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AssigneeWestinghouse Electric Corp.
InventorsRobert A. Yannone, Terry J. Reed
Estimating the term…
A hybrid digital computer gas turbine power plant control system which may operate in a multiple control loop arrangement is provided with selected process variable monitoring and control and turbine system failure detection means. More specifically, open, shorted, grounded and reversed thermocouples are detected and alarmed. Problems of any one combustor in a multiple combustor arrangement are similarly detected and alarmed. Additionally, automatic correction of previously computed temperature related control inputs is provided in response to detected variations from a predetermined temperature reasonability criterion. Novel placement and orientation of system thermocouples facilitates achieving improved monitoring, detection and control.
A gas turbine electric power plant comprising a gas turbine having compressor, combustion and turbine elements, a generator coupled to said gas turbine for drive power, a fuel system for supplying fuel to said gas turbine combustion elements, a control system including a digital computer and an input/output system therefor, means for operating said fuel system to energize said gas turbine operably coupled between said fuel system and said control means, a plurality of process sensors operably coupled to said control system and disposed to detect plant conditions related to said gas turbine and said generator, said plurality of sensors comprising at least a first arrangement of process temperature sensors operatively associated with said combustion elements, each of said temperature sensors providing a gas discharge temperature indication for at least one corresponding combustion element, means for operating said computer for processing said temperature indications to determine the validity of each of such indications, means for operating said computer for combining valid temperature indications retained after said processing step to derive a control parameter, and means for operating said computer to make control action determinations for implementation by said fuel system operating means and to make predetermine turbine alarm status determinations in response to individual temperature indications derived from at least said first arrangement of process temperature sensors.
A gas turbine electric power plant comprising a gas turbine having compressor, combustion and turbine elements, a generator coupled to said gas turbine for drive power, a fuel system for supplying fuel to said gas turbine combustion elements, a control system for operating said plant in accordance with predetermined criteria and in response to information concerning predetermined plant parameters, means for operating said fuel system operably coupled between said fuel system and said control system, a plurality of sensors operably coupled to said control system and disposed to detect plant conditions related to said gas turbine and said generator, said plurality of sensors including at least a first arrangement of temperature sensors operatively associated with said combustion elements, each of said temperature sensors providing a gas discharge temperature indication for at least one corresponding combustion element, means for processing said temperature indications to determine the validity of each of such indications, means for combining valid temperature indications retained after said processing step to derive a control parameter, and means for operating said control system to make control action determinations for implementation by said fuel system operating means and to make predetermined turbine alarm status determinations, both in response to individual temperature indications derived from at least said first arrangement of temperature sensors.
A gas turbine electric power plant comprising a gas turbine having compressor, combustion and turbine elements, a generator coupled to said gas turbine for drive power, a fuel system for supplying fuel to said gas turbine combustion elements, means for operating said fuel system to energize said gas turbine, a plurality of process sensors disposed to detect plant conditions related to said gas turbine and said generator, said plurality of sensors comprising at least a first arrangement of process temperature sensors operatively associated with said combustion elements, each of said temperature sensors providing a gas discharge temperature indication for at least one corresponding combustion element and means for deriving and displaying alarm status conditions in response to individual temperature indications derived from at least said first arrangement of process temperature sensors, particularized to one or more of the following malfunctions of said process temperature sensors:
As gas turbine electric power plant comprising a gas turbine having compressor, combustion and turbine elements, said turbine element including a blade assembly defining a blade path for discharged gases which terminates at the discharge end of said turbine element, a generator coupled to said gas turbine for drive power, a fuel system for supplying fuel to said gas turbine combustion elements, a digital computer and an input/output system therefor, means for operating said fuel system to energize said turbine operably coupled between said fuel system and said computer, a plurality of process sensors operably coupled to said computer and disposed to detect plant conditions related to said gas turbine and said generator, said plurality of sensors comprising at least a first arrangement of process temperature sensors located at said blade path discharge portion of said turbine element and operatively associated with said combustion elements, each of said temperature sensors providing a gas discharge temperature indication for at least one corresponding combustion element, means for operating said computer for processing said temperature indications to determine the validity of each of such indications, means for operating said computer for combining valid temperature indications retained after said processing step to derive a control parameter, and responsive control action determinations for implementation by said fuel system operating means functionally related to individual temperature indications derived from at least said first arrangement of process temperature sensors.
A method for operating a digital control computer associated with industrial gas turbine apparatus including an electric generator a gas turbine having compressor, combustion and turbine elements, a fuel system for supplying fuel to the combustion elements, and a plurality of process temperature sensors disposed to detect plant conditions related to said gas turbine and said generator, said plurality of sensors comprising at least a first arrangement of process temperature sensors located at the blade path discharge of said turbine elements and operatively associated with said combustion elements, the steps of said method comprising determining individual temperature readings derived from said individual process temperature sensors, processing said derived temperature indications to determine the validity of each of such indications, combining valid temperature indications retained after said processing step to derive a control parameter, and supplying fuel to said fuel system in a manner functionally related to said control parameter.
Dependencies are inferred from the claim text.