Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
02/2013
02/13/2013EP2557282A1 Acoustic Helmholtz dampening device for use in gas turbine engine
02/13/2013CN102933904A Damping device for damping pressure oscillations within a combustion chamber of a turbine
02/13/2013CN102933819A Lean-fuel intake gas turbine
02/13/2013CN102927592A Turbomachine combustor assembly
02/13/2013CN102927591A System and method for monitoring combustor
02/13/2013CN102159890B Burner arrangement for liquid fuels and method for producing burner arrangement
02/10/2013CA2784660A1 Acoustic dampening device for use in gas turbine engine
02/07/2013US20130032643 Combustor leaf seal arrangement
02/07/2013US20130031909 Combustor heat shield with integrated louver and method of manufacturing the same
02/07/2013US20130031908 Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
02/07/2013US20130031906 Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
02/07/2013US20130031905 Fuel nozzle
02/07/2013US20130031904 Combustion chamber
02/07/2013DE102011052413A1 Brennkammervorrichtung oder Schubkammervorrichtung Combustion chamber device or thrust chamber device
02/06/2013EP2554911A2 Fuel Nozzle
02/06/2013EP2554910A2 Methods relating to integrating late lean injection into combustion turbine engines
02/06/2013EP2554909A2 Fuel injector
02/06/2013EP2554908A2 Combustor leaf seal arrangement
02/06/2013EP2554907A1 Combustor and gas turbine
02/06/2013EP2554906A2 Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
02/06/2013EP2554905A1 Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
02/06/2013EP2554904A2 Combustion chamber device or thrust chamber device
02/06/2013EP2554903A2 A combustion chamber
02/06/2013EP2554823A1 Fuel supply device of gas turbine engine
02/06/2013EP2554792A1 Double-jet film cooling structure
02/06/2013EP2553341A1 A combustion apparatus and gas turbine engine
02/06/2013EP2553340A1 Turbomachine combustion chamber having a centrifugal compressor with no deflector
02/06/2013CN202719635U Multilayer plate structure and combustion chamber and turbine blade and aero-engine
02/06/2013CN202719634U Flame tube wall in combustion chamber
02/06/2013CN102913953A Methods relating to integrating late lean injection into combustion turbine engines
02/06/2013CN102913952A Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
02/06/2013CN102913951A 燃料喷嘴 Fuel nozzle
02/06/2013CN102913950A Sub-area premixing combusting method for reducing gas turbine engine pollutant emission
02/06/2013CN102913625A Combustor leaf seal arrangement
02/06/2013CN101983305B 燃烧器 Burner
02/06/2013CN101981378B Passage in a burner
02/06/2013CN101842636B A combustor for a gas-turbine engine
02/06/2013CN101636619B Fuel-air premixing arrangement structure ,burner and method for operating the burner
02/06/2013CN101545640B Combustion cap floating collar using E-seal
02/06/2013CN101377304B System and method for mixing fuel and air in gas turbine
02/05/2013US8365534 Gas turbine combustor having a fuel nozzle for flame anchoring
02/05/2013CA2539948C High temperature seal
02/01/2013DE202012104984U1 Hochfeste keramische Leichtbaustrukturen High-strength ceramic lightweight structures
01/2013
01/31/2013US20130029236 Device for Providing Hot Exhaust Gases
01/31/2013US20130025293 Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustor
01/31/2013US20130025288 Microcircuit cooling for gas turbine engine combustor
01/31/2013US20130025287 Distributed cooling for gas turbine engine combustor
01/31/2013US20130025284 Premixing apparatus for gas turbine system
01/31/2013US20130025283 Sector nozzle mounting systems
01/31/2013US20130025253 Reduction of co and o2 emissions in oxyfuel hydrocarbon combustion systems using oh radical formation with hydrogen fuel staging and diluent addition
01/30/2013EP2551599A2 Reduction of CO and O2 emissions in oxyfuel hydrocarbon combustion systems using OH radical formation with hydrogen fuel staging and diluent addition
01/30/2013EP2551598A2 Combustor portion for a turbomachine and method of operatig a turbomachine
01/30/2013EP2551597A2 Sector nozzle mounting systems
01/30/2013EP2551596A2 Combustor, burner, and gas turbine
01/30/2013EP2551595A2 Premixing apparatus for gas turbine system
01/30/2013EP2551594A2 Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustor
01/30/2013EP2551593A2 Distributed cooling for gas turbine engine combustor
01/30/2013EP2551592A2 Microcircuit cooling for gas turbine engine combustor
01/30/2013EP2551491A2 System for conditioning air flow into a multi-nozzle assembly
01/30/2013CN202709181U Flame tube of short-ring reflow combustion chamber
01/30/2013CN202709180U Double-oil-way fuel injection device
01/30/2013CN202709179U Air suction hopper structure
01/30/2013CN102906500A Swirl blade, burner and gas turbine
01/30/2013CN102901127A Premixing pre-evaporation low-pollution combustion chamber for main-combustion-stage double-layer pre-film three-cyclone
01/30/2013CN102901126A Combustion organizational structure
01/30/2013CN102901125A Combustor, burner, and gas turbine
01/30/2013CN102901124A Combustor portion for a turbomachine and method of operating a turbomachine
01/30/2013CN102901123A System for conditioning air flow into a multi-nozzle assembly
01/30/2013CN102901122A Premixing apparatus for gas turbine system
01/30/2013CN102900538A Double-working-medium combined cycle turbine annular combustion phase change chamber
01/30/2013CN102900471A Efficient low-resistant structural or efficient energy-gathered structural or efficient engine
01/29/2013CA2717487C Method for operating a premix burner, and a premix burner for carrying out the method
01/29/2013CA2690216C Turbine wash port for a gas turbine engine
01/29/2013CA2590056C Gas turbine fuel nozzle manufacturing
01/29/2013CA2525189C Gas turbine engine fuel injector
01/24/2013US20130024087 Abnormal combustion detection and characterization method for internal-combustion engines
01/24/2013US20130019603 Insert for gas turbine engine combustor
01/24/2013US20130019584 Burner, gas turbine combustor, burner cooling method, and burner modifying method
01/23/2013EP2549189A2 System for damping oscillations in a turbine combustor
01/23/2013EP2549188A2 Insert for a gas turbine engine combustor
01/23/2013EP2549186A2 Multi-stage amplification vortex mixture for gas turbine engine combustor
01/23/2013EP2549183A1 A fuel injector
01/23/2013EP2547959A1 Swirled fuel injection
01/23/2013CN102889619A Sealing device of multi-stranded cable aiming at perforation lead-out
01/23/2013CN102889618A Annular combustion chamber based on Venturi pre-mixing bispin nozzle
01/23/2013CN102889617A Premixing and pre-evaporation combustor for main combustion stage using radial film formation
01/23/2013CN102889616A Multi-point direct spray combustion chamber based on venturi premixing double spiral nozzle
01/23/2013CN102889615A Fuel oil atomizing device
01/23/2013CN102889614A Direct-flow spraying nozzle
01/23/2013CN102889613A System for damping oscillations in a turbine combustor
01/23/2013CN101646841B Eccentric chamfer at inlet of branches in a flow channel
01/22/2013US8356467 Combustion wave ignition for combustors
01/22/2013CA2674070C Gas turbine combustor repair using a make-up ring
01/22/2013CA2665353C Multi-channel fuel manifold
01/22/2013CA2513049C Gas turbine floating collar
01/17/2013WO2013009211A1 Fuel cooled combustor
01/17/2013WO2010008633A3 Mixer for combustor and method of manufacturing
01/16/2013EP2546575A2 Systems and methods for bulk temperature variation reduction of a gas turbine through can-to-can fuel temperature modulation
01/16/2013EP2546574A2 Ceramic matrix composite combustor vane ring assembly
01/16/2013EP2546464A2 Coated gas turbine components
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