Method and apparatus for achieving power augmentation in gas turbines via wet compression
AssigneeThe Dow Chemical Company
InventorsRichard E. Zachary, Roger D. Hudson
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AssigneeThe Dow Chemical Company
InventorsRichard E. Zachary, Roger D. Hudson
Estimating the term…
A wet compression power augmentation apparatus and method for effectively adding a mass flow of water particles to a gas turbine preferably by use of a spray rack group assembly having at least one spray rack water pipe and at least one spray rack water nozzle. Water mass flow is added preferably in increments such that operationally-induced thermal transients within the gas turbine are sufficiently minimized to preserve the structural integrity of the gas turbine. Monitoring of the temperature profile of fluid-cooled rotor blades in the turbine section with an optical pyrometer to detect clogging of cooling pathways in those rotor blades from impurities in the liquid added through the wet compression, monitoring of temperature in proximity to the gas turbine compressor inlet to guard against the possibility of icing, a deformation measurement device, preferably a laser emitter and laser target measuring system mounted to the exterior of the gas turbine housing to detect deformation in the housing of the gas turbine from associated cooling effects of the wet compression technique, and periodic addition of heat and humidity, preferably steam, to the compressor inlet are disclosed.
A method for augmenting the net output of a gas turbine characterized in operation by periods of continuous use exceeding about 4 hours in duration in driving a generator or compressor, the gas turbine having an axial-flow multistage compressor having an inlet for acquiring a working fluid comprising air, the method comprising the steps of:
A method for augmenting the net output of an industrial gas turbine characterized in operation by periods of continuous use exceeding about 4 hours in length in driving a generator or compressor, the industrial gas turbine having an axial-flow multistage compressor having an inlet for acquiring a working fluid comprising air, said axial-flow multistage compressor having a housing, the method comprising the steps of:
A method for augmenting the net output of an industrial gas turbine characterized in operation by periods of continuous use exceeding about 4 hours in length in driving a generator or compressor, the industrial gas turbine having an axial-flow multistage compressor having an inlet for acquiring a working fluid comprising air, said axial-flow multistage compressor having a housing, the method comprising the steps of:
A method for augmenting the net output of a gas turbine having an axial flow multistage compressor for acquiring and compressing a working fluid comprising air, the method comprising the steps of:
Apparatus comprising a gas turbine having an axial-flow multistage compressor having an inlet for acquiring a working fluid comprising air, the apparatus further comprising:
Apparatus comprising an industrial gas turbine having an axial-flow multistage compressor having an inlet for acquiring a working fluid comprising air, the apparatus further comprising:
Dependencies are inferred from the claim text.