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Winding curing device for thin-walled skirts made of carbon fiber composites

A composite material and curing device technology, which is applied in the molding field of solid rocket motor housing accessory skirts, can solve the problems of increased maintenance costs and low dimensional accuracy of thin-walled skirts made of carbon fiber composite materials, and achieves improved dimensional accuracy Effect

Active Publication Date: 2017-08-22
湖北三江航天江北机械工程有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the above method, the wound material is not extruded, resulting in low dimensional accuracy of the thin-walled carbon fiber composite skirt.
[0005] In addition, the existing mandrel and the mandrel are of an integrated structure, and the mandrel is generally a wearing part. When the mandrel is damaged, the mandrel and the mandrel need to be replaced together, which increases the maintenance cost

Method used

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  • Winding curing device for thin-walled skirts made of carbon fiber composites
  • Winding curing device for thin-walled skirts made of carbon fiber composites
  • Winding curing device for thin-walled skirts made of carbon fiber composites

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Embodiment Construction

[0025] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0026] Such as Figure 1-8 The winding and curing device for thin-walled skirts made of carbon fiber composite materials includes a mandrel 1, a mandrel assembly 2 installed on the mandrel 1, an inner wedge-shaped cylinder 3, an outer wedge-shaped cylinder 4, an upper platen 5, Base 6, screw rod 7, upper adjusting plate 8 and lower adjusting plate 9, wherein, the first shaft hole 5.1 is provided on the upper pressing plate 5, and the bottom of the upper pressing plate 5 is provided with a radial limit on the top surface of the upper adjusting plate 8. The base 6 is provided with a second shaft hole 6.1 coaxial with the first shaft hole 5.1, and the base 6 is provided with a radial direction to the bottom surface of the lower adjustment plate 9 on the edge of the second shaft hole 6.1. Limiting positioning counterbore 6.2, the top surface of the...

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Abstract

The invention relates to a winding and curing device for thin-walled skirts made of carbon fiber composite materials, which includes a mandrel, a core mold installed on the mandrel, an inner wedge-shaped cylinder, an outer wedge-shaped cylinder, an upper pressure plate, a base, a screw, The upper regulating plate and the lower regulating plate, after using the winding curing device of the carbon fiber composite material thin-walled skirt type part of the present invention, can squeeze and solidify the fibers wound in the mandrel as a whole, and then heat and demould, in this way An extrusion curing process is added between winding and heating, which can further improve the dimensional accuracy, shape tolerance and surface finish of the carbon fiber composite thin-walled skirt.

Description

technical field [0001] The invention relates to the molding of the skirt body of the accessory part of the solid rocket motor casing, in particular to a winding and curing device for the thin-walled skirt part of carbon fiber composite material. Background technique [0002] The solid rocket motor is the power device of the aerospace vehicle, which is composed of a charge combustion chamber, a nozzle and an ignition device. As an important power device for space delivery and missile propulsion systems, with the rapid development of aerospace technology, the development trend of solid rocket motors is high speed, high precision, small mass, high specific impulse, and high thrust-to-mass ratio. The structural quality of the solid rocket motor shell is the most important part of the negative mass of the engine, which has a great impact on the performance of the engine. Therefore, high-strength and light-weight shell materials should be selected. Carbon fiber composite material...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C35/04B29C70/54
Inventor 刘亮初敬生吴萍王明坤
Owner 湖北三江航天江北机械工程有限公司
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