Aft fan gas turbine engine

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60 39142, 244135R, F02K 302

Patent

active

051613697

ABSTRACT:
An aft fan gas turbine engine comprises a coaxially related compressor, compressor turbine, fan turbine, and aft fan. An annular fuel tank is disposed about the compressor and an annular combustion chamber is disposed between the compressor and turbine.

REFERENCES:
patent: 2644298 (1953-07-01), McLeod
patent: 2943815 (1960-07-01), Besson
patent: 3332242 (1967-07-01), Johnson

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