Invention Application
US20110072826A1 CAN TO CAN MODAL DECOUPLING USING CAN-LEVEL FUEL SPLITS 审中-公开
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CAN TO CAN MODAL DECOUPLING USING CAN-LEVEL FUEL SPLITS
Abstract:
In exemplary embodiments, a gas turbine system is provided. The gas turbine system can include a compressor configured to compress air and combustor cans in flow communication with the compressor, the combustor cans being configured to receive compressed air from the compressor and to combust a fuel stream. The gas turbine system can also include a multi-circuit manifold coupled to the combustor cans and configured to provide a split fuel stream from the fuel stream to the combustor cans.
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