Gas turbine engines employing fixed volume combustion

Power plants – Combustion products used as motive fluid – Plural combustion products generators in ring coaxial with...

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60 3943, 60 3976, F02C 500

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active

046930752

ABSTRACT:
A gas turbine engine includes a rotor forming an inducer and a turbine which succesively register with a series of circumferentially spaced combustion chambers. The engine has the capability of firing less than the total number of combustion chambers for each cycle of rotor rotation.

REFERENCES:
patent: 1077314 (1913-11-01), Stern
patent: 1395995 (1921-11-01), George
patent: 2659198 (1953-11-01), Cook
patent: 2928239 (1960-03-01), Goldstein
patent: 3756019 (1973-09-01), Holzapfel et al.
Hill et al., Mechanics and Thermodynamics of Propulsion, Addison-Wesley Co., Reading, Mass., p. 147.

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