Patent application number | Description | Published |
20090289013 | Method for determining the filterability of jet fuel containing additive(s) and conditions for the delivery of acceptable water content fuel - It has been discovered that jet fuel containing enhanced thermal stability additives and water can be delivered with a final water content of 15 ppm or less via existing jet fuel distribution system by controlling the fuel flow rate through the fuel delivery system comprising one or more filter coalescers and separator systems, said controlled fuel flow rate being determined by passing a sample of actual fuel through a sample of the fuel filter at various fuel flow rates to identify the flowrate at which the fuel effluent contains 15 ppm or less. | 11-26-2009 |
20100312033 | OLEFIN FEED PURIFICATION PROCESS - A light olefin feed for an olefin utilization process is subjected to a water wash to remove water-soluble contaminants after which the water is separated from the olefin by coalescence separation at a low temperature, typically below 40° C. The coalescence separation technique is effective for separating the olefins from the water with its dissolved contaminants. If desired, a supplemental washing may be carried out by adding additional water to the feed/water mix after the initial wash step but before the coalescer in order to remove provide additional contaminant removal. | 12-09-2010 |
20140007498 | AVIATION GAS TURBINE FUEL WITH IMPROVED LOW TEMPERATURE OPERABILITY - The addition of biodiesel to petroleum-based kerosene jet fuels in very low concentrations can lower the temperature at which crystals appear in the fuel. The fuels can comprise a blend of a hydrocarbon base fuel component and, for example, up to 1000 ppm, v/v of the total fuel, of a biodiesel component comprising a lower alkyl ester of a fatty acid of natural origin having from 8 to 24 carbon atoms; these blends can be characterized by improved low temperature flow properties, especially of Cloud Point (ASTM D 2500), which can be lower than that of the petroleum fuel component without the alkyl ester, even in the presence of dissolved water up to the saturation level. | 01-09-2014 |
20140187827 | BLENDING OF DEWAXED BIOFUELS WITH MINERAL-BASED KERO(JET) DISTILLATE CUTS TO PROVIDE ON-SPEC JET FUELS - The present invention describes a method of making a jet fuel composition comprising: providing a mineral-based kero/jet-type distillate component having certain enumerated physico-chemical properties, typically an off-spec jet fuel; providing a deoxygenated and dewaxed renewable component derived from triglycerides and/or fatty acids and having an isoparaffin to normal paraffin ratio from about 2:1 to about 6:1 and an aromatics content less than about 1 vol %; and blending from about 75 vol % to about 97 vol % of the mineral-based distillate components with from about 3 vol % to about 25 vol % of the renewable component to form an on-spec blended jet fuel composition. | 07-03-2014 |
Patent application number | Description | Published |
20110192147 | MODEL-BASED CONTROLS FOR SELECTIVE CATALYST REDUCTION SYSTEM - Systems and methods are provided for controlling ammonia slip downstream of a selective catalyst reduction (SCR) system. The SCR system can include a SCR reactor having a catalyst, inlet, and outlet. The SCR system can also include an injector for injecting a reductant into the SCR reactor at a location upstream from the inlet of the SCR reactor. An estimated value, a reference value, and an error between the two values of ammonia adsorbed on the catalyst surface can be provided. A saturation indication can also be provided to indicate whether the catalyst surface is saturated with the estimated value of adsorbed ammonia. The saturation indication and the error between the estimated and reference values of adsorbed ammonia can be used to adjust a command signal by an open-loop control scheme. The injection of the reductant into the SCR reactor can also be regulated by the command signal. | 08-11-2011 |
20120083933 | METHOD AND SYSTEM TO PREDICT POWER PLANT PERFORMANCE - The present disclosure relates to the use of hybrid predictive models to predict one or more of performance, availability, or degradation of a power plant or a component of the power plant. The hybrid predictive model comprises at least two model components, one based on a physics-based modeling approach and one based on an observational or data-based modeling approach. The hybrid predictive model may self-tune or self-correct as operational performance varies over time. | 04-05-2012 |
20120102951 | APPARATUS FOR REDUCING EMISSIONS AND METHOD OF ASSEMBLY - A heat recovery steam generator (HRSG) is coupled to a gas turbine engine that is configured to combust a fuel in air to produce shaft power and a flow of exhaust gases including oxides of nitrogen (NO | 05-03-2012 |
20120260668 | Combined Cycle Power Plant - A combined cycle power plant is provided and includes a gas turbine engine to generate power, a heat recovery steam generator (HRSG) to produce steam from high energy fluids produced from the generation of power in the gas turbine engine, a steam turbine engine to generate additional power from the steam produced in the HRSG and a thermal load reduction system to reduce thermal loading of components of the HRSG and/or the steam turbine engine during at least startup and/or part load operations, which includes an eductor by which a mixture of compressor discharge air and entrained ambient air is injectable into the HRSG and/or an attemperator to cool superheated steam to be transmitted to the steam turbine engine. | 10-18-2012 |
20120317989 | SYSTEMS AND METHODS FOR COMBUSTOR EMISSIONS CONTROL - The present application thus provides a gas turbine engine system. The gas turbine engine system may include a gas turbine engine, a nitrogen oxides reduction system in communication with a flow of combustion gases downstream from the gas turbine engine, and a nitrogen oxides controller to control the ratio of nitrogen dioxide to nitrogen oxides in the flow of combustion gases entering the nitrogen oxides reduction system. | 12-20-2012 |
20130031910 | Efficient Selective Catalyst Reduction System - The present application provides a gas turbine engine system. The gas turbine engine system may include a gas turbine engine producing a flow of combustion gases, an emissions reduction system in communication with the gas turbine engine, a flow of ammonia to be injected into the flow of combustion gases, and a source of compressed gas to vaporize the flow of ammonia. | 02-07-2013 |
20140075954 | Methods And Systems For Substance Profile Measurements In Gas Turbine Exhaust - Methods and systems for substance profile measurements in gas turbine exhaust. In an embodiment, a concentration of a substance may be determined and associated with a combustor out of a plurality of combustors. An alert may be transmitted in reference to the combustor when the concentration of the substance crosses a threshold level. | 03-20-2014 |
20140126991 | SYSTEMS AND METHODS FOR ACTIVE COMPONENT LIFE MANAGEMENT FOR GAS TURBINE ENGINES - The present application thus provides an active cooling system for a compressor and a turbine of a gas turbine engine. The active cooling system may include an air extraction pipe extending from the compressor to the turbine, a heat exchanger positioned about the air extraction pipe, and an external air cooling system in communication with the air extraction pipe. | 05-08-2014 |