosetting resin solution is deposited on the fiber surface to form a certain rigid coating, which is the entire large-sized The low-density long-fiber needle-punched structure provides rigid support, which solves the problems of easy deformation and difficult control of dimensional accuracy during the molding process

Method used

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  • Size accuracy control method for large-sized low-density long fiber needle structure
  • Size accuracy control method for large-sized low-density long fiber needle structure
  • Size accuracy control method for large-sized low-density long fiber needle structure

Examples

Experimental program
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Embodiment 1

[0064] In the preparation of a large curvature fan-shaped structure with a thickness of 25mm and an in-plane area greater than 2㎡ ( image 3 ), firstly, design and process Figure 4 tray structure. Then, the phenolic resin was dissolved in ethyl acetate in a container to form a phenolic solution with a phenolic mass content of 2% and a content of 8%. Then, evenly spray 3 times of phenolic solution with a content of 8% on the surface of the needle-punched fiber layer of the large-curvature fan-shaped structure needled with the initial 10 layers and the final 10 layers of carbon fiber, and spray evenly on the surface of the remaining intermediate fiber layers with a content of 2 times. % phenolic solution. The acupuncture structure molding is completed on the acupuncture mould. Then, under the protection of the acupuncture mould, the mold clamping of the acupuncture structure and the tray structure is completed, and the inner surface is evenly pressurized by the acupuncture m...

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Abstract

The invention relates to a size accuracy control method for a large-sized low-density long fiber needle structure. The method comprises the steps that a heat convertible resin solution with a certaingel content is prepared; the heat convertible resin solution is uniformly sprayed onto the surface of a structural fiber layer by using a spraying device or tool, the heat convertible resin solution is deposited on surface layer fiber to form a rigid layer, the rigidity of the fiber surface is improved, a rigid support is provided for the whole large-sized low-density long fiber needle structure,and the problems are solved that deformation is easily caused in the forming process, and the size accuracy control difficulty is high. In the subsequent process, it is not required that extra flexible protection is provided for the low-density long fiber needle structure, and the operation is convenient.

Description

technical field [0001] The invention relates to a dimensional accuracy control method for large-sized low-density long-fiber needle-punched structures, belongs to the technical field of thermal protection structure product molding, and is applied to the development of a thermal protection system for an aircraft at a second cosmic speed. Background technique [0002] During the return flight process, the manned spacecraft needs to experience high heat flow, and the outer surface of the returning aircraft must be protected by a thermal protection system. With the continuous development of deep space exploration technology, traditional heat protection materials cannot meet the needs of the heat flow environment of the second space flight speed. One development direction of the thermal protection system is to use low-density long-fiber needle-punched structure and integrally formed thermal protection materials. The reinforcement of the low-density long-fiber, integrally formed ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): D06N3/00D04H3/105
Inventor 赖小明张璇张明张玉生郑建虎张鹏飞关鑫孙天峰刘佳宫顼黎昱杨海涛尉世厚张鑫
Owner BEIJING SATELLITE MFG FACTORY
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