Patent ID: 9194303
Filing Date: 2015-11-24
Classification: F02C,F05D,F23R

Abstract:
1. A gas turbine system, comprising: a compressor configured to compress air; a fuel source configured to supply fuel to a plurality of fuel manifolds; a combustor configured to receive the air from the compressor, to receive the fuel from the plurality of fuel manifolds, and to combust the air and the fuel into combustion products; a turbine configured to extract work from the combustion products; a plurality of fuel control valves, each corresponding to a respective one of the plurality of fuel manifolds and configured to throttle the fuel to the combustor when the gas turbine system is operating in an electrical island mode; and a controller comprising a processor and an article of manufacture that includes one or more tangible, machine-readable media at least collectively comprising instructions executable by the processor, the instructions comprising instructions to: