Gas turbine engines

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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415181, F02C 900

Patent

active

039568873

ABSTRACT:
A core engine or gas generator for use in a range of gas turbine engines, which consist of a multi-stage compressor and a single stage supersonic turbine, the compressor and turbine being mouned on a single shaft. The compressor includes a number of stages of variable angle and the gas generator has an annular combustion chamber.

REFERENCES:
patent: 2870958 (1959-01-01), Pinsley
patent: 2935246 (1960-05-01), Roy
patent: 2974927 (1961-03-01), Johnson
patent: 2989843 (1961-06-01), Ferri
patent: 3442441 (1969-05-01), Dettmering
patent: 3804335 (1974-04-01), Sohre

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