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T800HB碳纤维复合材料壳体定量化等强度补强技术

张世杰 王汝敏 廖英强 周伟江 程勇

宇航材料工艺2018,Vol.48Issue(3):51-55,5.
宇航材料工艺2018,Vol.48Issue(3):51-55,5.DOI:10.12044/j.issn.1007-2330.2018.03.011

T800HB碳纤维复合材料壳体定量化等强度补强技术

Quantitative Isostrength Reinforcement of Composite Case Made of T800HB Carbon Fiber

张世杰 1王汝敏 1廖英强 2周伟江 3程勇2

作者信息

  • 1. 西北工业大学理学院应用化学系,西安710072
  • 2. 西安航天复合材料研究所,西安710025
  • 3. 高性能碳纤维制造及应用国家地方联合工程研究中心,西安710089
  • 折叠

摘要

Abstract

Composite case made of brittle T80OHB carbon fiber is sensitive to stress concentration,and easily cause case dome failure at low pressure.In order to overcome redundant mass of longitudinal layer of cylinder section induced by traditional carbon cloth and UD cloth reinforcement,isostrength reinforcement method is used.Φ150 mm pressure case is treated as study object,stress equilibrium factor in processing design of composite case is referred,and composite thickness in quantitative isostrength reinforcement is concluded by comparison about strain result and experiment result.As a result,quantitative isostrength reinforcement is practicable and reliable.Burst pressure of T800HB carbon fiber case using isostrength reinforcement method totally achieves design value,and longitudinal layer strength in cylinder is not redundant.The method can increase PV/W of case,especially high length-to-diameter ratio case.

关键词

T800HB碳纤维/壳体/定量化等强度补强/纤维强度转化率

Key words

T800HB carbon fiber/Case/Quantitative isostrength reinforcement/Percentage translation of fiber strength

分类

通用工业技术

引用本文复制引用

张世杰,王汝敏,廖英强,周伟江,程勇..T800HB碳纤维复合材料壳体定量化等强度补强技术[J].宇航材料工艺,2018,48(3):51-55,5.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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