Method of and device for controlling fuel for gas turbine

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S039281, C060S039465

Reexamination Certificate

active

07047747

ABSTRACT:
Values such as a pressure for supplying fuel gas to a gas turbine, a pressure in a combustor casing of the gas turbine, an output of a generator connected to the gas turbine, and a controlled output for a flow rate control valve are detected by sensors. The detected values are input into a control device. A differential pressure across the flow rate control valve and a target value of the differential pressure are also input into the control device. The control device performs a desired arithmetic operation based on these input values to output a lift instruction for a pressure control valve.

REFERENCES:
patent: 4716719 (1988-01-01), Takahashi et al.
patent: 5272637 (1993-12-01), Urushidani et al.
patent: 5899073 (1999-05-01), Akimaru
patent: 6901735 (2005-06-01), Lohn
patent: 195 18 634 (1995-10-01), None
patent: 0 377 292 (1990-07-01), None
patent: 0 661 426 (1995-07-01), None
patent: 11-236824 (1999-08-01), None
Patent Abstracts of Japan, JP 61-205340, Sep. 11, 1986.

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