Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
10/2013
10/17/2013US20130269359 Combustor flow sleeve with supplemental air supply
10/17/2013US20130269354 Substrate with Shaped Cooling Holes and Methods of Manufacture
10/17/2013US20130269353 Combustion system for a gas turbine comprising a resonator
10/17/2013US20130269352 Gas-turbine burner
10/17/2013US20130269350 Turbine combustor system having aerodynamic feed cap
10/16/2013EP2650612A1 Burner
10/16/2013CN103354890A Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector
10/15/2013US8555647 Methods and apparatus for providing a sacrificial shield for a fuel injector
10/10/2013WO2013151875A1 Combustor having a beveled grommet
10/10/2013WO2013151162A1 Gas turbine combustor
10/10/2013WO2013106119A3 Mounting apparatus for a trailing edge box of a gas turbine augmentor
10/10/2013WO2013083348A3 Combustion chamber for a gas turbine and gas turbine as well as a method
10/10/2013US20130266902 Low emissions combustion apparatus and method
10/10/2013US20130263605 Diffusion Combustor Fuel Nozzle
10/09/2013EP2647912A2 System and method for supporting fuel nozzles inside a combustor
10/09/2013EP2647911A2 Combustor and method for supplying fuel to a combustor
10/09/2013EP2647910A2 Diffusion combustor fuel nozzle
10/09/2013EP2647799A2 Combustor with non-circular head end
10/09/2013CN103348188A Low calorific fuel combustor for gas turbine
10/09/2013CN103343985A Double-pre-film pneumatic nebulization low pollution combustor head structure
10/09/2013CN103343984A Combustor for combustion test with biomass replacing fuel oil
10/09/2013CN103343983A Supersonic-speed stable combustion method based on strong magnetic field stable electric arc
10/09/2013CN102506446B Fuel and air mixing device for low-pollution burning chamber of gas turbine
10/08/2013US8550060 Glow plug heater control
10/08/2013US8549860 Method for combusting hydrogen-rich, gaseous fuels in a burner, and burner for performing said method
10/08/2013CA2517080C Adjusting airflow in turbine component by depositing overlay metallic coating
10/04/2013WO2012133774A1 Nozzle, gas turbine combustor and gas turbine
10/03/2013WO2013147633A1 Turbomachine combustor assembly
10/03/2013WO2013147632A1 Bi-directional end cover with extraction capability for gas turbine combustor
10/03/2013WO2013144070A1 Combustion chamber seal segments equipped with damping devices
10/03/2013WO2013144048A1 Gas turbine combustor
10/03/2013WO2013143975A1 Gas turbine power plant with non-homogeneous input gas
10/03/2013WO2013143627A1 An improved hole arrangement of liners of a combustion chamber of a gas turbine engine with low combustion dynamics and emissions
10/03/2013US20130255269 Combustor having a beveled grommet
10/03/2013US20130255266 Transition Nozzle Combustion System
10/03/2013US20130255265 Combustors with quench inserts
10/03/2013US20130255263 Air blocker ring assembly with radial retention
10/03/2013US20130255262 Combustor with Non-Circular Head End
10/03/2013US20130255261 Swirler for combustion chambers
10/02/2013EP2645000A2 Swirler for combustion chambers
10/02/2013EP2644999A1 Gas turbine assembly with fluidic injector
10/02/2013EP2644998A2 System and method of improving emission performance of a gas turbine
10/02/2013EP2644997A1 Mixing arrangement for mixing fuel with a stream of oxygen containing gas
10/02/2013EP2644996A2 Combustors with quench inserts
10/02/2013EP2644995A1 An improved hole arrangement of liners of a combustion chamber of a gas turbine engine with low combustion dynamics and emissions
10/02/2013CN103335333A Single-oil passage pre-diaphragm type staggered plate primary combustion stage premixing and pre-vaporizing low-pollution combustor
10/01/2013US8545215 Late lean injection injector
09/2013
09/27/2013CA2806951A1 Passive equilization flow divider valve
09/26/2013WO2013139914A1 Combustion device
09/26/2013WO2013139813A1 Annular helmholtz damper
09/26/2013US20130247576 Apparatus, system and method for observing combustor flames in a gas turbine engine
09/26/2013DE112011103736T5 Gasturbinenbrennkammer mit ultraniedrigen Emissionen Gas turbine combustor with ultra low emissions
09/26/2013DE102012204777A1 Method for manufacture of lining element for combustion chamber of aircraft engine, involves attaching old attachment unit to connection region of base portion by rotation friction welding
09/25/2013EP2642208A2 Systems and methods for dampening combustor dynamics in a micromixer
09/25/2013EP2642207A2 Micromixer combustion head end assembly
09/25/2013EP2642206A2 Systems and methods for preventing flash back in a combustor assembly
09/25/2013EP2642204A1 Simultaneous broadband damping at multiple locations in a combustion chamber
09/25/2013EP2642203A1 Annular Helmholtz damper
09/25/2013EP2642098A1 Gas turbine power plant with non-homogeneous input gas
09/25/2013CN103328149A Method for perforating a wall of a combustion chamber
09/25/2013CN103322593A Systems and methods for dampening combustor dynamics in micromixer
09/25/2013CN103322592A Micromixer combustion head end assembly
09/25/2013CN102272427B 发动机 Engine
09/25/2013CN101818908B Apparatus for fuel injection in a turbine engine
09/24/2013US8540508 Method for the combustion of a fluid fuel, and burner, especially of a gas turbine, for carrying out said method
09/24/2013US8539773 Premixed direct injection nozzle for highly reactive fuels
09/24/2013CA2603410C Fuel conveying member with heat pipe
09/23/2013CA2810028A1 Combustor heat shield
09/23/2013CA2809801A1 Fabricated heat shield
09/19/2013WO2013138050A1 Fuel air premixer for gas turbine engine
09/19/2013WO2013135702A2 Heat-shield element for a compressor-air bypass around the combustion chamber
09/19/2013WO2013135324A1 Gas turbine combustion system and method of flame stabilization in such a system
09/19/2013US20130239585 Tangential flow duct with full annular exit component
09/19/2013US20130239575 System for supplying a working fluid to a combustor
09/19/2013DE102012204162A1 Ringbrennkammer-Bypass Annular combustor bypass
09/19/2013DE102012204103A1 Hitzeschildelement für einen Verdichterluftbypass um die Brennkammer Heat shield element for a compressor air bypass around the combustion chamber
09/19/2013DE102012204022A1 Gasturbine und Verfahren zu deren Betrieb Gas turbine and method for its operation
09/18/2013EP2639510A2 System for enhancing mixing in a multi-tube fuel nozzle
09/18/2013EP2639509A2 Combustor and method of reducing thermal stresses in a combustor
09/18/2013EP2639508A2 System for supplying a working fluid to a combustor
09/18/2013EP2639507A2 System for supplying a working fluid to a combustor
09/18/2013EP2639505A1 Gas Turbine Combustion System and Method of Flame Stabilization in such a System
09/18/2013CN103307636A System for supplying a working fluid to a combustor
09/18/2013CN103307635A System for supplying a working fluid to a combustor
09/18/2013CN103307634A Combustor and method of reducing thermal stresses in the combustor
09/18/2013CN103307633A A fuel nozzle and a combustor for a gas turbine
09/18/2013CN103307632A Method of operating a combustor from a liquid fuel to a gas fuel operation
09/18/2013CN103307631A System for enhancing mixing in a multi-tube fuel nozzle
09/17/2013CA2604636C Internal fuel manifold with airblast nozzles
09/17/2013CA2548905C Assembly of a turbine engine annular combustion chamber
09/12/2013WO2012057908A3 Substrate with shaped cooling holes and methods of manufacture
09/12/2013US20130232988 Burner for a gas combustor and a method of operating the burner thereof
09/12/2013US20130232987 Gas turbine fuel injector with insulating air shroud
09/12/2013US20130232986 Combustor and method for reducing thermal stresses in a combustor
09/12/2013US20130232980 System for supplying a working fluid to a combustor
09/12/2013US20130232979 System for enhancing mixing in a multi-tube fuel nozzle
09/12/2013US20130232978 Fuel air premixer for gas turbine engine
09/12/2013US20130232977 Fuel nozzle and a combustor for a gas turbine
09/12/2013US20130232940 Gradual oxidation below flameout temperature
09/11/2013EP2636953A2 Method of operating a combustor from a liquid fuel to a gas fuel operation
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