US2018016983A1PendingUtilityA1
State determining device, operation controlling device, gas turbine, and state determining method
Assignee: MITSUBISHI HITACHI POWER SYSPriority: Feb 3, 2015Filed: Nov 27, 2015Published: Jan 18, 2018
Est. expiryFeb 3, 2035(~8.5 yrs left)· nominal 20-yr term from priority
F05D 2270/061F01D 25/36F02C 9/263F02C 7/057F01D 21/003F05D 2270/05F01D 15/10F02C 9/00F02C 9/28F05D 2270/303F05D 2270/306
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Claims
Abstract
A state determining device determines a state of a gas turbine connected to an electric generator. The gas turbine includes a compressor that compresses intake air into compression air, a fuel supply device that supplies fuel, a combustor that mixes the compression air supplied from the compressor and the fuel supplied from the fuel supply device and combusts a resultant mixture to generate combustion gas, and a turbine that is rotated with the generated combustion gas.
Claims
exact text as granted — not AI-modified1 . A state determining device that determines a state of a gas turbine connected to an electric generator, the gas turbine comprising a compressor that compresses intake air into compression air, a fuel supply device that supplies fuel, a combustor that mixes the compression air supplied from the compressor and the fuel supplied from the fuel supply device and combusts a resultant mixture to generate combustion gas, and a turbine that is rotated with the generated combustion gas, the state determining device comprising:
an instruction-value detecting unit that detects a difference in an instruction value related to an output of the gas turbine; an output detecting unit that detects a difference in an output of the electric generator; and a determining unit that determines an operation of the gas turbine has departed from a predetermined relation when a difference between the difference in the instruction value and the difference in the output is equal to or larger than a threshold.
2 . The state determining device according to claim 1 , wherein the instruction value is a fuel-flow instruction value of fuel to be supplied from the fuel supply device to the combustor.
3 . The state determining device according to claim 1 , wherein
the instruction-value detecting unit detects a difference between a detected instruction value and an instruction value detected at a last time, and the output detecting unit detects a difference between a detected output and an output detected at a last time.
4 . An operation controlling device comprising:
the state determining device according to claim 1 ; and a controlling device that controls the gas turbine on a basis of the instruction value and the output of the electric generator.
5 . The operation controlling device according to claim 4 , wherein the controlling device changes a value of the detected output of the electric generator to a value with smaller fluctuation when the state determining device has determined that an operation of the gas turbine departs from a predetermined relation.
6 . The operation controlling device according to claim 5 , wherein the controlling device uses a value at a last time as a value of the output of the electric generator when the state determining device has determined that an operation of the gas turbine departs from a predetermined relation.
7 . The operation controlling device according to claim 4 , wherein the controlling device changes a calculated value to a value with smaller fluctuation on a basis of a value of the output of the electric generator when the state determining device has determined that an operation of the gas turbine departs from a predetermined relation.
8 . A gas turbine comprising:
a compressor that compresses intake air into compression air; a fuel supply device that supplies fuel; a combustor that mixes the compression air supplied from the compressor and the fuel supplied from the fuel supply device and combusts a resultant mixture to generate combustion gas; a turbine that is rotated with the generated combustion gas; and the operation controlling device according to claim 4 .
9 . A state determining method that determines a state of a gas turbine connected to an electric generator, the gas turbine comprising a compressor that compresses intake air into compression air, a fuel supply device that supplies fuel, a combustor that mixes the compression air supplied from the compressor and the fuel supplied from the fuel supply device and combusts a resultant mixture to generate combustion gas, and a turbine that is rotated with the generated combustion gas, the state determining method comprising steps of:
detecting a difference in an instruction value related to an output of the gas turbine; detecting a difference in an output of the electric generator; and determining that an operation of the gas turbine has departed from a predetermined relation when a difference between the difference in the instruction value and the difference in the output is equal to or larger than a threshold.Join the waitlist — get patent alerts
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