Cooling system for a hypersonic aircraft

Details Cooling system for a hypersonic aircraft Cooling system for a hypersonic aircraft

1990-05-17

1992-09-22

Peters, Jr., Joseph F.

Aeronautics and astronautics

Aircraft structure

244 57, 244163, 165908, 60912, 60267, B64C 100

Patent

active

051490188

ABSTRACT:
A cooling system for a hypersonic aircraft is disclosed which enables hypersonic flight using non-cryogenic fuels. The cooling system positions a primary heat exchanger at an external location on the aircraft which remains relatively cool during hypersonic flight. A working fluid is passed through the primary heat exchanger to the hot parts of a supersonic combustion ram jet engine.

REFERENCES:
patent: 2133514 (1938-10-01), Holmas
patent: 2291607 (1942-08-01), Chaussoh
patent: 2330632 (1943-09-01), Seligman
patent: 3550678 (1970-12-01), Pfouts
patent: 4273304 (1981-06-01), Frosch et al.
patent: 4505124 (1985-03-01), Mayer
patent: 4687048 (1987-08-01), Edlestein et al.
patent: 4776536 (1988-10-01), Hudson et al.
patent: 4804571 (1989-02-01), Jouffreau
patent: 4986495 (1991-01-01), Stromath et al.

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