发明名称 Cryogenic cooler
摘要 An improved cryogenic cooler 100 includes a flange 106 with an elongated pressure vessel 120 extending therefrom. The pressure vessel 120 is connected to the flange 106 at a proximal end thereof. The pressure vessel 120 is adapted to cool a surface in the proximity of the distal end thereof. Vibration isolation is provided at both proximal and distal ends of the elongated pressure vessel. A coupler 126 serves to maintain a gap between the distal end of the pressure vessel 120 and the surface at cryogenic temperatures. In a specific embodiment, the coupler 234 has a coefficient of thermal expansion which is less than the coefficient of thermal expansion of an end cap 224 on the pressure vessel. The coefficients of expansion are chosen to provide a tight slip fit between the cooler and the coupler at ambient temperatures and a very small continuous air gap at cryogenic temperatures. Another novel feature is the provision of an energy-absorbing ring 114 within the flange to dissipate vibration therein.
申请公布号 US5542254(A) 申请公布日期 1996.08.06
申请号 US19940286859 申请日期 1994.08.05
申请人 HUGHES AIRCRAFT COMPANY 发明人 PRUITT, GERALD R.
分类号 F17C13/00;F25B9/14;F25D19/00;G01J5/06;(IPC1-7):F25B9/00;F25B19/00 主分类号 F17C13/00
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