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Performance analyses of the aircraft low-power thermoelectric refrigeration system

  • Beihang University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The aircraft low-power thermoelectric refrigeration system (TRS) is proposed in this paper. By setting the aircraft flight conditions, the variations of the cooling capacity and the refrigeration coefficient with the working current for three flight altitudes are obtained. Its performance is evaluated with the entropy-generation analysis and the take-off loss method. The analyses prove that the thermoelectric refrigeration system has the advantage of precision and should be used in peculiar flight conditions. The results can be an elementary reference for the research.

Original languageEnglish
Title of host publicationProceedings - 6th International Symposium on Heating, Ventilating and Air Conditioning, ISHVAC 2009
Pages2141-2147
Number of pages7
StatePublished - 2009
Event6th International Symposium on Heating, Ventilating and Air Conditioning, ISHVAC 2009 - Nanjing, China
Duration: 6 Nov 20099 Nov 2009

Publication series

NameProceedings - 6th International Symposium on Heating, Ventilating and Air Conditioning, ISHVAC 2009
Volume3

Conference

Conference6th International Symposium on Heating, Ventilating and Air Conditioning, ISHVAC 2009
Country/TerritoryChina
CityNanjing
Period6/11/099/11/09

Keywords

  • Aircraft cooling system
  • Compensation lost
  • Entropy generation analysis
  • Thermoelectric refrigeration

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