Thaw flow control for liquid heat transport systems

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

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16510431, 16510417, 16510414, 165 41, 137334, 137339, 137340, 376214, 376367, F28D 1500

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048009520

ABSTRACT:
In a liquid metal heat transport system including a source of thaw heat for use in a space reactor power system, the thaw flow throttle or control comprises a fluid passage having forward and reverse flow sections and a partition having a plurality of bleed holes therein to enable fluid flow between the forward and reverse sections. The flow throttle is positioned in the system relatively far from the source of thaw heat.

REFERENCES:
patent: 1295687 (1919-02-01), Bullard
patent: 3537515 (1970-11-01), Byrd
patent: 3688800 (1972-09-01), Hayner et al.
patent: 4086958 (1978-05-01), Lindner et al.
patent: 4371028 (1983-02-01), Helshoj
patent: 4671348 (1987-06-01), Bauer
"Elements and Concepts of the SP-100 Heat Rejection System", by Edward J. McNamara, pp. 24-28, published in the Fourth Symposium on Space Nuclear Power Systems, Trans. of the 1987 SP-100 Program Sessions, dated Jan. 15, 1987.
"Trade-offs and Studies of the SP-100 Systems Concept", by A. Kirpich et al., pp. 3-8, published in the Fourth Symposium on Space Nuclear Power Systems, Trans. of the 1987 SP-100 Program Sessions, dated Jan. 15, 1987.
"SP-100 Ground Engineering System Project", General Electric Company Proposal No. SP5086, dated Feb. 3, 1986.

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