High performance turbine engine

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60 3907, 60 3975, 60 3983, 60728, F02C 304

Patent

active

049913948

ABSTRACT:
A high performance turbine engine includes refrigeration apparatus powered by the engine and effective upon a fractional air flow received from the engine compressor to provide chilled air for cooling of internal engine components. The refrigeration process facilitates rejection of unwanted heat to ambient air despite high stagnation temperatures at high flight speeds. The invention allows increased turbine inlet temperature and improved fuel efficiency or thrust per pound of engine weight with present-day metals and cooling technology being used for engine construction.

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