PASSIVE COOLING SYSTEM FOR AN AIRCRAFT ELECTRONIC BOX

Yury F. Maydanik; S.  Vershinin; Vladimir G. Pastukhov; M.  Chernysheva; C.  Sarno; C.  Tantolin

doi:10.1615/HeatPipeScieTech.2011003408

热管科学与技术

总编辑s: Leonard L. Vasiliev (open in a new tab) Marcia Barbosa Henriques Mantelli (open in a new tab)

每年出版 4 期

ISSN 打印: 2151-7975

ISSN 在线: 2151-7991

PASSIVE COOLING SYSTEM FOR AN AIRCRAFT ELECTRONIC BOX

卷 1, 册 3, 2010, pp. 251-260

DOI: 10.1615/HeatPipeScieTech.2011003408

Get access

Yury F. Maydanik
Institute of Thermal Physics, Ural Branch of the Russian Academy of Sciences, 107a Amundsen Str., Yekaterinburg, 620016, Russia

S. Vershinin
Institute of Thermal Physics, Ural Branch of the Russian Academy of Sciences, 106 Amundsen St., Ekaterinburg 620016, Russia

Vladimir G. Pastukhov
Institute of Thermal Physics, Ural Branch of the Russian Academy of Sciences, 107a Amundsen Str., Yekaterinburg, 620016, Russia

M. Chernysheva
Institute of Thermal Physics, Ural Branch of the Russian Academy of Sciences, Ekaterinburg, 620016, Russia

C. Sarno
Thales Avionics, 26027 Valence, France

C. Tantolin
Thales Avionics, 26027 Valence, France

摘要

The paper represents the results of development and thermal tests of a cooling system of a seat electronic box, managing the in-flight entertainment system used aboard commercial aircrafts. The system is completely passive and consists of two conventional copper-water miniature heat pipes and two miniature loop heat pipes with R-141b as a working fluid. Two crossbeams of a passenger seat made of aluminum alloy cooled by means of free air convection were used as heat sinks. At the maximum heat load of 100 W the cooling system provides a temperature of a cooled object at a level of not above 81°C at the ambient temperature of 22°C, which is 4°C below that of the maximum specified temperature.

键词: aircrafts, electronic box, passive cooling system, loop heat pipe

对本文的引用

Sarno C., Tantolin C., Hodot R., Maydanik Yu., Vershinin S., Loop thermosyphon thermal management of the avionics of an in-flight entertainment system, Applied Thermal Engineering, 51, 1-2, 2013. Crossref
Chernysheva M.A., Yushakova S.I., Maydanik Yu.F., Copper–water loop heat pipes for energy-efficient cooling systems of supercomputers, Energy, 69, 2014. Crossref
Zilio Claudio, Righetti Giulia, Mancin Simone, Hodot Romain, Sarno Claude, Pomme Vincent, Truffart Bertrand, Active and passive cooling technologies for thermal management of avionics in helicopters: Loop heat pipes and mini-Vapor Cycle System, Thermal Science and Engineering Progress, 5, 2018. Crossref

801 文章浏览量 1840 文章下载统计数据

801 文章浏览量 1840 下载次数 3 Crossref 引用次数 Google
Scholar 引用次数

相似内容的文章:

ETHANE TWO-PHASE THERMAL CONTROL HARDWARE (HP, LHP) FOR CRYOGENICS APPLICATIONS Heat Pipe Science and Technology, An International Journal, Vol.5, 2014, issue 1-4
M. Molina, Donatas Mishkinis, Joaquin Melendez, Alejandro Torres, E. Turrión

NUMERICAL STUDY OF THE PERFORMANCE OF HEAT PIPE-BASED THERMAL MANAGEMENT SYSTEM FOR POWER LITHIUM BATTERY Heat Transfer Research, Vol.54, 2023, issue 14
Ying Zhang, Zhaoqing Ke, Ming Ma, Qi Zeng, Peisheng Li, Wei Wu

EXPERIMENTAL STUDY OF NATURAL-CONVECTION COOLING OF DISCRETE HEATERS ON A PLATE IN RECTANGULAR ENCLOSURE International Heat Transfer Conference 9, Vol.2, 1990, issue
Cha'o-Kuang Chen, C. J. Ho, Y. H. Hsu

LOOP HEAT PIPE APPLICATIONS IN AUTOMOTIVE THERMAL CONTROL Heat Pipe Science and Technology, An International Journal, Vol.5, 2014, issue 1-4
Yuji Saito, Masataka Mochizuki, R. Singh, Tien Nguyen, Tadao Yamada, Aliakbar Akbarzadeh, Thang Nguyen

RESEARCH ON DEFROSTING OF REFRIGERATOR USING PHASE CHANGE MATERIAL HEAT EXCHANGER Heat Transfer Research, Vol.52, 2021, issue 11
Zhongbao Liu, Ruonan Teng, Xin Qi, Chaojie Cheng

PASSIVE COOLING SYSTEM FOR AN AIRCRAFT ELECTRONIC BOX

摘要

相似内容的文章:

最新一期