日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
予冷ターボジェットエンジンにおけるジェット噴射を用いた熱交換器の除霜
吹場 活佳井上 翔佐藤 哲也大久保 英敏
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ジャーナル フリー

2008 年 56 巻 657 号 p. 464-470

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An innovative defrosting method for precooled turbojet engines are presented, and validated in this study using experimental methods. High speed gas jet was impinged on the cooling tubes of a heat exchanger for the purpose of defrosting. The coolant of the heat exchanger was liquid nitrogen, and whose temperature was 83K. The air flow speed, the air temperature and the air humidity were 1.0m/s, 23ºC and 59%, respectively. The effects of the jet duration, jet intervals and humidity of the jet gas on the heat exchange were assessed. As a result, we found that the presenting defrosting method is valid for the defrosting of the precooler.

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© 2008 The Japan Society for Aeronautical and Space Sciences
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