Invention Application
- Patent Title: GAS TURBINE LOAD/UNLOAD PATH CONTROL
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Application No.: US16254909Application Date: 2019-01-23
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Publication No.: US20200232645A1Publication Date: 2020-07-23
- Inventor: Jason Nathaniel Cook , Jason Dean Fuller , Christopher James Wenner
- Applicant: General Electric Company
- Main IPC: F23R3/34
- IPC: F23R3/34 ; F02C7/228 ; F02C9/26 ; F02C9/56 ; F01D15/10

Abstract:
A loading/unloading method for a gas turbine system is disclosed. The gas turbine system includes a combustion section featuring a primary combustion stage with a first plurality of fuel nozzles and a downstream, secondary combustion stage with a second plurality of fuel nozzles. For loading, the method progresses through each of a plurality of progressive combustion modes that sequentially activate a higher number of at least one of the first or second plurality of fuel nozzles; and for unloading, the method progresses through each of a plurality of progressive combustion modes that sequentially activate a lower number of at least one of the first or second plurality of fuel nozzles. During each combustion mode, regardless of whether loading or unloading, a primary combustion stage exit temperature of a combustion gas flow is controlled to be within a predefined target range corresponding to the respective combustion mode.
Public/Granted literature
- US11384940B2 Gas turbine load/unload path control Public/Granted day:2022-07-12
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