Power unit with gas turbine

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

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Details

60261, F02C 308, F02K 302

Patent

active

043898424

ABSTRACT:
A gas turbine driving a compressor is supplemented by a centrifugal injection chamber which receives fuel as well as air compressed by the compressor; the chamber is configured as an annular nozzle, surrounding the turbine discharge duct, both feeding a mixing tube with thrust nozzle. A portion of the combustion gases is discharged via the annular nozzle, the remainder is fed via a control valve to the turbine.

REFERENCES:
patent: 2229805 (1941-01-01), Graves
patent: 2531761 (1950-11-01), Zucrow
patent: 2715814 (1955-08-01), Barr
patent: 2747363 (1956-05-01), Cohen et al.
patent: 3613361 (1971-10-01), Rifkin

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