航空学报 > 2016, Vol. 37 Issue (S1): 53-58   doi: 10.7527/S1000-6893.2016.0176

高温合金前缘热防护结构隔热性能分析

王曼, 杨家勇, 何二锋, 涂冰   

  1. 中航工业成都飞机设计研究所, 成都 610091
  • 收稿日期:2016-05-13 修回日期:2016-06-02 出版日期:2017-01-10 发布日期:2016-07-22
  • 通讯作者: 王曼,Tel.:028-65020733,E-mail:realidog@gmail.com E-mail:realidog@gmail.com
  • 作者简介:王曼,女,硕士,工程师。主要研究方向:热防护结构设计。Tel.:028-65020733,E-mail:realidog@gmail.com;杨家勇,男,硕士,高级工程师。主要研究方向:机翼结构设计,热防护结构设计。E-mail:yangjy611@sina.com;何二锋,男,本科,工程师。主要研究方向:热防护结构设计。E-mail:549430908@qq.com;涂冰,男,硕士,工程师。主要研究方向:热防护结构设计。E-mail:43242275@qq.com

Analysis and design of leading edge using metallic thermal protection system

WANG Man, YANG Jiayong, HE Erfeng, TU Bing   

  1. AVIC Chengdu Aircraft Design and Research Institute, Chengdu 610091, China
  • Received:2016-05-13 Revised:2016-06-02 Online:2017-01-10 Published:2016-07-22

摘要:

高温合金前缘热防护结构由高温合金蜂窝和隔热毡、连接件构成,同时具有承载和隔热作用,易于拆卸和维修,具有经济性和安全性。通过分析高温合金前缘热防护结构隔热性能和承载能力,对前缘结构进行设计。高温合金蜂窝隔热效果良好,并可以承受1 200℃高温。隔热毡所用的隔热材料在高温试验下保持良好的隔热效果,验证了本文传热分析方法的正确性。建立了传热迭代分析算例,确认结构各项参数满足某型高速临近空间飞行器的热环境和承载使用要求,完成了前缘结构隔热一体化初步设计。

关键词: 高温合金, 前缘, 热防护, 隔热, 结构隔热一体化设计

Abstract:

Leading edge using metallic thermal protection system consists of super alloy honeycomb and thermal insulation felt, duct fastening, which has the function of loading and thermal insulation capacity. The leading edge is easy to be disassembled and maintained, with economic efficiency and safety. The leading edge's loading and thermal insulation capacity are analyzed, then the final structure design is obtained. Super alloy honeycomb has good thermal insulation effect, and has high temperature resistance at 1 200℃. The material of thermal insulation felt maintains excellent thermal insulation effect in high temperature test, so the correctness of heat transfer analysis method is verified. By modeling local heat transfer analysis structure, the leading edge design parameters can be iteratively fixed to achieve the leading edge structure-thermal integrative design.

Key words: super alloy, leading edge, thermal protection, thermal insulation, structure-thermal integrative design

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