Title:
排気温度に基づくガスタービン用モード制御方法およびガスタービン
Document Type and Number:
Japanese Patent JP2013512379
Kind Code:
A
Abstract:
Gas turbine, computer readable medium, and method for controlling an operating point of the gas turbine that includes a compressor, a combustor and a turbine is provided. The method includes determining a turbine pressure ratio, calculating a primary to lean-lean mode transfer threshold reference curve as a function of the turbine pressure ratio, determining at a first time when an exhaust temperature associated with the operating point is higher than an exhaust temperature of the primary to lean-lean mode transfer threshold reference curve for the same turbine pressure ratio, and changing, after a predetermined time after the first time, a split fuel quantity from a first value to a second value if the exhaust temperature associated with the operating point remains higher than the exhaust temperature of the primary to lean-lean mode transfer threshold reference curve.
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Inventors:
Botarreri, claudio
Application Number:
JP2012540368A
Publication Date:
April 11, 2013
Filing Date:
November 19, 2010
Export Citation:
Assignee:
Nuovo Pinone Societa Peratini
International Classes:
F02C9/34; F02C9/00; F02C9/28; F23R3/28
Domestic Patent References:
JP2007309279A | 2007-11-29 | |||
JP2002181399A | 2002-06-26 | |||
JP2000205563A | 2000-07-25 | |||
JP2002357320A | 2002-12-13 | |||
JP2002130852A | 2002-05-09 | |||
JP2007077867A | 2007-03-29 | |||
JP2005155622A | 2005-06-16 | |||
JP2002097970A | 2002-04-05 | |||
JP2004027848A | 2004-01-29 | |||
JP2003176726A | 2003-06-27 |
Foreign References:
US20040107702A1 | 2004-06-10 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka