摘要:
A system (200) for modifying the operation and/or performance of a gas turbine (205) comprising one or more combustors, the system comprising at least one sensor (240) for determining a gas exhaust temperature (220) for the gas turbine, and a controller (245) operable to receive the gas exhaust temperature from the at least one sensor, estimate a transient heat transfer rate (225) for the gas turbine based at least in part on the gas exhaust temperature, and control the one or more combustors based at least in part on the estimated transient heat transfer rate for the gas turbine.
摘要:
Systems and methods for providing stepping actuations in a power generation unit 104 are disclosed. Certain embodiments herein may relate to manipulating actuators to produce a desired output in a power generation unit 104 without disrupting production by the power generation output, such as megawatt and/or steam production. A model may be generated 110 that includes one or more inputs and associated outputs in a power generation unit 104. The model may be leveraged to determine an actuator to adjust to create a desired output, as well as one or more different actuators to adjust to offset an otherwise negative impact on power generation unit 104 production while maintaining the desired output.
摘要:
The subject application involves a method of controlling operation of a gas turbine (10). The method includes determining a first temperature associated with a portion of the gas turbine (10) during operation of the gas turbine (10), and sensing an operational parameter of the gas turbine (10) during operation of the gas turbine (10). An ambient pressure in an ambient environment of the gas turbine (10) is also sensed, and the operational parameter is corrected using the ambient pressure sensed in the ambient environment of the gas turbine (10) to establish a corrected operational parameter. A threshold temperature is determined based at least in part on the corrected operational parameter, and a backup routine is initiated to limit operation of the gas turbine (10) when the temperature associated with the gas turbine (10) is greater than or equal to the threshold temperature.
摘要:
Systems and methods for providing stepping actuations in a power generation unit 104 are disclosed. Certain embodiments herein may relate to manipulating actuators to produce a desired output in a power generation unit 104 without disrupting production by the power generation output, such as megawatt and/or steam production. A model may be generated 110 that includes one or more inputs and associated outputs in a power generation unit 104. The model may be leveraged to determine an actuator to adjust to create a desired output, as well as one or more different actuators to adjust to offset an otherwise negative impact on power generation unit 104 production while maintaining the desired output.
摘要:
A system (200) for modifying the operation and/or performance of a gas turbine (205) comprising one or more combustors, the system comprising at least one sensor (240) for determining a gas exhaust temperature (220) for the gas turbine, and a controller (245) operable to receive the gas exhaust temperature from the at least one sensor, estimate a transient heat transfer rate (225) for the gas turbine based at least in part on the gas exhaust temperature, and control the one or more combustors based at least in part on the estimated transient heat transfer rate for the gas turbine.
摘要:
The subject application involves a method of controlling operation of a gas turbine (10). The method includes determining a first temperature associated with a portion of the gas turbine (10) during operation of the gas turbine (10), and sensing an operational parameter of the gas turbine (10) during operation of the gas turbine (10). An ambient pressure in an ambient environment of the gas turbine (10) is also sensed, and the operational parameter is corrected using the ambient pressure sensed in the ambient environment of the gas turbine (10) to establish a corrected operational parameter. A threshold temperature is determined based at least in part on the corrected operational parameter, and a backup routine is initiated to limit operation of the gas turbine (10) when the temperature associated with the gas turbine (10) is greater than or equal to the threshold temperature.