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Anti-radiation high temperature resistant heat insulating composite bushing and preparation method

A composite sleeve and high temperature resistant technology, which is applied in the direction of heat insulation protection pipelines, heat exchange equipment, chemical instruments and methods, etc., can solve the problems that affect the effect of flame retardant and heat insulation cables, and the surface of the coating does not have reflected heat flow, etc. Achieve the effect of improving heat insulation and flame retardant effect, ensuring that it will not be burned out, and good anti-radiation performance

Active Publication Date: 2014-04-02
衡阳凌云特种材料有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the advantage of the high-temperature-resistant heat-insulating coating itself is to deal with flame ablation, when encountering strong heat flow radiation (the heat flow temperature is characterized by rising from low to low), the high-temperature-resistant heat-insulating coating of the casing can only be passively It absorbs a large amount of heat, because the surface of the coating does not have the function of reflecting heat flow. When the temperature of the heat flow becomes higher and higher, the organic substances contained in the coating will be ignited and ignited while the coating is carbonized, which affects the flame retardancy. Heat insulation effect and hidden danger of cables being burnt out

Method used

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  • Anti-radiation high temperature resistant heat insulating composite bushing and preparation method
  • Anti-radiation high temperature resistant heat insulating composite bushing and preparation method
  • Anti-radiation high temperature resistant heat insulating composite bushing and preparation method

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Embodiment Construction

[0022] A radiation-proof, high-temperature-resistant and heat-insulating composite casing, which includes an inner lining casing 1, a high-temperature-resistant and heat-insulating coating 2 coated on the inner lining casing 1, and a thin-shaped heat-resistant coating 2 wound on the high-temperature-resistant and heat-insulating coating 2 Aluminum wrapping tape3.

[0023] The inner lining sleeve 1 is an alkali-free glass fiber sleeve.

[0024] The high-temperature-resistant heat-insulating coating 2 has a thickness of 2 mm and is made of the following components in parts by weight, wherein: 30 parts of refined adipic acid; 18 parts of trimethylolpropane Obtain clone: ​​25 parts; antimony trioxide: 4 parts; ammonium borate: 6 parts; starch: 10 parts; zinc oxide: 6 parts; ammonium polyphosphate: 13 parts; cyclohexanone or xylene 150 parts.

[0025] The thin aluminum film winding belt 3 is wound on the high temperature resistant heat insulation coating 2 in the manner of a 1 / 2 b...

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Abstract

The invention provides an anti-radiation high temperature resistant heat insulating composite bushing and a preparation method. The anti-radiation high temperature resistant heat insulating composite bushing comprises a lining bushing, a high temperature resistant heat insulating coating layer coated on the lining bushing, and a thin type aluminum film winding band winded on the high temperature resistant heat insulating coating layer. The thickness of the high temperature resistant heat insulating coating layer is 1-2mm, the high temperature resistant heat insulating coating layer is made from raw materials in component parts as follows, the parts are weight parts, wherein: adipic acid: 25-35 parts; trimethylolpropane: 16-20 parts; dechlorane plus: 20-30 parts; diantimony trioxide: 3-10 parts; ammonium borate: 5-12 parts; starch: 8-15 parts; zinc oxide: 5-12 parts; ammonium polyphosphate: 10-20 parts; and cyclohexanone or xylene 100-200 parts. The thin type aluminum film winding band is formed via cutting after synthesis of alkali-free glass fiber cloth and an aluminum plated film via a high temperature resistant flame retardant adhesive, and is winded on the high temperature resistant heat insulating coating layer in a mode of 1 / 2 hasp.

Description

technical field [0001] The invention relates to a radiation-proof, high-temperature-resistant and heat-insulating composite casing and a preparation method thereof, in particular to a radiation-proof, high-temperature-resistant and heat-insulating composite sleeve used to protect cables at engine parts of aerospace, rockets and missiles from being damaged by high heat flux radiation and burning. Casing and preparation method. Background technique [0002] At present, in the existing technology, the high-temperature heat-resistant heat-insulating sleeves used in the cables of rocket and missile engines mostly use alkali-free glass fiber sleeves as the inner liner sleeves, and then coat the surface of the inner liner sleeves with high-temperature heat-resistant heat insulation. Coating, after baking, weave a layer of aramid wire braided sleeve on the high temperature resistant heat insulation coating. Although this kind of high-temperature-resistant and heat-insulating casing...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16L59/02C09D167/00C09D103/02C09D5/33C08G63/12B32B1/08B32B15/20B32B15/04
Inventor 周霞唐亚林
Owner 衡阳凌云特种材料有限公司
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