Method for controlling gas turbine combustor

Details Method for controlling gas turbine combustor Method for controlling gas turbine combustor

1992-12-02

1994-06-14

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

60 39091, 60 3927, F02C 928

Patent

active

053199197

ABSTRACT:
A method for controlling a gas turbine combustor which comprises nozzles for injecting fuel into a combustor and which serves to combust the fuel with air in a combustion chamber so as to rotatively drive a gas turbine by combustion gas compressed as a result of combustion of a fuel, wherein the ratio of a flow rate of fuel supplied into the combustor to a flow rate of air supplied into the combustor is changed in accordance with at least one of the states of fuel, air and rotational frequency of the turbine.

REFERENCES:
patent: 3584459 (1971-06-01), Amann
patent: 3977182 (1976-08-01), Schroff
patent: 4138842 (1979-02-01), Zwick
patent: 4380894 (1983-04-01), Abo et al.
patent: 4648242 (1987-03-01), Griesinger
patent: 4766721 (1988-08-01), Iizuka et al.
patent: 5121597 (1992-06-01), Urushidani et al.
patent: 5127229 (1992-07-01), Ishibashi et al.
patent: 5201181 (1993-04-01), Ohmori et al.

Affiliated with

Also associated with

Rating

Method for controlling gas turbine combustor does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method for controlling gas turbine combustor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for controlling gas turbine combustor will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1239677