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高温界面接触热阻试验

张婕 丛琳华 吴敬涛

沈阳航空航天大学学报2024,Vol.41Issue(2):14-20,7.
沈阳航空航天大学学报2024,Vol.41Issue(2):14-20,7.DOI:10.3969/j.issn.2095-1248.2024.02.002

高温界面接触热阻试验

Interface contact resistance test under high temperature environment

张婕 1丛琳华 1吴敬涛1

作者信息

  • 1. 中国飞机强度研究所 强度与结构完整性全国重点实验室,西安 710065
  • 折叠

摘要

Abstract

Thermal contact resistance between aircraft components is unavoidably.It is very important to acquire thermal contact resistance accurately for detailed design of thermal structure.To overcome the measurement difficulty under high temperature and high pressure,a measuring device was indepen-dently developed based on static heat flow method.The device can effectively obtain the thermal con-tact resistance between solid structures under given interface pressure and hot surface temperature up to 1 500℃.By using this device,three kinds of thermal contact resistance tests were carried out successfully.The influence law of pressure,temperature and interface roughness on the thermal contact resistance were figured out.Experimental results show that the measurement device is stable and reliable with uncompli-cated operation,while the simulation accuracy for temperature and pressure load is satisfied.This device can provide supports for the development and engineering application of aircraft thermal structures.

关键词

接触热阻/静态热流计法/界面压力/热阻测量装置/热防护系统/高温界面

Key words

thermal contact resistance/static heat flow method/interface pressure/thermal resistance measuring device/thermal protection system/high temperature interface

分类

能源科技

引用本文复制引用

张婕,丛琳华,吴敬涛..高温界面接触热阻试验[J].沈阳航空航天大学学报,2024,41(2):14-20,7.

基金项目

国家自然科学基金(项目编号:U214120164) (项目编号:U214120164)

沈阳航空航天大学学报

2095-1248

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