| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide improved systems and methods for controlling a plurality of fuel flows, which does not lead to combustion instabilities when a plurality of different fuel types are utilized in a gas turbine. <P>SOLUTION: A plurality of fuel types provided to a machine and a plurality of fuel circuits 110 associated with the machine can be identified, each of the plurality of fuel circuits 110 adapted to be provided with one or more of the plurality of fuel types. A fuel flow parameter for calculating fuel flow can be identified, and a respective fuel flow for each of the one or more fuel types provided to each of the plurality of fuel circuits 110 may be calculated based at least in part on the identified fuel flow parameter. Based at least in part on the calculation of the respective fuel flows, operation of one or more fuel flow control devices providing fuel to the plurality of fuel circuits 110 can be controlled. <P>COPYRIGHT: (C)2011,JPO&INPIT</p> |
