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Strategic Study of CAE >> 2007, Volume 9, Issue 2

Discussion on Integrated Environment Control Thermal Management System Concepts for Hypersonic Vehicle

1. School of Aeronautics Science and Technology, Beihang University, Beijing 100083, China;

2. Chengdu Research Institute of Aircraft, Chengdu 610064, China

Funding project:国家自然科学基金资助项目(60402032);国防预研基金资助项目(41303040203);国家杰出青年基金资助项目(60025102) Received: 2005-12-01 Revised: 2006-01-23

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Abstract

Hypersonic vehicle is nowadays a focus in the field of aeronautics and astronautics. It will encounter with severe aero-heating during hypersonic flight. As a result, a reliable integrated thermal management system is a necessity to ensure flight safety. Concept of integrated thermal management system was put forward respectively,based on the characteristics of hypersonic vehicles with different missions.For vehicle which is characterized by short flight time and quick change of velocity and altitude,a concept of thermal management system which uses liquid唱hydrogen as major heat sink and PCM material as supplementary heat sink was presented. For that with longer flight time and higher Mach number,a concept of thermal management system using endothermic fuels as heat sink was advanced.Key technologies concerning these concepts were discussed, and research focuses in the future were indicated.

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References

[ 1 ] 黄志澄 .高超音速飞行器及其发展趋势分析 [J] . 国际航空 ,1998 ,(3) :17 ~ 20 link1

[ 2 ] 解发瑜 ,李 刚 ,徐忠昌 .高超声速飞行器概念及 发展动态 [J] .飞航导弹 ,2004 ,(5) :27 ~ 31 link1

[ 3 ] 王晓峨 .国外天地往返运输系统的防热系统 [R] . 航天情报研究报告 ,HQ - B89018

[ 4 ] Sridhar K , Michael M . Thermal management and environmental control of hypersonic vehicle [R] . SAE 891440

[ 5 ] Christensen L L , Rrichards J A . Environmental control system considerations for supersonic cruising aircraft [R] . SAE 650226

[ 6 ] Letlow J T , Jenkins L C . Development of an integrated environmental control system [R] .SAE 981544

[ 7 ] Bear J . Heat options for a more electric aircraft thermal management system [R] .SAE 971244

[ 8 ] Ghanekar M . Vapor cycle system for the F - 22 raptor [R] .SAE 2000 - 01 - 2268

[ 9 ] Vrable D L ,Yerkes K L .A thermal management concept for more electric aircraft power system application [R] . SAE 981289

[10] 寿荣中 ,何慧姗 .飞行器环境控制 [M] .北京 :北 京航空航天大学出版社 ,2004

[11] 崔海亭 ,杨 锋 .蓄热技术及其应用 [M] .北京 :化 学工业出版社 ,2004

[12] 张寅平 ,胡汉平 ,孔祥冬 ,等 .相变储能 ——— 理论 和应用 [M] . 合肥 : 中国科学技术大学出版社 , 1996

[13] 张 华 ,李 芳 .高温相变共晶盐潜热蓄冷介质的 配制与测试 [J] .暖通空调 ,1999 ,29(6) :62 ~ 64 link1

[14] Huang H , Sobel K R , Spadaccini J . Endothermic heat sink of hydrocarbon fuels for scramjet cooling [R] .AIAA 2002 - 3871

[15] Spadaccini L J , Marteney P J , Colket M B Ⅲ , et al . Method of cooling with an endothermic fuel [ P] . US 5176814 ,1993

[16] Petley D H , Jones S . Thermal management for Mach 5 cruise aircraft using endothermic fuel [R] . AIAA 90 - 3284

[17] Korabelnikov A ,Kuranov A .Thermo-chemical conversion of hydrocarbon fuel under the concept “AJAX” [R] . AIAA 99 - 4921

[18] Korabelnicov A V , Kuranov A L . Thermo_chemical conversion of hydrocarbon fuel for the AJAX concept[R] . AIAA 99 - 3537

[19] 贺 芳 ,禹天福 ,李亚裕 .吸热型碳氢燃料的研究 进展 [J] .导弹与航天运载技术 ,2005 ,(1) :26 ~ 29 link1

[20] 何 龙 ,潘富敏 ,林瑞森 .吸热型碳氢燃料催化裂 解的研究述评 [J] . 推进技术 , 2001 , 25(2) : 97 ~ 100 link1

[21] 李祖光 ,高 涵 ,厉 刚 ,等 .吸热型碳氢燃料的 量热研究 [J] .推进技术 ,1999 ,20(4) :92 ~ 95 link1

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