JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

このアイテムに関連するファイルはありません。

タイトル'Bootstrap' Configuration for Multistage Pulse-Tube Coolers
本文(外部サイト)http://hdl.handle.net/2060/20080048053
著者(英)Nguyen, Bich; Nguyen, Lauren
著者所属(英)Boeing Co.
発行日2008-12-01
言語eng
内容記述A bootstrap configuration has been proposed for multistage pulse-tube coolers that, for instance, provide final-stage cooling to temperatures as low as 20 K. The bootstrap configuration supplants the conventional configuration, in which customarily the warm heat exchangers of all stages reject heat at ambient temperature. In the bootstrap configuration, the warm heat exchanger, the inertance tube, and the reservoir of each stage would be thermally anchored to the cold heat exchanger of the next warmer stage. The bootstrapped configuration is superior to the conventional setup, in some cases increasing the 20 K cooler's coefficient of performance two-fold over that of an otherwise equivalent conventional layout. The increased efficiency could translate into less power consumption, less cooler mass, and/or lower cost for a given amount of cooling.
NASA分類Fluid Mechanics and Thermodynamics
レポートNOMSC-23500-1
権利Copyright, Distribution as joint owner in the copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/509938


このリポジトリに保管されているアイテムは、他に指定されている場合を除き、著作権により保護されています。