Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
05/2007
05/30/2007EP1790908A2 Gas turbine combustor dome repair method
05/30/2007EP1790828A2 Dirt separator for compressor diffuser in gas turbine engine
05/30/2007EP1789728A1 Method and apparatus for providing an afterburner fuel-feed arrangement
05/30/2007EP1789606A1 Smooth outer coating for combustor components and coating method therefor
05/30/2007CN1318805C Gas turbine combustion chamber
05/30/2007CN1318797C Burner for heat generator
05/30/2007CA2568818A1 Methods and apparatuses for assembling a gas turbine engine
05/30/2007CA2560561A1 Methods and apparatuses for assembling a gas turbine engine
05/29/2007US7222488 Fabricated cowl for double annular combustor of a gas turbine engine
05/28/2007CA2568972A1 Combustor dome repair method
05/24/2007US20070113558 Combustion liner for gas turbine formed of cast nickel-based superalloy and method
05/24/2007US20070113556 Combustion chamber end wall with ventilation
05/24/2007DE102006053679A1 Niedrigemissionsbrennkammer und Betriebsverfahren Low emission combustion chamber and operating procedures
05/23/2007EP1788310A2 System for Coupling Flow from a Centrifugal Compressor to an Axial Combustor for Gas Turbines
05/23/2007EP1788309A2 Methods and apparatus for operating gas turbine engine systems
05/23/2007EP1787062A1 Improved combustor heat shield and method of cooling
05/22/2007CA2568474A1 System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines
05/22/2007CA2183753C Tangential entry fuel nozzle
05/17/2007US20070107439 Fastening a combustion chamber inside its casing
05/17/2007US20070107437 Low emission combustion and method of operation
05/17/2007US20070107436 Premixing device for low emission combustion process
05/16/2007EP1785672A2 Reduced thermal system assembly and process of making same
05/16/2007EP1785671A1 Ventilated combustor dome
05/16/2007EP1785612A1 High efficiency thermal machine
05/16/2007CN1965197A Premix burner with staged liquid fuel supply and also method for operating a premix burner
05/16/2007CN1316198C Premixed exit ring pilot burner
05/15/2007US7216488 Methods and apparatus for cooling turbine engine combustor ignition devices
05/15/2007US7216486 Method for operating a turbine group
05/15/2007CA2567878A1 Rear of combustion chamber with ventilation
05/15/2007CA2458304C Gas turbine combustor by-pass valve device
05/15/2007CA2384153C Simple low cost fuel nozzle support
05/15/2007CA2377284C Fuel injector heat shield
05/15/2007CA2283693C Cooling supply manifold assembly for cooling combustion turbine components
05/10/2007WO2007051705A1 Fuel lance
05/10/2007WO2007051698A1 Burner lance
05/10/2007US20070105061 Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement
05/10/2007US20070101727 Helical channel for distributor and method
05/10/2007US20070101722 Open cooled component for a gas turbine, combustion chamber, and gas turbine
05/09/2007EP1783429A2 Methods and apparatus for injecting fluids into turbines engines
05/09/2007EP1783427A2 Combustion turbine fuel recirculation system and nitrogen purge system
05/09/2007EP1783342A2 Methods and apparatus for injecting fluids into a turbine engine
05/09/2007EP1676078A4 Combustion method and apparatus for carrying out same
05/09/2007CN1959213A Nozzle structure of combustion chamber in low heat value of gas turbine, and combustion method
05/07/2007CA2566802A1 Methods and apparatus for injecting fluids into turbine engines
05/07/2007CA2566789A1 Methods and apparatus for injecting fluids into a turbine engine
05/03/2007US20070099142 Premix burner with staged liquid fuel supply and also method for operating a premix burner
05/03/2007US20070095071 Apparatus for assembling gas turbine engine combustors
05/02/2007EP1327108B1 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine
05/02/2007CN1957208A Injector for liquid fuels and stepped premix burner comprising said injector
05/02/2007CN1955548A Gas turbine engine combustor hot streak control
05/02/2007CN1313778C Panel seal for an air handling unit
05/01/2007CA2565743A1 Methods and apparatus for operating gas turbine engines
04/2007
04/26/2007WO2007006680A3 Hot gas-conducting housing element, protective shaft jacket, and gas turbine system
04/26/2007US20070089427 Two-branch mixing passage and method to control combustor pulsations
04/26/2007US20070089426 Cumbustor with staged fuel premixer
04/26/2007US20070089419 Combustor for gas turbine engine
04/26/2007US20070089417 Catalytic reformer with upstream and downstream supports, and method of assembling same
04/26/2007DE102006050422A1 Combustion chamber for gas turbine engine has first and second turbulators for staged mixing of charge to combustion chamber
04/25/2007EP1777461A2 Attachment of a ceramic combustor can
04/25/2007EP1777460A1 Fastening of a combustion chamber inside its housing
04/25/2007EP1777459A2 Combustor for gas turbine
04/25/2007EP1777458A1 Improvement of the performances of a combustion chamber by multiperforating the walls
04/25/2007CN1952487A Combustor with staged fuel premixer
04/24/2007US7208230 High temperature gas turbine and optical reflector coating system for heat exchanging
04/24/2007CA2425895C Process for drilling holes in a metallic workpiece having a thermal barrier coating
04/24/2007CA2252077C Steam cooling type gas turbine combustor
04/19/2007US20070084219 Performance of a combustion chamber by multiple wall perforations
04/19/2007US20070084217 Combustor and component for a combustor
04/19/2007US20070084215 System of attaching an injection system to a turbojet combustion chamber base and method of attachment
04/19/2007DE102005050029A1 Resonatorvorrichtung für eine Brennkammer, Brennkammer und Verfahren zur Einstellung der akustischen Eigenschaften einer Brennkammer A resonator for a combustion chamber, combustion chamber and method for adjusting the acoustic characteristics of a combustion chamber
04/18/2007EP1775517A2 Bolting configuration for joining ceramic combustor liner to metal mouting attachments
04/18/2007EP1775516A2 Gas turbine combustor
04/18/2007EP1775515A2 Resonating device for combustion chamber, combustion chamber and method for adjusting the acoustic characteristics of a combustion chamber
04/18/2007CN1948732A Bolting configuration for joining ceramic combustor liner to metal mouting attachments
04/18/2007CN1311195C Thermal shield for component carrying hot gases, especially for structural components of gas turbines
04/17/2007US7204089 Arrangement for the cooling of thermally highly loaded components
04/12/2007WO2007040829A1 Turbine engine having acoustically tuned fuel nozzle
04/12/2007WO2007003587A3 Molding compound for producing a refractory lining
04/11/2007EP1771640A1 Multi-zone tubing assembly and installing method for a transition piece of a gas turbine
04/11/2007CA2555091A1 Fuel system and method of reducing emission
04/10/2007US7200998 Gas turbine combustor and operating method thereof
04/10/2007US7200986 Fuel injector
04/10/2007CA2255549C Bluff body premixing fuel injector and method for premixing fuel and air
04/05/2007WO2007036964A1 Method for starting a gas turbine equipped with a gas burner, and axial swirler for said burner
04/05/2007WO2007036486A1 Combustion chamber and gas turbine plant
04/05/2007US20070074520 Combustion chamber of a gas turbine engine with an upstream fairing for separating the gas stream, annular wall forming a cap of the upstream fairing of the chamber, and gas turbine engine with the chamber
04/05/2007US20070074518 Turbine engine having acoustically tuned fuel nozzle
04/05/2007US20070074517 Fuel nozzle having swirler-integrated radial fuel jet
04/05/2007US20070074500 Fuel injector
04/04/2007EP1770333A1 Anti-coking injector arm
04/04/2007EP1770332A1 Device for guiding an element into an orifice of a gas turbine combustion chamber wall
04/04/2007EP1770331A2 Method of controlling bypass air split to gas turbine combustor
04/04/2007CN1942710A Premixing burner arrangement for operating a burner chamber and method for operating a burner chamber
04/03/2007US7198860 hot gas path components of a combustion turbine engine, and specifically to ceramic insulating tiles applied over portions of a gas turbine component
04/03/2007US7197882 Turbojet diffuser
03/2007
03/29/2007WO2007034230A1 Fuel injector
03/29/2007WO2007033876A1 An arrangement for preparation of a fuel for combustion
03/29/2007US20070068166 Device for guiding an element in an orifice in a wall of a turbomachine combustion chamber
03/29/2007US20070068165 Diffuser for a gas turbine, and gas turbine for power generation
03/29/2007CA2623358A1 Fuel injector
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