General Electric Company

Airgas Usa, LLC

William S Adams

Jametra Stitt

Randall John Kleen

Tabrez Shakeel

James K Prochaska

Victor Alfonso Gonzalez Tellez

Garland W Ferguson

Thomas Edward Stowell

Joanne Burrows

Louis N Hannett

Nileshpuri Goswami

Charles Cory

Timothy LeBlanc

Edward Benya

A system and method for preventing icing in the combustion inlet air path of a gas turbine system. An air intake system of the gas turbine system supplies intake air to a gas turbine engine. The air intake system includes an air filter inlet house to filter the intake air. The air filter inlet house includes at least one filter stage having an array of pulse filters, with each of the pulse filters being hydrophobic. A combustion inlet air path is in fluid communication with the air intake system and the gas turbine engine. The combustion inlet air path receives the filtered air from the air filter inlet house and supplies the filtered air as combustion inlet air to an inlet of the gas turbine engine. A surface of at least one component in the combustion inlet air path includes an anti-icing coating to prevent ice from forming thereon.

System and method for preventing icing in the combustion inlet air path of a gas turbine system

Aspects of the invention include a nozzle assembly having a housing configured for attachment to the wall of the vessel. The housing has a proximal end portion and a distal end portion spaced from the proximal end portion along a length of the housing. The housing defines a passageway extending from the proximal end portion to the distal end portion, which is delineated by an inner surface of the housing. The nozzle assembly further includes a nozzle that has a base portion adapted for coupling to the housing, a shaft portion that extends from the base portion, and a tip portion coupled to the shaft portion of the nozzle. The tip portion defines a plurality of orifices. The nozzle also has an outer surface extending along a length of the nozzle that is spaced from the inner surface of the housing to create a gap when the nozzle is coupled to the housing.

Nozzle assemblies for coolant systems, methods, and apparatuses

Embodiments of the disclosure relate to transient event mitigating systems and methods that can be incorporated into a power generation system. The power generation system can include an exciter coupled to an alternating current (AC) generator that provides electric power to power lines. The transient event mitigating system can include an automatic voltage regulator that detects a transient event in one or more of the power lines and configures a power converter to respond to the transient event by increasing an amount of direct current (DC) voltage coupled into the power converter. The power converter can provide the increased DC voltage to an exciter coil of the exciter for a transitory period of time in order to adjust the electric power generated by the AC generator and mitigate adverse effects of the transient event.

Systems and methods for mitigating transient events in a power generation system

A system is provided for controlling power generation. For example, the system may include a drive, an electrical generator coupled to the drive, and a controller coupled to the drive. The controller may include a stabilizing mode responsive to a utility signal representative of a grid destabilizing event.

Generator control having power grid communications

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Sugar Land, TX, United States of America

William S Adams