Gas turbine apparatus

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

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Details

60746, F02C 722

Patent

active

047350520

ABSTRACT:
In a gas turbine apparatus of a premixed gas combustion type, a plurality of fuel supply systems are provided for supplying fuels to a combustion chamber of the gas turbine apparatus after the fuels are mixed with a high-pressure air, and the supply of fuels from the plurality of fuel supply systems is controlled according to programmed patterns which are predetermined for the fuel supply systems. According to a variation of the turbine load, the patterns of fuel supplies are executed in a transferred manner at a number of transfer points along a variation of the turbine load, with equal amounts of fuel reduced and increased stepwisely in the precedingly and subsequently executed patterns at each of the transfer points.

REFERENCES:
patent: 3925002 (1975-12-01), Verdouw
patent: 4112676 (1978-09-01), DeCorso
patent: 4344280 (1982-08-01), Minakawa et al.
patent: 4356698 (1982-11-01), Chamberlain
patent: 4589260 (1986-05-01), Krockow
patent: 4603548 (1986-08-01), Ishibashi et al.
patent: 4683715 (1987-08-01), Iizuka et al.

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