Gas turbine and a method for controlling a gas turbine

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S039281, C060S039511, C060S803000

Reexamination Certificate

active

07404294

ABSTRACT:
Method and arrangement for providing and controlling a gas turbine (1) at least one turbine (11, 20, 20′), at least one compressor (2, 5) driven by the turbine and a combustion chamber (16) arranged between the compressor and the turbine in the airflow path. The gas turbine includes devices (8) for direct measurement of the air mass flow at a position upstream of the combustion chamber in the airflow path, with the aim of regulating the quantity of fuel that is delivered to the combustion chamber (16) on the basis of the measured air mass flow.

REFERENCES:
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patent: 5129222 (1992-07-01), Lampe et al.
patent: 5533329 (1996-07-01), Ohyama et al.
patent: 6095793 (2000-08-01), Greeb
patent: 6405521 (2002-06-01), Ranasinghe et al.
patent: 6945030 (2005-09-01), Hirayama et al.
patent: 701503 (1953-12-01), None
patent: 806345 (1958-12-01), None
International Search Report for International Patent Application PCT/SE2004/000856, dated Aug. 4, 2004.

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