Patent application number | Description | Published |
20130319041 | NITROGEN-COOLED DYNAMOELECTRIC MACHINE SYSTEM AND RELATED METHOD - Various embodiments of the invention include systems and methods for cooling a dynamoelectric machine. In some embodiments, a system is disclosed including: at least one of a nitrogen separation unit (NSU) or an air separation unit (ASU) for extracting nitrogen from an inlet air source; a nitrogen expander fluidly connected with the at least one of the NSU or the ASU, the nitrogen expander for expanding the extracted nitrogen; and a dynamoelectric machine fluidly connected with the nitrogen expander, the dynamoelectric machine configured to receive the expanded nitrogen for cooling the dynamoelectric machine. | 12-05-2013 |
20140007553 | HOT WATER INJECTION FOR TURBOMACHINE - A turbomachine is provided and includes a combustor in which a first compressed air is combustible along with fuel and which is receptive of water. The water is provided to the combustor subsequent to the water being used to cool a second compressed air, and the water is used to cool the second compressed air prior to the second compressed air being used to atomize the fuel. | 01-09-2014 |
20140060057 | METHOD AND APPARATUS FOR HEATING LIQUID FUEL SUPPLIED TO A GAS TURBINE COMBUSTOR - A method of heating liquid fuel upstream of a combustor in a system where compressor discharge air is cooled before being supplied to fuel nozzles in the combustor includes the steps of passing the compressor discharge air through a heat exchanger in heat exchange relationship with the liquid fuel to heat the liquid fuel and cool the compressor discharge air; supplying the heated liquid fuel and the cooled compressor discharge air to the combustor. | 03-06-2014 |
20140090387 | FUEL HEATING SYSTEM FOR A POWER PLANT AND METHOD OF HEATING FUEL - A fuel heating system for a power plant includes an exhaust structure having an interior region for receiving an exhaust gas therein. Also included is a fluid injection arrangement comprising a first fluid duct for transferring a fluid, the first fluid duct extending at least partially throughout the interior region of the exhaust structure for heating the fluid. Further included is a heat exchanger for receiving the fluid and a liquid fuel, the fluid heating the liquid fuel during passage of the liquid fuel through the heat exchanger. | 04-03-2014 |
20140110092 | ATOMIZING AIR HEAT FOR ATTEMPERATION - An attemperation system and an atomizing air system are integrated for a combined cycle turbine including a gas turbine and a steam turbine. The atomizing air system receives compressor discharge air for fuel atomization. The atomizing air system includes an atomizing air cooler that serves to cool the compressor discharge air. A heat recovery steam generator receives exhaust from the gas turbine and generates steam for input to the steam turbine via an attemperation system. A feed water circuit draws feed water from the heat recovery steam generator and communicates in a heat exchange relationship with the atomizing air cooler to heat the feed water. The feed water circuit communicates the heated feed water to the attemperation system of the heat recovery steam generator. | 04-24-2014 |
20140123623 | GAS TURBOMACHINE SYSTEM INCLUDING AN INLET CHILLER CONDENSATE RECOVERY SYSTEM - A gas turbomachine system includes a compressor portion including an inlet portion, a turbine portion fluidically connected to, and mechanically linked with, the compressor portion, and a combustor assembly including at least one combustor fluidically connected to the turbine portion. An inlet system is fluidically connected to the inlet portion of the compressor portion. The inlet system includes an inlet chiller. An inlet chiller condensate recovery system is fluidically connected to the inlet system. The inlet chiller condensate recovery system includes an inlet fluidically connected to the inlet chiller and an outlet fluidically connected to one of the compressor portion and the combustor assembly. | 05-08-2014 |
20140130478 | GAS TURBOMACHINE INCLUDING A FUEL PRE-HEAT SYSTEM - A gas turbomachine includes a compressor portion, a turbine portion operatively connected to the compressor portion, a combustor assembly including at least one combustor fluidically connected to the turbine portion, and an accessory mechanically linked with and driven by the turbine portion. The gas turbomachine also includes a fuel pre-heat system including a fuel pre-heat element having a fuel circuit fluidically connected to the at least one combustor arranged in a heat exchange relationship with a heating medium circuit fluidically connected to at least one of the compressor portion, the turbine portion, and the accessory. | 05-15-2014 |
20150315927 | ENHANCED GENERATOR CAPABILITY IN HOT AMBIENT TEMPERATURES - A gas turbine includes a compressor, a combustor, a turbine, and a generator disposed upstream of the compressor. The gas turbine also includes a heat exchange circuit with a generator cooler circuit cooperable with the generator and circulating a coolant in the generator. The heat exchange circuit also includes a water circuit circulating water in a heat exchange relationship with the generator cooler circuit. The coolant in the generator cooler circuit is cooled by the water in the water circuit. | 11-05-2015 |
20150315970 | BASELOAD EFFICIENCY IMPROVEMENT BY USING CHILLED WATER IN EVAPORATIVE COOLER IN LNG APPLICATION - A heat exchange circuit in a gas turbine includes an evaporative cooling medium circuit circulating an exchange medium, and a cooling source containing fuel. The cooling source is coupled with a supply line in a heat exchange relationship with the evaporative cooling medium circuit. The exchange medium is cooled by the fuel in the supply line, and the evaporative cooling medium circuit directs the cooled exchange medium through the evaporative cooler. The fuel is heated by the evaporative cooling medium circuit, and the supply line directs the heated fuel to the one or more combustors of the gas turbine. The cooler turbine inlet air results in increased baseload output. | 11-05-2015 |