Patent application number | Description | Published |
20100031387 | PREVENTION OF TRANSGENE ESCAPE IN GENETICALLY MODIFIED PERENNIALS - Genes can be introduced into plants that confer desirable traits such as, drought and stress tolerance, insect and pest resistance, as well as environmental qualities such as phyto-remediation. However, possibility for transgene escape to wild and non-transformed species raises commercial and ecological concerns. Disclosed herein are methods and compositions for generating sterile perennial plants for the prevention of transgene escape. For example, sterile switchgrass can be produced using these methods, for example which can be used to produce biofuel. | 02-04-2010 |
20110078820 | METHODS AND COMPOSITIONS FOR TRANSGENIC PLANTS PRODUCING ANTIMICROBIAL PEPTIDES FOR ENHANCED DISEASE RESISTANCE - The present invention provides methods and compositions for producing transgenic plants having increased disease resistance resulting from the expression of exogenous nucleotide sequences encoding antimicrobial peptides. | 03-31-2011 |
20110197316 | METHODS AND COMPOSITIONS FOR TRANSGENIC PLANTS WITH ENHANCED ABIOTIC STRESS RESISTANCE AND BIOMASS PRODUCTION - The present invention provides methods and compositions for producing transgenic plants having enhanced tolerance to biotic and/or abiotic stress and/or enhanced biomass production resulting from the expression of exogenous nucleotide sequences encoding SUMO E3 ligase or an active fragment thereof. | 08-11-2011 |
20130117882 | METHODS AND COMPOSITIONS FOR ENHANCED RESISTANCE TO ABIOTIC STRESS IN PLANTS - The present invention provides transgenic plants having increased tolerance to abiotic stress comprising a recombinant nucleic acid molecule, said recombinant nucleic acid molecule comprising a nucleotide sequence encoding miR319 operatively associated with a promoter, a nucleotide sequence that is antisense to a portion of consecutive nucleotides of a nucleotide sequence encoding PCF5, and/or a nucleotide sequence that encodes a portion of consecutive nucleotides of a nucleotide sequence encoding PCF5, which when expressed produces an antisense nucleotide sequence, wherein expression of the nucleotide sequence confers increased tolerance to abiotic stress. Also provided are methods and compositions for making said transgenic plants. | 05-09-2013 |
20140237684 | METHODS AND COMPOSITIONS FOR TRANSGENIC PLANTS WITH ENHANCED RESISTANCE TO BIOTIC AND ABIOTIC STRESS - The present invention provides methods and compositions for producing transgenic plants having increased resistance to biotic and/or abiotic stress and comprising an exogenous nucleotide sequence encoding a cysteine protease inhibitor. | 08-21-2014 |
Patent application number | Description | Published |
20090158738 | METHODS AND APPARATUS FOR STARTING UP COMBINED CYCLE POWER SYSTEM - Methods and apparatus for fast starting and loading a combined cycle power system are described. In one example embodiment, a method for starting a combined cycle power generation system is provided. The system includes a gas turbine and a steam turbine. The method includes loading the gas turbine at a loading rate that is facilitated to be at an increased loading rate, setting a first predetermined value for a bypass pressure set point for high-pressure steam, and increasing the first predetermined value to a second predetermined value at a predetermined rate. | 06-25-2009 |
20100236240 | Systems and Methods for Pre-Warming a Heat Recovery Steam Generator and Associated Steam Lines - Embodiments of the invention can provide systems and methods for pre-warming a heat recovery steam generator and associated steam lines. According to one embodiment, a method for pre-warming a heat recovery steam generator can be provided. The method can include providing heating steam from a steam source. The heating steam is directed from the steam source to a superheater so that at least a portion of the superheater can be warmed. Once exiting the superheater, the heating steam can be further directed from the superheater to at least one bypass line and maintained in the bypass line until the bypass line attains a predefined temperature or pressure. Furthermore, the method can include directing, after the bypass line attains a predefined temperature or pressure, at least a portion of the heating steam from the bypass line to a reheater so that the reheater can be warmed. | 09-23-2010 |
20100242430 | COMBINED CYCLE POWER PLANT INCLUDING A HEAT RECOVERY STEAM GENERATOR - A combined cycle power plant includes a gas turbomachine, a steam turbomachine operatively coupled to the gas turbomachine, and a heat recovery steam generator operatively coupled to the gas turbomachine and the steam turbomachine. The heat recovery steam generator includes a high pressure reheat section provided with at least one high pressure superheater and at least one reheater. The combined cycle power plant further includes a controller operatively connected to the gas turbomachine, the steam turbomachine and the heat recovery steam generator. The controller is selectively activated to initiate a flow of steam through the heat recovery steam generator following shutdown of the gas turbomachine to lower a temperature of at least one of the high pressure superheater and the at least one reheater and reduce development of condensate quench effects during HRSG purge of a combined cycle power plant shutdown. | 09-30-2010 |
20110220037 | Oxygen-Enriched Air Assisting System for Improving the Efficiency of Cogeneration System - Systems and methods for exhaust gas recirculation in which at least a desired effective oxygen concentration is maintained for stable combustion at increased recirculation rates. Oxygen-enriched gas is injected into the recirculated exhaust gas to achieve the desired effective oxygen concentration. | 09-15-2011 |
20120055157 | FUEL HEATING SYSTEM - A system may include an insulated water tank configured to store a first heated water from a first plant component during operation of a plant, and a fuel heater comprising a heat exchanger, wherein the heat exchanger is configured to transfer heat from the first heated water to a fuel for a gas turbine engine during startup of the plant. | 03-08-2012 |
Patent application number | Description | Published |
20100307157 | METHODS RELATING TO TURBINE ENGINE CONTROL AND OPERATION - A method of controlling a combustion turbine engine, wherein the engine includes: a fuel line including a heat exchange portion; a heating value meter; a cold leg bypass comprising an alternate fuel line that bypasses the heat exchange portion, the cold leg bypass being connected to the fuel line at an upstream fork and at a fuel mixing junction, the fuel mixing junction being positioned such that a length of fuel line between it and the inlet to the combustor is short; and valves for controlling the amount of fuel being directed through the heat exchange portion; the method comprising: measuring the heating value of the fuel; determining a target fuel temperature range based on the heating value and a target Modified Wobbe Index range; and controlling the fuel that bypasses the heat exchange portion such that the temperature of the fuel is within the target temperature range. | 12-09-2010 |
20110185744 | METHOD AND APPARATUS FOR COMBINED CYCLE POWER PLANT STARTUP - A combined cycle power plant startup system is provided. The system includes a steam turbine, a HRSG, a condenser, and a bypass system. The steam turbine may include a turbine section. The HRSG may be operably connected to the steam turbine for providing steam to the steam turbine. The HRSG may include a reheater. The bypass system may be configured to adjust the steam pressure downstream of the reheater by routing steam downstream of the reheater to the condenser. The bypass system may include at least one bypass line, at least one control valve operably connected to the at least one bypass line, a pressure gauge configured to monitor the steam pressure downstream of the reheater, and a controller configured to communicate with the pressure gauge and operate the at least one control valve. | 08-04-2011 |
20120036828 | Combined Cycle Power Plant Including a Heat Recovery Steam Generator - A combined cycle power plant includes a gas turbomachine, a steam turbomachine operatively coupled to the gas turbomachine, and a heat recovery steam generator operatively coupled to the gas turbomachine and the steam turbomachine. The heat recovery steam generator includes a high pressure reheat section provided with at least one high pressure superheater and at least one reheater. The combined cycle power plant further includes a controller operatively connected to the gas turbomachine, the steam turbomachine and the heat recovery steam generator. The controller is selectively activated to initiate a flow of steam through the heat recovery steam generator following shutdown of the gas turbomachine to lower a temperature of at least one of the high pressure superheater and the at least one reheater and reduce development of condensate quench effects during HRSG purge of a combined cycle power plant shutdown. | 02-16-2012 |
20130098041 | SYSTEM FOR TURBINE COMBUSTOR FUEL MIXING - A system includes a plurality of interconnected mixing assemblies configured to mix a first fuel and water to generate a first mixture, and mix a second fuel and the water to generate a second mixture. The first and second fuel mixtures are configured to combust in a plurality of combustors of a gas turbine. The interconnected mixing assemblies include first and second fuel passages, a water passage, first and second mixers, first and second fuel valves, and first and second water valves disposed in an integrated housing. The first fuel valve has a first fuel flow coefficient between approximately 1.0 to 1.5, the second fuel valve has a second fuel flow coefficient between approximately 3.0 to 5.0, the first water valve has a first water flow coefficient between approximately 0.4 to 0.55, and the second water valve has a second water flow coefficient between approximately 3.5 to 5.0. | 04-25-2013 |
20140321967 | Gas Turbine Power Augmentation System - The present application provides a power augmentation system for use with a gas turbine engine. The power augmentation system may include a compressor discharge manifold, an inlet bleed heat system in communication with the compressor discharge manifold via an inlet bleed heat line, and an auxiliary compressor in communication with the compressor discharge manifold via the inlet bleed heat line. | 10-30-2014 |
Patent application number | Description | Published |
20080315419 | CHROMIUM/TITANIUM/ALUMINUM-BASED SEMICONDUCTOR DEVICE CONTACT - A contact to a semiconductor including sequential layers of Cr, Ti, and Al is provided, which can result in a contact with one or more advantages over Ti/Al-based and Cr/Al-based contacts. For example, the contact can: reduce a contact resistance; provide an improved surface morphology; provide a better contact linearity; and/or require a lower annealing temperature, as compared to the prior art Ti/Al-based contacts. | 12-25-2008 |
20130260490 | Light Emitting Device Substrate with Inclined Sidewalls - A light emitting device having improved light extraction is provided. The light emitting device can be formed by epitaxially growing a light emitting structure on a surface of a substrate. The substrate can be scribed to form a set of angled side surfaces on the substrate. For each angled side surface in the set of angled side surfaces, a surface tangent vector to at least a portion of each angled side surface in the set of angled side surfaces forms an angle between approximately ten and approximately eighty degrees with a negative of a normal vector of the surface of the substrate. The substrate can be cleaned to clean debris from the angled side surfaces. | 10-03-2013 |
20140308766 | Chromium/Titanium/Aluminum-based Semiconductor Device Contact - A contact to a semiconductor including sequential layers of Cr, Ti, and Al is provided, which can result in a contact with one or more advantages over Ti/Al-based and Cr/Al-based contacts. For example, the contact can: reduce a contact resistance; provide an improved surface morphology; provide a better contact linearity; and/or require a lower annealing temperature, as compared to the prior art Ti/Al-based contacts. | 10-16-2014 |
Patent application number | Description | Published |
20130269351 | MICROMIXER ASSEMBLY OF A TURBINE SYSTEM AND METHOD OF ASSEMBLY - A micromixer assembly of a turbine system includes a plate having at least one aperture comprising a receiving diameter. Also included is at least one tube having an inlet and an outlet for receiving a flow and dispersing the flow to a combustor, wherein the at least one tube includes an inner diameter and an outer diameter, wherein the outer diameter is configured to fit within the receiving diameter of the at least one aperture, wherein the at least one tube is operably coupled at a location on the outer diameter to the receiving diameter of the at least one aperture by exerting a radial force on the inner diameter of the tube. | 10-17-2013 |
20140075755 | SYSTEM AND METHOD FOR MANUFACTURING AN AIRFOIL - A system for manufacturing an airfoil includes an outer surface of the airfoil, a cavity inside the airfoil, and a collimator outside of the airfoil. The system further includes a fluid column flowing from the collimator toward the outer surface of the airfoil, and a laser beam inside the fluid column creates a confined laser beam directed at the outer surface of the airfoil. A method for manufacturing an airfoil includes confining a laser beam inside a fluid column to create a confined laser beam, directing the confined laser beam at an outer surface of the airfoil, and creating a passage through the outer surface of the airfoil with the confined laser beam. | 03-20-2014 |
20140076857 | SYSTEM AND METHOD FOR MANUFACTURING AN AIRFOIL - A system for manufacturing an airfoil includes a laser beam and a first fluid column surrounding the laser beam to create a confined laser beam directed at the airfoil. A gas flowing inside the airfoil disrupts the first fluid column inside the airfoil. A method for manufacturing an airfoil includes confining a laser beam inside a first fluid column to create a confined laser beam and directing the confined laser beam at a surface of the airfoil. The method further includes creating a hole through the surface of the airfoil with the confined laser beam, flowing a gas inside the airfoil, and disrupting the first fluid column with the gas flowing inside the airfoil. | 03-20-2014 |
20140076868 | SYSTEM AND METHOD FOR MANUFACTURING AN AIRFOIL - A system for manufacturing an airfoil includes a laser beam and a first fluid column surrounding the laser beam to create a confined laser beam directed at the airfoil. A liquid flowing inside the airfoil disrupts the first fluid column inside the airfoil. A method for manufacturing an airfoil includes confining a laser beam inside a first fluid column to create a confined laser beam and directing the confined laser beam at a surface of the airfoil. The method further includes creating a hole through the surface of the airfoil with the confined laser beam, flowing a liquid inside the airfoil, and disrupting the first fluid column with the liquid flowing inside the airfoil. | 03-20-2014 |
20140294490 | WELDING PROCESS, WELDING SYSTEM, AND WELDED ARTICLE - A welding process, welding system and welded article are disclosed. The welding process includes directing energy from one or more fusion beams to join a first element to a second element and to join the first element to a third element. The directing of the energy is at a first lateral angle and a second lateral angle with respect to the first element. The welding system includes an energy emitting device, a first fusion beam and a second fusion beam. The first fusion beam and the second fusion beam are oriented to extend diagonally through an article. The laser welded article includes the first element joined to the second element, and the first element joined to the third element. A fillet weld is formed in a first inaccessible portion between the first element and the second element and a second inaccessible portion between the first element and the third element. | 10-02-2014 |
20150052751 | SYSTEM AND METHOD FOR MANUFACTURING AN AIRFOIL - A system for manufacturing an airfoil includes an unfocused laser beam and a first fluid column surrounding the unfocused laser beam to create a confined laser beam directed at the airfoil. A sensor inside the airfoil detects penetration of the confined laser beam through the surface of the airfoil. A method for manufacturing an airfoil includes confining an unfocused laser beam inside a first fluid column to create a confined laser beam, directing the confined laser beam at a surface of the airfoil, and penetrating the surface of the airfoil with the confined laser beam. The method further includes detecting penetration of the confined laser beam through the surface of the airfoil. | 02-26-2015 |
20150129150 | LASER ASSISTED CASTING AND RELATED SYSTEM - Various embodiments include methods and related systems for laser-assisted casting. Some embodiments include a method including: performing laser ablation to a preliminary wax casting model to form a modified wax model including at least one additional feature absent from the wax casting substrate; coating the modified wax model to form a mold shape around the modified wax model; and removing the modified wax model to leave a casting mold including the at least one additional feature. | 05-14-2015 |
20150129151 | LASER ASSISTED CASTING OF SURFACE TEXTURE AND RELATED SYSTEM - Various embodiments include methods and related systems for laser-assisted casting. Some embodiments include a method including: performing laser ablation to a preliminary wax casting model to form a modified wax model including at least one surface texture element absent from the wax casting substrate; coating the modified wax model to form a mold shape around the modified wax model; and removing the modified wax model to leave a casting mold including the at least one surface texture element. | 05-14-2015 |
20150129152 | LASER ASSISTED CASTING OF COOLING HOLE AND RELATED SYSTEM - Various embodiments include methods and related systems for laser-assisted casting. Some embodiments include a method including: performing laser ablation to a preliminary wax casting model to form a modified wax model including at least one cooling hole absent from the wax casting substrate; coating the modified wax model to form a mold shape around the modified wax model; and removing the modified wax model to leave a casting mold including the at least one cooling hole. | 05-14-2015 |
20150129153 | PROCESS CYCLE INCLUDING LASER ASSISTED CASTING AND RELATED SYSTEM - Various embodiments include methods and related systems for laser-assisted casting. Some embodiments include a method including: performing laser ablation on a preliminary wax casting model to form a modified wax model including at least one additional feature absent from the preliminary wax casting model; coating the modified wax model to form a mold shape around the modified wax model; removing the modified wax model to leave a casting mold including the at least one additional feature; forming a shape from a casting material using the casting mold having the at least one additional feature; and scanning the modified wax model to image the at least one additional feature after the performing of the laser ablation. | 05-14-2015 |
20150209899 | METHOD FOR DRILLING A HOLE IN AN AIRFOIL - A method for manufacturing an airfoil is provided, the method including drilling a hole in a near wall of the airfoil using a laser drill and activating a back strike protection in a cavity of the airfoil. The method additionally includes detecting a breakthrough of a laser from the laser drill through the near wall of the airfoil and subsequently initiating a drilling subroutine, with the drilling subroutine including a continued operation of the laser drill. Such a method may provide for an improved hole, such as a cooling passage, in the airfoil. | 07-30-2015 |
20150209900 | METHOD DETERMINING HOLE COMPLETION - The present disclosure provides a method for determining a hole completing in laser drilling of a hole in a near wall of an airfoil. The method includes drilling a hole in the near wall of the airfoil using a laser drill. The laser drill may move in a pattern relative to the airfoil. The method also includes determining when the drilling of the hole is complete based on a calculated time duration between successive breakthroughs of a laser from the laser drill through the near wall of the airfoil, or based on a calculated time duration since the latest breakthrough of the laser from the laser drill through the near wall of the airfoil. | 07-30-2015 |
20150209901 | METHOD AND SYSTEM FOR DETECTING DRILLING PROGRESS IN LASER DRILLING - A method for detecting drilling progress in laser drilling is provided. The method includes sensing a process condition during the drilling of an airfoil, and sensing a change in the process condition indicative of a breakthrough of a laser from the laser drill through a near wall of the airfoil. The method additionally includes continuing to sense the process condition subsequent to the sensed change in the process condition to improve the accuracy of the breakthrough detection. | 07-30-2015 |