Benzoxazine resin-based reinforcing fiber composite material and forming method thereof

A benzoxazine resin, benzoxazine technology, applied in high-strength glass fiber reinforced plastic products, high temperature resistance field, can solve the problems of incomplete release of small molecules, stress concentration, bulging and cracks, etc., to achieve mechanical properties and ablation resistance. Excellent performance, dense internal shape, and the effect of improving flexibility

Inactive Publication Date: 2019-03-19
西安长峰机电研究所
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] In order to overcome the deficiencies of the prior art, the present invention provides a benzoxazine resin-based reinforced fiber composite material, which can improve the internal and external quality of the nozzle liner, avoid incomplete release of small molecules of the product, and cause stress concentration on the surface, resulting in bulges and cracks. crack situation

Method used

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  • Benzoxazine resin-based reinforcing fiber composite material and forming method thereof
  • Benzoxazine resin-based reinforcing fiber composite material and forming method thereof
  • Benzoxazine resin-based reinforcing fiber composite material and forming method thereof

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Embodiment Construction

[0016] The present invention will be further described below in conjunction with the examples, and the present invention includes but not limited to the following examples.

[0017] Under the premise of ensuring the tensile performance of the solid rocket motor heat-resistant lining ≥ 39Mpa, the bending strength ≥ 59MPa, and the oxyacetylene line ablation rate < 0.18mm / s, the aminophenol-formaldehyde resin used in the molding production of the nozzle lining is cured During the process, polycondensation reaction will occur, and small molecules will be released. After the product is cooled and demoulded, the release of small molecules will often be incomplete, stress concentration will occur on the surface of the product, and bulges and cracks will appear. The invention provides a benzoxazine resin base-reinforced fiber composites. .

[0018] The commonly used aminophenol-formaldehyde resin used in the molding of the nozzle lining of solid rocket motors is diluted with ethanol ...

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Abstract

The invention provides a benzoxazine resin-based reinforcing fiber composite material and a forming method thereof. The method includes steps: dissolving, by weight, 50-70 parts of benzoxazine resin and 30-50 parts of ammonia phenolic resin into a ketone solvent in equal weight; well mixing with, by weight, 0.5-2.5 parts of gamma-aminopropyl triethoxysilane and 170 parts of high-silica chopped fibers; airing in the sun, drying and performing compression molding. A prepared lining is smooth and glossy in surface and free of bumps and cracks, the tested average tensile strength is 145MPa, the bending strength is 150MPa, the linear ablative rate is 0.13mm/s, and the lining is dense and flawless internally. The benzoxazine resin-based reinforcing fiber composite material can be applied to preparation of solid rocket engine jet pipe linings and other heatproof structures and has advantages of great product manufacturability, no pores, no cracks, ablation resistance and flame retardation.

Description

technical field [0001] The invention relates to a composite material, which is used for the heat-proof lining of solid rocket motor nozzles, partitions and other components, and is also suitable for high-temperature resistant and high-strength glass fiber reinforced plastic products. Background technique [0002] Solid rocket motor heat-resistant linings generally require tensile properties ≥ 39MPa, bending strength ≥ 59MPa, and oxyacetylene line ablation rate < 0.18mm / s. At present, the common solid rocket motor nozzle lining is molded with high silica fiber / aminophenolic aldehyde. This molding method has mature technology, excellent mechanical properties and ablation performance of the material, and can meet the mechanical properties and ablation resistance of the solid rocket motor heat-resistant inner lining. However, the nozzle liner made of fiber / phenol formaldehyde heat press has technical problems such as large curing shrinkage rate, small molecule release when t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C08L61/34C08L63/00C08K5/544C08J5/06
CPCC08J5/06C08J2361/34C08J2461/34C08J2463/00C08K5/544
Inventor 邹敏秦锋张新航李晓奋沈红欣
Owner 西安长峰机电研究所
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