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filingDate 1966-02-15-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 1967-09-06-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber GB-1081962-A
titleOfInvention Cryogenic fluid transfer arrangement
abstract 1,081,962. Refrigerating. HUGHES AIRCRAFT CO. Feb. 15, 1966 [June 29, 1965], No. 6557/66. Heading F4H. In a cryogenic fluid transfer system, for cooling an optically sensitive detector 30 for use in an aircraft scanning system and adapted to maintain efficient heat transfer during tilting, which comprises a finger 18, thermally insulated within an evacuated cavity 16, bounded by a casing 14 and a window 34 and enlarged at one end to form a refrigerant chamber 28, droplets of liquid refrigerant entrained in a gas stream flowing from a refrigerating machine through filler tube 40 retain sufficient kinetic energy to escape from the opening 68, the gas bleeding off through apertures 66, and be collected in a funnel-shaped section 54 of a device 52 supported in a housing 48, from whence they are conveyed by standpipe section 56 to the refrigerating chamber 28. Exhaust tube 44 mounted in a filler and exhaust housing 36 is made of a high thermal conductivity material, e.g. copper. Silver or bronze wire metal shavings 62 dispose the liquid in heat transfer relationship with the heat load 30. A layer of heat conducting material 60 is formed on the insides of the chambers 28 and 44. The housings 36 and 48 are made of brass and the collector and guide device 52 is made of glass-loaded tetrafluorethylene resin. The housings 36 and 48 are sealed by annular seals 46 and 50, respectively.
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