Pump-assisted heat pipe
AssigneeLockheed Missiles & Space Company, Inc.
InventorsGary D. Bizzell, William F. Ekern
Life of this patent
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AssigneeLockheed Missiles & Space Company, Inc.
InventorsGary D. Bizzell, William F. Ekern
Estimating the term…
A closed-loop heat transfer system comprises a heat pipe (10) and an external liquid-phase pump (11). The heat pipe (10) includes an evaporator (12) and a condenser (13) connected by a conduit (14). The evaporator (12) is a hollow structure having an interior surface defining an evaporation region in which a working field in liquid phase absorbs heat from a heat source by evaporation. A capillary pumping structure, e.g., capillary channels (30) or a fine-mesh screen (41), is provided on or adjacent the interior wall of the evaporator (12). Evaporated working fluid laden with heat is thermodynamically driven substantially adiabatically via the conduit (14) from the evaporator (12) to the condenser (13), wherein the working fluid rejects heat to a heat sink by condensation. Condensed working fluid is thereupon returned from the condenser (13) to the evaporator (12) via external conduits (22, 15) by means of the liquid-phase pump (11). The capillary pumping structure inside the evaporator (12) serves to maintain a constant supply of working fluid in liquid phase adjacent the interior surface of the evaporator (12), thereby promoting efficient transfer of heat from the heat source to the working fluid in the evaporator (12). There is no limitation on the length of the heat pipe (10) caused by capillary pumping requirements of the system. Pursuant to 37 CFR 1.72(b), the foregoing abstract shall not be used for interpreting the scope of the claims herein.
A closed-loop heat transfer system through which a fluid can be circulated substantially independently of gravity and substantially independently of pressure outside said system to transfer heat from a heat source to a heat sink, said system comprising:
Dependencies are inferred from the claim text.