Abstract: Disclosed are systems and methods for active inlet turbine control. The systems and methods may include receiving a plurality of signals, determining a temperature gradient across an inlet of a gas turbine engine, and transmitting an activation signal to a modulating valve. Each of the plurality of signals may correspond to a temperature measured by one of a plurality of sensors located proximate the inlet of the gas turbine engine. The temperature gradient across the inlet of the gas turbine engine may be determined based on the plurality of signals. The activation signal may be operative to open or close the modulating valve based on the temperature gradient.

Abstract: Disclosed are systems and methods for active inlet turbine control. The systems and methods may include receiving a plurality of signals, determining a temperature gradient across an inlet of a gas turbine engine, and transmitting an activation signal to a modulating valve. Each of the plurality of signals may correspond to a temperature measured by one of a plurality of sensors located proximate the inlet of the gas turbine engine. The temperature gradient across the inlet of the gas turbine engine may be determined based on the plurality of signals. The activation signal may be operative to open or close the modulating valve based on the temperature gradient.

Abstract: A method (110) of controlling an imbalance response in a power plant comprising first and second gas turbine engines and a steam turbine driven by steam generated by exhaust from the first and second gas turbine engines can comprise operating the first gas turbine engine at a first power output (116A), operating the second gas turbine engine at a second power output (116B), monitoring load demand from a power grid operating at a steady state condition (114), detecting a load imbalance on the power grid (120) that causes a deviation from the steady state condition, and adjusting the first power output and the second power output incongruently (128) during the imbalance response to change the first power output and the second power output to match the deviation from the steady state condition depending on contemporaneous efficiency states of the first and second gas turbine engines.

Abstract: A method of reducing applied heat within an inlet duct of a gas turbine generating electricity includes applying heat to the inlet duct of the gas turbine to attain an initial temperature set point and to produce conditions sufficient for preventing formation of ice within the inlet duct, measuring a position of an inlet guide vane (IGV) of the gas turbine, an inlet duct temperature, and an inlet duct relative humidity to determine a thermodynamic state in the inlet duct, evaluating the thermodynamic state to determine if the conditions are sufficient for preventing formation of ice within the inlet duct, and in response to determining that sufficient conditions exist within the inlet duct for preventing formation of ice, adjusting the applied heat to maintain the measured inlet duct temperature.

Abstract: A method of reducing applied heat within an inlet duct of a gas turbine generating electricity includes applying heat to the inlet duct of the gas turbine to attain an initial temperature set point and to produce conditions sufficient for preventing formation of ice within the inlet duct, measuring a position of an inlet guide vane (IGV) of the gas turbine, an inlet duct temperature, and an inlet duct relative humidity to determine a thermodynamic state in the inlet duct, evaluating the thermodynamic state to determine if the conditions are sufficient for preventing formation of ice within the inlet duct, and in response to determining that sufficient conditions exist within the inlet duct for preventing formation of ice, adjusting the applied heat to maintain the measured inlet duct temperature.

Abstract: A method (110) of controlling an imbalance response in a power plant comprising first and second gas turbine engines and a steam turbine driven by steam generated by exhaust from the first and second gas turbine engines can comprise operating the first gas turbine engine at a first power output (116A), operating the second gas turbine engine at a second power output (116B), monitoring load demand from a power grid operating at a steady state condition (114), detecting a load imbalance on the power grid (120) that causes a deviation from the steady state condition, and adjusting the first power output and the second power output incongruently (128) during the imbalance response to change the first power output and the second power output to match the deviation from the steady state condition depending on contemporaneous efficiency states of the first and second gas turbine engines.

Abstract: A method of controlling operation of a first power plant in response to changing power grid conditions can comprise: receiving a power-plant-specific power assignment from an operator of a grid system, monitoring an operating frequency of the power grid relative to a control frequency, operating at least one power generator of the first power plant at the control frequency to provide a local power output to meet the power-plant-specific power assignment under steady state conditions, detecting a load imbalance from the power grid wherein the operating frequency and the control frequency are different, and operating the at least one power generator to provide a power-plant-specific imbalance response wherein the local power output is adjusted based on a power-plant-specific-trait of the first power plant relative to a second power plant working with the operator.

Abstract: Disclosed are systems and methods for active inlet turbine control. The systems and methods may include receiving a plurality of signals, determining a temperature gradient across an inlet of a gas turbine engine, and transmitting an activation signal to a modulating valve. Each of the plurality of signals may correspond to a temperature measured by one of a plurality of sensors located proximate the inlet of the gas turbine engine. The temperature gradient across the inlet of the gas turbine engine may be determined based on the plurality of signals. The activation signal may be operative to open or close the modulating valve based on the temperature gradient.

Abstract: Disclosed are systems and methods for active inlet turbine control. The systems and methods may include receiving a plurality of signals, determining a temperature gradient across an inlet of a gas turbine engine, and transmitting an activation signal to a modulating valve. Each of the plurality of signals may correspond to a temperature measured by one of a plurality of sensors located proximate the inlet of the gas turbine engine. The temperature gradient across the inlet of the gas turbine engine may be determined based on the plurality of signals. The activation signal may be operative to open or close the modulating valve based on the temperature gradient.

Abstract: A security system comprising: a first gateway device; a second gateway device; and a duplex communication line, wherein a first proxy part of the first gateway device is configured, if an inbound data is of a specific protocol, to receive a communication information of the specific protocol transmitted by the inbound data and to send the communication information of the specific protocol to the second gateway device, and, if the inbound data is not of the specific protocol, not to send the inbound data to the second gateway device, and wherein the second proxy part is configured, when the second gateway device receives the communication information of the specific protocol from the first proxy part, to acquire a destination address for communication in an internal network from the communication information of the specific protocol and to send the communication information of the specific protocol to the destination address.

Abstract: A security system comprising: a first gateway device; a second gateway device; and a duplex communication line, wherein a first proxy part of the first gateway device is configured, if an inbound data is of a specific protocol, to receive a communication information of the specific protocol transmitted by the inbound data and to send the communication information of the specific protocol to the second gateway device, and, if the inbound data is not of the specific protocol, not to send the inbound data to the second gateway device, and wherein the second proxy part is configured, when the second gateway device receives the communication information of the specific protocol from the first proxy part, to acquire a destination address for communication in an internal network from the communication information of the specific protocol and to send the communication information of the specific protocol to the destination address.

Abstract: A security system comprising: a first gateway device; a second gateway device; and a duplex communication line, wherein a first proxy part of the first gateway device is configured, if an inbound data is of a specific protocol, to receive a communication information of the specific protocol transmitted by the inbound data and to send the communication information of the specific protocol to the second gateway device, and, if the inbound data is not of the specific protocol, not to send the inbound data to the second gateway device, and wherein the second proxy part is configured, when the second gateway device receives the communication information of the specific protocol from the first proxy part, to acquire a destination address for communication in an internal network from the communication information of the specific protocol and to send the communication information of the specific protocol to the destination address.