Gas turbine jet propulsion engine

Details Gas turbine jet propulsion engine Gas turbine jet propulsion engine

1976-11-29

1980-09-09

Bentley, Stephen C.

Power plants

Reaction motor

Condition responsive thrust varying means

60233, 60261, 60262, F02K 306, F02K 116

Patent

active

042211140

ABSTRACT:
A gas turbine engine has three turbines, the intermediate and high pressure turbines running at substantially constant corrected speed. The low pressure turbine has variable nozzle guide vanes and the low pressure compressor has variable stators so as to enable its speed to be varied, while its mass flow is arranged to be large at low speeds.

REFERENCES:
patent: 2931173 (1960-04-01), Schapker
patent: 2999672 (1961-09-01), Harshman
patent: 3273340 (1966-09-01), Hull, Jr.
patent: 3316714 (1967-05-01), Smith et al.
patent: 3514952 (1970-06-01), Schumacher et al.

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