高速飞行器红外罩热力失效机制

鄂羽佳; 王天宇; 高鸽; 耿方娟; 艾俊强; 韩杰才; 朱嘉琦

doi:10.6052/1000-0992-16-047

高速飞行器红外罩热力失效机制

doi: 10.6052/1000-0992-16-047

鄂羽佳¹,
王天宇¹,
高鸽¹,
耿方娟¹,
艾俊强²,
韩杰才^1,ɛ, ,,
朱嘉琦^1,3,’, ,

1 哈尔滨工业大学复合材料与结构研究所, 哈尔滨 150001
2 中航工业第一飞机设计研究院, 西安 710089
3 哈尔滨工业大学微系统与微结构制造教育部重点实验室, 哈尔滨 150080

基金项目: 国家杰出青年基金项目(51625201), 国家自然科学基金面上项目(51372053)和国家自然科学基金创新群体科学基金项目(11421091)资助.

详细信息

作者简介:
null

作者简介：
朱嘉琦, 哈尔滨工业大学航天学院教授、博导, 长江学者特聘教授, 国家杰出青年基金获得者, 万人计划领军人才.主要从事极端环境红外罩失效机制及其抗失效方法研究, 担任中国硅酸盐学会薄膜与涂层分会副理事长、中国仪表材料学会常务理事、中国机械工程学会表面工程分会常务委员, 获得中国青年科技奖、省青年五四奖章等荣誉, 获国家技术发明奖二等奖1项, 黑龙江省技术发明一等奖和二等奖各1项.发表SCI论文131篇, 授权发明专利50余项.
韩杰才, 中国科学院院士, 哈尔滨工业大学航天学院教授、博导, 国家自然科学基金委创新研究群体负责人, 特种环境复合材料技术国防科技重点实验室主任, 国家某重大科技工程专家, 国家863计划某主题专家组副组长.主要从事飞行器结构与热防护系统、梯度复合材料、超高温热防护材料、光电晶体与薄膜以及材料燃烧合成技术等研究, 曾获国家自然科学奖二等奖、国家技术发明奖二等奖等.获国家发明专利授权61项, 出版学术专著2本, 在国际期刊发表文章350余篇.

通讯作者:
韩杰才

朱嘉琦

中图分类号: V241;
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出版历程
- 收稿日期: 2016-12-20
- 刊出日期: 2018-02-08

Aerothermal dynamic failure of infrared window in high-speed aircraft

E Yujia¹,
WANG Tianyu¹,
GAO Ge¹,
GENG Fangjuan¹,
AI Junqiang²,
HAN Jiecai^{1,ɛ
, ,},
ZHU Jiaqi^{1,3,’
, ,}

Harbin Institute of Technology, Center for Composite Materials, Harbin 150001, China
AVIC the First Aircraft Institute, Xi'an 710089, China
Harbin Institute of Technology, Key Laboratory of Micro-systems and Micro-strucrures Manufacturing, Harbin 150080, China

More Information

Author Bio:
^’ E-mail:zhujq@hit.edu.cn
^ɛ E-mail:hanjc@hit.edu.cn

Corresponding author: HAN Jiecai; ZHU Jiaqi

摘要

摘要: 红外罩材料包括红外罩增透保护膜和基底材料, 是高速导弹结构--功能一体化的关键部件, 应用极为广泛. 但是, 红外罩材料通常工作于恶劣的外界环境下, 处于复杂的热力混合作用状态, 可能导致窗口失效, 因此对红外罩材料热力响应和失效的研究具有重要的科学研究价值和工程实际意义.本文针对高速飞行器环境下红外罩材料的气动热力失效机制, 从典型材料的特性及制备、气动热力响应机理及分析、红外罩材料的结构性和功能性失效等方面总结相关学者的研究成果, 并对今后的发展趋势进行展望.
- 红外罩 /
- 气动热力 /
- 失效机制
Abstract: As one of the key components of a high-speed aircraft, the infrared window which is composed by matrix materials and functional films is widely applied. In the harsh environment, however, the infrared window works under complex aerothermal conditions, which may lead to its structural failure or dysfunction. Thus, the investigation on the aerothermal dynamic failure of infrared window in high-speed aircraft is of scientific importance and practical significance. This article reviews the studies on the aerodynamic thermal failure mechanisms of infrared windows in high-speed conditions, concerning typical materials, the aero-thermo-dynamics and structural failure or dysfunction. Finally, the prospects of further investigations on infrared windows are discussed.
- infrared window /
- aerothermal dynamic /
- failure mechanism

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参考文献(189)

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