Combustor controller

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

Reexamination Certificate

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Details

C060S039281

Reexamination Certificate

active

10528408

ABSTRACT:
A turbine inlet temperature operating section (15) determines the turbine inlet temperature T4based on the flow rate Gf and temperature Tf of fuel being supplied to a combustor (3) and the flow rate G3and temperature T3of air. Based on the turbine inlet temperature T4, a pilot ratio operating section (16) sets a pilot ratio, and a bypass valve operating section (17) and an IGV opening operating section (18) generate a bypass valve control signal and an IGV control signal, respectively.

REFERENCES:
patent: 4094142 (1978-06-01), Pfefferle
patent: 5533329 (1996-07-01), Ohyama et al.
patent: 6095793 (2000-08-01), Greeb
patent: 2004/0008010 (2004-01-01), Ebrahim et al.
patent: 2011091 (1979-07-01), None
patent: 51-98414 (1976-08-01), None
patent: 54-90409 (1979-07-01), None
patent: 7-189743 (1985-07-01), None
patent: 61-96332 (1986-05-01), None
patent: 5-52174 (1993-03-01), None
patent: 8-178290 (1996-07-01), None
patent: 11-22490 (1999-01-01), None

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