Heat pipe

Heat exchange – Intermediate fluent heat exchange material receiving and... – Liquid fluent heat exchange material

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122366, F28D 1502

Patent

active

053357205

ABSTRACT:
A heat pipe comprising a hermetic shell tube, a heat conveying fluid within the shell tube and a plurality of capillary circumferential or axial grooves provided entirely of an inner surface of the shell. A capillary axial channel structure which includes axially extending plates defining a U-shaped or V-shaped channels therebetween circumferential grooves and having an opening defining therein a meniscus of the heat conveying fluid in the liquid phase at least in the evaporator section and the condenser section. The capillary axial channel structure may comprise an inner tube for defining a tubular, axially extending capillary space therebetween. The inner tube has open ends disposed within the evaporation and condensation sections for allowing the heat conveying fluid to flow therethrough.

REFERENCES:
patent: 3528494 (1970-09-01), Levedahl
patent: 3734173 (1973-05-01), Moritz
patent: 4846263 (1989-07-01), Miyazabi et al.
T. Ogushi et al., "Composite Wick Heat Pipes", Advances in Heat Pipe Technology, Proceedings of the IVth International Heat Pipe Conference, Sep. 7-10, 1981, London, UK, pp. 651-663.
W. E. Ellis, "The Space Active Thermal Control Technical Challenge", published by NASA, 27th Aerospace Sciences Meeting, Jan. 9.varies.12, 1989 (AIAA 1989), Reno Nevada, pp. 1-12.

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