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编织复合材料在高温热结构中的应用

季宝锋 孙艳杰 章凌 杨柳 提亚峰

宇航材料工艺2017,Vol.47Issue(4):14-18,36,6.
宇航材料工艺2017,Vol.47Issue(4):14-18,36,6.DOI:10.12044/j.issn.1007-2330.2017.04.003

编织复合材料在高温热结构中的应用

Application of Braiding Composites in Design of High-Temperature Thermal Structures

季宝锋 1孙艳杰 2章凌 1杨柳 1提亚峰1

作者信息

  • 1. 北京宇航系统工程研究所,北京100076
  • 2. 航天材料及工艺研究所,北京100076
  • 折叠

摘要

Abstract

The 3D braiding composites is widely used in the field of aviation,aerospace and other high technology because of excellent properties.The resistance of 3D braiding composites to high-temperature is an important application.In this paper,the heat conduction characteristics of a revolving thin wall under high-temperature are obtained through the heat conduction analysis of a 2.5D braiding CFRP engine structure.Then,through the test under the ground state of oxygen enrichment,it is proved that the structure can be used under high-temperature of 950℃ for long time.The consistency of finite element analysis and test results verifies the calculation correctness and the rationality of compensation parameters selection in test.The study has a good guiding significance to the application of 3D braiding composites in engineering.

关键词

编织复合材料/2.5D编织结构/热结构

Key words

Braiding composites/2.5D braiding structure/Thermal structure

分类

通用工业技术

引用本文复制引用

季宝锋,孙艳杰,章凌,杨柳,提亚峰..编织复合材料在高温热结构中的应用[J].宇航材料工艺,2017,47(4):14-18,36,6.

基金项目

国防基础科研项目(A0320131001) (A0320131001)

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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