Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
04/2011
04/20/2011CN102022753A Low-pollution combustion chamber with premixed and pre-evaporated precombustion part
04/20/2011CN102022752A Impingement cooled crossfire tube assembly
04/20/2011CN102022192A Gas turbine combustion dynamics control system
04/19/2011US7926286 Heat shield for a fuel manifold
04/19/2011CA2465573C Outer and inner cowl-wire wrap to one piece cowl conversion
04/14/2011WO2011042037A1 Combustion apparatus
04/14/2011WO2011012126A3 Gas turbine combustion chamber
04/14/2011WO2011009452A3 Axial-piston motor and method for operating an axial-piston motor
04/14/2011WO2011009451A3 Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
04/14/2011WO2010105709A3 Heat shield element of a heat shield
04/14/2011DE102010037863A1 System und Verfahren zur Verteilung von Brennstoff in einer Turbomaschine System and method for distribution of fuel into a turbomachine
04/14/2011DE102010037811A1 Vorrichtung und Verfahren zum Kühlen von Düsen Apparatus and method for cooling nozzles
04/13/2011EP2309189A2 Low NOx combustor for hydrogen-containing fuel and its operation
04/13/2011EP2309188A1 Combustion device and control method thereof
04/13/2011EP2309187A2 Dual fuel can combustor with automatic liquid fuel purge
04/13/2011EP2307806A1 Burner arrangement for liquid fuels and method for producing a burner arrangement
04/13/2011EP2307805A2 Gas turbine engine combustion chamber comprising cmc deflectors
04/13/2011CN102015086A Methods and systems for feed injector multi-cooling channel
04/13/2011CN102012043A Monolithic fuel injector and related manufacturing method
04/13/2011CN101080596B Gas turbine combustor
04/12/2011US7921653 Internal manifold air extraction system for IGCC combustor and method
04/07/2011US20110079016 Compact aircraft combustor
04/07/2011US20110079014 Burner arrangement, and use of such a burner arrangement
04/07/2011DE112004002704B4 Verbrennungsanlage Incinerator
04/07/2011DE102010037411A1 Brennkammer-zu-Brennkammer-Modenentkopplung mittels Brennstoffaufteilungen auf Brennkammerrohrebene Combustion chamber-to-chamber mode decoupling means fuel splits to combustor level
04/07/2011DE102005054442B4 Brennkammer für eine Gasturbine Combustion chamber for a gas turbine
04/07/2011CA2686713A1 Fuel nozzle and method of repair
04/06/2011EP2306091A2 Fuel premixing module for gas turbine engine combustor
04/06/2011EP2306090A2 Gas turbine combustor
04/06/2011EP1689992B1 Method and apparatus for actuating fuel trim valves in a gas turbine
04/06/2011CN102007342A Burner element and burner with corrosion-resistant insert
04/06/2011CN102007341A Burner
04/06/2011CN101473171B Armor-plated machine components and gas turbines
04/05/2011US7919187 Environmental barrier coating for silicon-containing substrates and process therefor
03/2011
03/31/2011WO2011037646A1 Fuel nozzle assembly for use in a combustor of a gas turbine engine
03/31/2011WO2011036073A1 Helmholtz resonator for a gas turbine combustion chamber
03/31/2011WO2011035444A1 Pressure gain combustion heat generator
03/31/2011DE102010036524A1 Vorrichtung und Verfahren für eine Gasturbinendüse Apparatus and method for a gas turbine nozzle
03/31/2011CA2771615A1 Pressure gain combustion heat generator
03/30/2011EP2302302A1 Helmholtz resonator for a gas turbine combustion chamber
03/30/2011EP2300749A1 Fuel injection method
03/30/2011CN101995033A Methods and systems for dry low NOx combustion systems
03/30/2011CN101230987B Two-stage fuel injector
03/30/2011CN101187477B System for vaporization of liquid fuels for combustion and method of use
03/29/2011CA2506344C Rich quick mix combustion system
03/24/2011WO2011033697A1 Mounting/dismounting jig for combustor tail pipe and tail pipe installation method
03/24/2011WO2011033242A2 Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations.
03/24/2011WO2011032959A1 Combustor of a gas turbine
03/24/2011WO2011032935A2 Method for combusting hydrogen-rich, gaseous fuels in a burner, and burner for performing said method
03/24/2011WO2011032839A1 A method and gas turbine combustion system for safely mixing h2-rich fuels with air
03/24/2011US20110067412 Gas turbine aircraft engines and operation thereof
03/24/2011US20110067401 Lean fuel intake gas turbine system
03/24/2011DE102010037414A1 Prallgekühlte Überschlagrohranordnung Impingement cooled crossfire tube assembly
03/24/2011DE102010037412A1 Zweibrennstoffdüse für eine Turbomaschine Dual fuel nozzle for a turbomachine
03/24/2011DE102010037409A1 Universelles Mehrfachdüsen-Verbrennungssystem und Verfahren Universal multi-nozzle combustion system and method
03/24/2011DE102005025823B4 Verfahren und Vorrichtung zum Kühlen einer Brennkammerauskleidung und eines Übergangsteils einer Gasturbine Method and apparatus for cooling a combustor liner and a transition piece of a gas turbine
03/24/2011CA2774440A1 Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations.
03/23/2011EP2299178A1 A method and gas turbine combustion system for safely mixing H2-rich fuels with air
03/23/2011EP2299177A1 Combustor of a gas turbine
03/23/2011EP2299091A1 Method for Switching over a Gas Turbine Burner Operation from Liquid to Gas Fuel and Vice-Versa
03/23/2011EP2299090A2 Combustion turbine system with integrated ion transport membrane
03/22/2011US7908865 Device for injecting a mixture of air and fuel, and combustion chamber and turbomachine provided with such a device
03/22/2011CA2496908C Stress relief feature for aerated gas turbine fuel injector
03/17/2011WO2011031341A1 Fuel injector for use in a gas turbine engine
03/17/2011WO2011031279A1 Vortex premixer for combustion apparatus
03/17/2011DE102010037052A1 Prallgekühlter hinterer Rahmen eines Übergangsstücks Impingement cooled rear frame of a transition piece
03/17/2011DE102010017779A1 Radiale Einlassleitschaufeln für einen Brenner Radial inlet guide vanes for a burner
03/17/2011CA2773946A1 Vortex premixer for combustion apparatus
03/16/2011EP2295865A2 Combustor tile mounting arrangement
03/16/2011EP2295864A1 Combustion device of a gas turbine
03/16/2011EP2295861A1 Burner, especially for gas turbines
03/16/2011EP2295860A2 Aerodynamic pylon fuel injector system for combustors
03/16/2011EP2295858A1 Stabilising of the flame of a burner
03/15/2011CA2494950C Nested channel ducts for nozzle construction and the like
03/15/2011CA2470682C Foam wall combustor construction
03/10/2011WO2011028287A2 Nanomolecular solid state electrodynamic thruster
03/10/2011WO2011026982A1 Method for switching over a gas turbine burner operation from liquid to gas fuel and vice-versa
03/10/2011WO2010036426A3 Modular transvane assembly
03/10/2011US20110056207 Diffuser for turbine engine including indented annular webs
03/10/2011DE102010017623A1 Monolithischer Brennstoffinjektor und zugehöriges Herstellungsverfahren Monolithic fuel injector and manufacturing method thereof
03/09/2011EP2292977A2 Cooling arrangement for a combustion chamber
03/09/2011EP2292898A1 Component with film cooling hole
03/09/2011CN1590849B Combustion liner cap assembly for combustion dynamics reduction
03/03/2011WO2011023669A1 Burner, in particular for gas turbines
03/03/2011WO2011023648A2 Swirl blade, burner and gas turbine
03/03/2011DE112009000781T5 Reparierbare Brennstoffdüse und Reparaturverfahren Repairable fuel and repair procedures
03/03/2011DE112009000753T5 Einheitliche Leitung zur Beförderung von Fluiden und Herstellungsverfahren Uniform management for the transport of fluids and methods of manufacture
03/03/2011DE112006000427B4 Brenner zum Verbrennen eines Vorgemischs für eine Gasturbine Burner for burning a premix for a gas turbine
03/03/2011DE102010037049A1 System und Verfahren zur Verbrennungsdynamiksteuerung einer Gasturbine System and method for controlling combustion dynamics of a gas turbine
03/03/2011DE102009038848A1 Brenner, insbesondere für Gasturbinen Burner, in particular for gas turbines
03/03/2011DE102009038845A1 Drallschaufel, Brenner und Gasturbine Swirl blade, burner and gas turbine
03/02/2011EP2290289A2 Gas turbine combustor with improved quench holes arrangement
03/02/2011EP2288852A1 Method for operating a premix burner, and a premix burner for carrying out the method
03/02/2011CN101983305A 燃烧器 Burner
03/02/2011CN101983304A Combustor casing
03/02/2011CA2713576A1 Fuel nozzle swirler assembly
03/01/2011US7896646 Premixing burner arrangement for operating a combustion chamber in addition to a method for operating a combustion chamber
02/2011
02/24/2011WO2009073109A3 Active combustion control for a turbine engine
02/24/2011US20110041507 Integral Liner and Venturi for Eliminating Air Leakage
02/24/2011DE112009000778T5 Reparatur einer Brennstoffdüsenkomponente Repairing a fuel nozzle component
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