Aircraft compound cycle propulsion engine

Details Aircraft compound cycle propulsion engine Aircraft compound cycle propulsion engine

1995-12-14

1997-12-02

Koczo, Michael

Power plants

Reaction motor

Interrelated reaction motors

60269, 60598, F02K 500

Patent

active

056923724

ABSTRACT:
A ducted fan aircraft compound cycle engine comprises a core engine which includes a compressor, three rotary internal combustion engines fed by the compressor and a power turbine to receive the combustion products of the rotary and combustion engines. The rotary internal combustion engines drive the compressor and the power turbine drives the fan. The engine combines the thermal efficiency of the rotary internal combustion engine with the compact size and light weight of the gas turbine engines.

REFERENCES:
patent: 2385366 (1945-09-01), Lysholm
patent: 2518660 (1950-08-01), Browne
patent: 2580591 (1952-01-01), Pouit
patent: 5471834 (1995-12-01), Kapich
"The Wankel RC Engine", R. F. Ansdale, Iliffe Books Ltd., 1968, pp. 39-43.

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