Heat management system for aircraft

Refrigeration – Automatic control – Of external fluid or means

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Details

123553, 244117A, 244135R, 60736, 60730, 165 41, 62239, 622386, F25D 1700, B64D 3700

Patent

active

045051240

ABSTRACT:
A novel heat management system for aircraft is provided which is based on the aircraft fuel as the heat exchange medium and comprises a dedicated thermal reserve fuel tank for containing refrigerated aircraft fuel (or other expendable liquid) which is cooled by heat exchange with the primary aircraft fuel flow to the engines, a fuel line loop for conducting fuel through a plurality of heat exchangers associated with cooling loops for heat generating aircraft systems, and a central microprocessor based controller for controlling fuel flow and temperature throughout the fuel loop system and into the aircraft engine.

REFERENCES:
patent: 2917903 (1959-12-01), Stineman et al.
patent: 2941372 (1960-06-01), Taylor
patent: 2943828 (1960-07-01), Van Driest
patent: 3015461 (1962-01-01), Fineblum
patent: 3410502 (1968-11-01), Leadon et al.
patent: 3929305 (1975-12-01), Sabol
patent: 4263786 (1981-04-01), Eng

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