Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
06/2008
06/19/2008WO2008071756A1 Improvements in or relating to burners for a gas turbine engine
06/19/2008DE19640980B4 Vorrichtung zur Dämpfung von thermoakustischen Schwingungen in einer Brennkammer Device for damping thermoacoustic oscillations in a combustion chamber
06/19/2008CA2615029A1 Deflector for bottom of combustion chamber, combustion chamber equipped with said deflector and turbojet engine containing them
06/19/2008CA2606121A1 Floatwall dilution hole cooling
06/18/2008EP1558875B1 Liner for a gas turbine engine combustor having trapped vortex cavity
06/18/2008CN101201176A High expansion fuel injection slot jet and method for enhancing mixing in premixing devices
06/17/2008CA2437758C Thermal barrier coatings with low thermal conductivity
06/12/2008US20080134682 Combustion chamber air inlet
06/11/2008EP1930659A1 Jet engine combustion chamber
06/11/2008EP1930569A1 System for controlling a combustion process for a gas turbine
06/11/2008EP1930546A2 Airfoil with plasma generator for shielding a boundary layer upstream of a film cooling hole and corresponding operating method
06/11/2008EP1930545A2 Airfoil with plasma generator for shielding a boundary layer downstream of a film cooling hole and corresponding operating method
06/11/2008EP1929208A1 Method for starting a gas turbine equipped with a gas burner, and axial swirler for said burner
06/11/2008CN100394110C Gas turbine
06/11/2008CN100393997C Combustion chamber
06/07/2008CA2613268A1 Chamber end, method for producing same, combustion chamber comprising same and turbojet equipped with same
06/05/2008DE19547506B4 Verfahren und Brenner zum Verbrennen von Wasserstoff A method and burner for combusting hydrogen
06/04/2008EP1926937A1 An arrangement for preparation of a fuel for combustion
06/04/2008EP1926936A1 Burner arrangement for a combustion chamber, associated combustion chamber and method for combusting fuel
06/03/2008US7380402 Method for operating a gas turbine and gas turbine system for carrying out the method
05/2008
05/30/2008CA2612043A1 Upstream plasma shielded film cooling
05/30/2008CA2612042A1 Downstream plasma shielded film cooling
05/28/2008EP1924762A2 Gas turbine engine combustion systems
05/28/2008CN101187477A System for vaporization of liquid fuels for combustion and method of use
05/28/2008CN100390389C Seal assembly
05/28/2008CN100390387C Diffuser located between a compressor and a combustion chamber of a gasturbine
05/27/2008US7377117 Transition piece for gas turbine
05/27/2008US7377116 Gas turbine combustor barrier structures for spring clips
05/22/2008WO2008059045A1 Improvements in or relating to combustion apparatus
05/22/2008US20080115506 Combustor liner and heat shield assembly
05/22/2008US20080115502 System for vaporization of liquid fuels for combustion and method of use
05/21/2008EP1923637A2 Triple annular counter rotating swirler
05/21/2008EP1923636A1 Device for injecting a mix of air and fuel, combustion chamber and turbomachine equipped with such a device
05/21/2008EP1923633A2 Active combustion control system for gas turbine engines
05/21/2008EP1923578A2 CMC fastening system
05/21/2008CN101182928A Triple annular counter rotating swirler
05/21/2008CN101182927A 气体燃料喷射器 Gas fuel injector
05/21/2008CN100389287C Combustion chamber flame drum tail sealing structure
05/20/2008US7373781 Methods and apparatus for injecting cleaning fluids into combustors
05/20/2008US7373772 Turbine combustor transition piece having dilution holes
05/20/2008CA2431286C A method and a device for supplying fuel to a combustion chamber
05/17/2008CA2610263A1 Combustor heat shield with variable cooling
05/17/2008CA2608869A1 Combustor liner and heat shield assembly
05/17/2008CA2608622A1 Combustor liner and heat shield assembly
05/16/2008CA2610516A1 Device for injecting a fuel-air mixture, combustion chamber and turbomachine equipped with such device
05/15/2008US20080110172 Catalytic oxidation element for a gas turbine engine
05/15/2008DE202008001702U1 Anlage zur Abgasreinigung für Raketentriebwerke For exhaust gas purification system for rocket engines
05/15/2008CA2665319A1 Combustor nozzle for a fuel-flexible combustion system
05/14/2008EP1921383A2 Combustor dome and methods of assembling such
05/14/2008EP1921382A2 Combustor dome mixer retaining means
05/14/2008EP1921381A2 Combustor and multi combustor including the combustor, and combusting method
05/14/2008EP1921378A2 Method and apparatus for enhanced mixing in premixing devices
05/14/2008EP1921377A2 High expansion fuel injection slot jet and method for enhancing mixing in premixing devices
05/14/2008EP1921376A1 Fuel injection system
05/14/2008CN201059603Y Long-term durability gas turbine flame barrel
05/14/2008CN201059602Y Gas turbine low discharging burning chamber
05/13/2008US7371352 Combustion catalyst coating on the surface of a ceramic thermal barrier coating having a surface microstructure (peaks, spikes, canyons, bowls, tunnels) that provides the necessary turbulent flow and surface area for interaction with a fuel-air mixture in a catalytic combustor of a gas turbine engine
05/13/2008US7370478 Method of controlling a gas combustor of a gas turbine
05/13/2008US7370477 Device for fastening a fluid duct to a turbojet casing
05/13/2008US7370466 Extended flashback annulus in a gas turbine combustor
05/08/2008WO2008052867A1 System for controlling a combustion process for a gas turbine
05/08/2008WO2008052830A1 Fuel-injector nozzle
05/08/2008WO2008033542A3 Gas turbine fuel injector with a removable pilot assembly
05/08/2008US20080104963 Heat Shield Element, Method for Its Production, Hot Gas Lining, and Combustion Chamber
05/08/2008DE102006053278A1 Brennkammervorrichtung Combustion chamber device
05/08/2008DE102006053277A1 Acoustic resonator device for combustion chamber, has front-sided opening connecting resonator and combustion areas, and fluid permeable resonance influencing elements producing turbulence and arranged in resonator area
05/07/2008EP1918642A2 Combustion chamber device
05/07/2008EP1918638A1 Burner, in particular for a gas turbine
05/07/2008EP1918548A2 Dynamic sealing assembly to accomodate differential thermal growth of fuel injector components
05/07/2008EP1917470A1 An apparatus for modifying the content of a gaseous fuel
05/07/2008EP1673576B1 Method and device for the combustion of fuel
05/07/2008EP1649219B1 Gas turbine burner
05/07/2008EP1320705B1 Piloted rich-catalytic lean-burn hybrid combustor
05/07/2008CN101173767A Method and apparatus for reducing stresses induced to combustor assemblies
05/06/2008US7367191 Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine
05/03/2008CA2608623A1 Combustor dome panel heat shield cooling
05/03/2008CA2608287A1 Fuel nozzle flange with reduced heat transfer
05/02/2008WO2008049678A1 Burner, in particular for a gas turbine
05/01/2008US20080098736 Combustor and multi combustor including the combustor, and combusting method
04/2008
04/30/2008EP1916482A2 Method for detecting onset of uncontrolled fuel in a gas turbine combustor
04/30/2008EP1916481A2 Premixing device, gas turbines comprising the premixing device, and methods of use
04/30/2008DE102007046623A1 Flüssigbrennstoffverbesserung für drallstabilisierte Erdgasdüse und Verfahren Liquid fuel improvement for spin-stabilized for natural gas and procedures
04/30/2008DE102006051286A1 Combustion device, has combustion chamber with combustion space and air injecting device including multiple nozzles arranged on circular line, where nozzles have openings formed as slotted holes in combustion space
04/30/2008CN201053353Y Mini turbine jet engine
04/30/2008CN101169252A Aerial engine lean premixed preevaporated low contamination combustion chamber
04/30/2008CN101169251A Gas turbine multiple nozzle dilution, diffusion and combustion system for synthesis gas
04/30/2008CN101169074A Method for detecting onset of uncontrolled fuel in a gas turbine combustor
04/30/2008CN100385173C Cooled flushing fuel injector
04/30/2008CN100385172C Fuel injection apparatus triggered flushing by differential pressure
04/29/2008US7364802 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity
04/29/2008US7363763 Combustor
04/29/2008US7363756 Method for combustion of a fuel
04/27/2008CA2608479A1 Gas turbine floating collar arrangement
04/24/2008WO2008047825A1 Gas turbine combustor
04/24/2008US20080092513 Method and Device for the Combustion of Hydrogen in a Premix Burner
04/24/2008DE102006048842A1 Combustion chamber for gas turbine, has flame tube, which develops combustion zone and post-primary combustion zone in flow direction of fuel-air-mixture
04/24/2008CA2667093A1 Premixer for gas and fuel for use in combination with energy release/conversion device
04/24/2008CA2605220A1 Gas turbine internal manifold mounting arrangement
04/23/2008EP1483536B1 Gas turbine
04/23/2008CN201050803Y Double fuel jet-nozzle for combustion turbine
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