Combustor for gas turbine

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

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60 3955, 60746, F02C 314, F02C 330

Patent

active

049551914

ABSTRACT:
A gas turbine combustor for a gas turbine plant comprises an outer casing and a combustor liner disposed in the outer casing, the interior of the combustor liner constituting a combustor chamber divided into a first stage of combustion area and a second stage of combustion area, disposed downstream of the first stage combustion area. The gas turbine combustor further comprises a nozzle member for supplying a first stage fuel into the first stage combustion area, a header for supplying a second stage fuel into the second stage combustion area, and a header for further supplying water or water vapor into the first stage combustion area. The nozzle member and both the headers are disposed in an end plate closing one end of the outer casing in a concentrical fashion. The flow rates of the first and second stage fuels and the water vapor are controlled by a control unit equipped with the gas turbine combustor.

REFERENCES:
patent: 3693347 (1972-09-01), Kydd et al.
patent: 3826080 (1974-07-01), De Corso et al.
patent: 4112676 (1977-03-01), Decorso
patent: 4259837 (1981-04-01), Russell et al.
patent: 4603548 (1986-08-01), Ishibashi et al.
patent: 4733527 (1988-03-01), Kidd
patent: 4735052 (1988-04-01), Maeda et al.
patent: 4766721 (1988-08-01), Iizuka et al.
Influence of Gas Turbine Combustor Design and Operating Parameters in Effectiveness of NO.sub.x Suppression by Injected Steam or Water, Trans. of ASME Journal of Engineering for Gas Turbines and Power, vol. 107, pp. 706-713; G. L. Touchton; Jul. 1985.

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