Performance Analyses of the Aircraft Low-power Thermoelectric Refrigeration System
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 entropygeneration 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.
Thermoelectric refrigeration Entropy generation analysis Aircraft cooling system Compensation lost
Xingjuan Zhang Yubai Wang
School of Aeronautic Science & Engineering,Beihang University,Beijing,China
国际会议
The 6th International Symposium on Heating,Ventilating and Air Conditioning(第六届国际暖通空调学术会议)
南京
英文
2141-2147
2009-11-06(万方平台首次上网日期,不代表论文的发表时间)