High-altitude heat transfer performance analysis for skin heat exchanger based on ground experiment
-
摘要: 面向未来我国大功率机载电子设备冷却需求,需要发展新型机载冷却方式,减少对传统环控制冷系统的依赖,为此研究了一种气/气蒙皮换热器用于电子设备热管理.该蒙皮换热器是一种无能耗被动换热方式,在不增加飞机代偿损失的情况下实现大功率电子设备热管理.为了考核所设计的蒙皮换热器机载飞机环境换热性能,设计加工了实验样件,在地面开展了换热性能实验研究工作,获得热边流动传热准则和对流换热系数.在此基础上推演出高空巡航状态下的蒙皮换热器换热性能,获得传热最不利安装位置和改进位置时的传热性能.研究工作预期为未来我国基于蒙皮换热器的飞机综合热管理提供设计及机载应用技术支持.Abstract: Facing to future high-power onboard electronic equipment cooling requirements for our country, it needs to develop a new onboard cooling technology to reduce the dependence on traditional environmental control system. A new gas-gas skin heat exchanger was studied for aircraft thermal management of electronic equipment. The skin heat exchanger is a non-energy consumption of passive heat exchanger with decreasing aircraft performance penalty when it realizes the thermal management for high-power electronic devices. To assess the heat transfer performance of skin heat exchanger onboard, an experimental prototype was designed and its heat transfer performance was carried out on the ground experimental device to obtain the convective heat transfer coefficients of its hot and cold sides. Based on this experiment, the heat transfer performance of skin heat exchanger in high-altitude cruise condition was deduced for the most unfavorable and improved installation position. This study is expected to provide technical support for its future onboard applications.
-
[1] Sprouse J.F22 environmental control / thermal management fluid transport optimization .SAE 2200020122266,2000 [2] O-Connell T C,Lui C,Walia P,et al.A hybrid economy bleed,electric drive adaptive power and thermal management system for more electric aircraft[J].SAE Int J Aerosp,2010,3(1):168-172 [3] 高峰,袁修干.高性能战斗机燃油热管理系统[J].北京航空航天大学学报,2009,35(11):1353-1357 Gao Feng,Yuan Xiugan.Fuel thermal management system of high performance fighter aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(11):1353-1357(in Chinese) [4] Airbus Industrie.A319/A320/A321 technical training manual .Toulouse:Airbus Industrie,1996 .http://www.avdyne.com/airbus_training/21zAircond.pdf [5] Hashemi A,Dyson E.Performance characterization of high-power electronic equipment onboard an aircraft[J].Heat transfer engineering,2000,21(1):15-24 [6] 杨世铭,陶文铨.传热学[M].2版.北京:高等教育出版社,1998:143-146 Yang Shiming,Tao Wenquan.Heat transfer [M].2nd ed.Beijng:Higher Education Press,1998:143-146(in Chinese) [7] 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,2004:228-229 Shou Rongzhong,He Huishan.Aircraft environment control [M].Beijing:Beihang University Press,2004:228-229(in Chinese) [8] 付仕明,潘增富.载人航天器舱内气压下降时的空气强制对流换热[J] .中国空间技术,2007,27(4) :44-47 Fu Shiming,Pan Zengfu.Heat transfer of air forced convection with dropping atmosphere pressure in manned spacecraft cabin [J].Chinese Space Sci and Tech,2007,27(4):44-47(in Chinese) [9] Wong H,Peck R E.Experimental evaluation of air-cooling electronics at high altitudes[J].Transactions of the ASME,2001,123 (4):356-366
点击查看大图
计量
- 文章访问数: 1788
- HTML全文浏览量: 157
- PDF下载量: 701
- 被引次数: 0