Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
11/2012
11/14/2012EP2522912A1 Flow straightener and mixer
11/14/2012EP2522911A1 Lobed swirler
11/14/2012EP2522910A1 Combustor Casing For Combustion Dynamics Mitigation
11/14/2012EP2522909A1 Burner and method for regulating a gas turbine with such a burner
11/14/2012EP2522908A1 Control method for controlling the pilot gas supply to at least one burner assembly of a gas turbine plant and gas turbine plant
11/14/2012EP2522907A1 Heat shield assembly
11/14/2012CN102782412A Device for providing hot exhaust gases
11/14/2012CN102782411A Injection system for a turbine engine combustion chamber, including air injection means improving the air-fuel mixture
11/14/2012CN102782410A Turbine engine combustion chamber
11/14/2012CN102777935A Burner and method for regulating a gas turbine with such a burner
11/14/2012CN102777934A Standing-vortex soft combustion chamber
11/14/2012CN102777933A Combustor casing for combustion dynamics mitigation
11/14/2012CN102777932A A combustor nozzle and method for supplying fuel to a combustor
11/14/2012CN102777931A Fuel injector and support plate
11/14/2012CN102777930A Bi-directional fuel injection method
11/14/2012CN102777929A Gas turbine engine combustor
11/14/2012CN101573510B Component with diagonally extending recesses in the surface and method for operating a turbine
11/13/2012CA2647764C Duplex turbine nozzle
11/13/2012CA2608042C Method and device for regulating the operating line of a gas turbine combustion chamber
11/08/2012WO2012150139A1 Cooled pilot fuel lance
11/08/2012US20120279223 Fuel Injector and Support Plate
11/07/2012EP2520865A2 Gas turbine engine combustor
11/07/2012EP2520864A2 Fuel injector and support plate
11/07/2012EP2520863A1 Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting said method
11/07/2012EP2520858A1 Fuel cooled pilot fuel lance for a gas turbine
11/07/2012EP2520857A1 A Combustor Nozzle And Method For Supplying Fuel To A Combustor
11/06/2012CA2597592C Gas turbine combustor and fuel manifold mounting arrangement
11/01/2012WO2012148675A1 A method of forming a multi-panel outer wall of a component for use in a gas turbine engine
11/01/2012WO2012145836A1 Apparatus and method for controlling a pressure gain combustor
11/01/2012US20120272662 Head part of an annular combustion chamber
11/01/2012US20120272661 Head part of an annular combustion chamber
11/01/2012US20120272659 Reheat burner injection system
11/01/2012US20120272653 Internal combustion engine hot gas path component with powder metallurgy structure
11/01/2012US20120272652 head part of an annular combustion chamber
11/01/2012CA2834285A1 Apparatus and method for controlling a pressure gain combustor
10/2012
10/31/2012EP2518408A2 A head part of an annular combustion chamber
10/31/2012EP2518407A2 A head part of an annular combustion chamber
10/31/2012EP2518406A1 Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities
10/31/2012EP2516697A1 Coating systems for protection of substrates exposed to hot and harsh environments and coated articles
10/31/2012EP2516696A1 Methods for coating articles exposed to hot and harsh environments
10/31/2012DE112009004301T5 Gasturbinenkraftstoffinjektor mit geringem Übersprechen Gasturbinenkraftstoffinjektor low-crosstalk
10/31/2012CN102759122A Fuel nozzle and method for operating a combustor
10/31/2012CN102759121A Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities
10/26/2012WO2012143318A1 Combustion chamber housing and gas turbine equipped therewith
10/26/2012WO2012118994A3 Fault tolerant control system for distributed micro-thrusters
10/26/2012WO2011152944A3 Self-regulating fuel staging port for turbine combustor
10/26/2012CA2833464A1 Combustion chamber housing and gas turbine equipped therewith
10/25/2012US20120266602 Aerodynamic Fuel Nozzle
10/24/2012EP2515042A2 Aerodynamic fuel nozzle
10/24/2012EP2515041A2 Fuel Nozzle And Method For Operating A Combustor
10/24/2012EP2513563A2 Tungsten carbide inserts for a gas turbine liner and method
10/24/2012EP2513562A1 Burner for a turbine
10/24/2012EP2513561A2 Guiding of a spark plug into a turbine engine combustion chamber
10/24/2012EP2513560A2 Resonator system for turbine engines
10/24/2012CN202501506U Swirler
10/24/2012CN202501505U 旋流器 Cyclone
10/24/2012CN102748776A Apparatus for combusting fuel within a gas turbine engine
10/24/2012CN102748775A Streamline flame stabilizer with built-in ignition sources
10/23/2012CA2686055C Combustion chamber arrangement for operating a gas turbine
10/20/2012CA2769809A1 Distributed aircraft engine fuel system
10/18/2012US20120260666 Multi-fuel combustion system
10/18/2012US20120260664 Fuel injector arrangement having an igniter
10/18/2012US20120260657 Combustor of a gas turbine
10/18/2012US20120260622 Reheat burner injection system
10/18/2012DE102011007562A1 Brennkammergehäuse und damit ausgerüstete Gasturbine Combustor casing and thus equipped gas turbine
10/17/2012EP2511613A2 Gas turbine combustion chamber with a holder of a seal for an extension
10/17/2012EP2511612A1 Structure for connecting a combustor to a turbine unit, and gas turbine
10/17/2012EP2511607A2 Combustor Nozzle And Method For Supplying Fuel To A Combustor
10/17/2012EP2510284A1 Turbine engine combustion chamber
10/17/2012CN102741615A Tungsten carbide inserts and method
10/17/2012CN102741614A Combustor and gas turbine
10/17/2012CN102734837A Combustor with integrated control valve system
10/17/2012CN102734836A Combustor probe for gas turbine
10/17/2012CN101551122B Sectorised cmc combustor for a gas turbine
10/11/2012US20120255308 Cooled double walled article
10/11/2012US20120255275 Guiding a sparkplug in a turbine engine combustion chamber
10/11/2012DE102011007059A1 Combustion chamber arrangement for partial load operation of gas turbine, has pipes whose walls are formed with apertures, where apertures are arranged such that air flow into chamber is adjusted by rotation of one pipe against another pipe
10/10/2012EP2508803A2 A cooled double walled article
10/10/2012EP2508802A2 Cooling structure, gas turbine combustor and manufacturing method of cooling structure
10/10/2012EP2507557A1 Burner assembly
10/10/2012CN102721084A Combustor crossfire tube having purge holes
10/10/2012CN102721083A Plasma-catalysis gaseous swirl nozzle
10/10/2012CN102721082A Cracking-gas fuel injection device for chemical regenerative cycle
10/10/2012CN102721081A Nozzle for enhancing atomization by plasma
10/10/2012CN102721059A Low-heating-value gas burner and burning technology
10/10/2012CN102226533B High-speed premixed flame furnace for supersonic burning research
10/10/2012CN101487595B Nozzle design for gas turbine combustor
10/10/2012CN101387410B Fuel nozzle and diffusion tip therefor
10/09/2012US8281596 Combustor assembly for a turbomachine
10/09/2012CA2512377C Turbojet with a guard plate to protect burner ring fuel rail, the burner ring and the guard plate
10/04/2012WO2012134816A1 Turbine combustion system liner
10/04/2012WO2012133630A1 Combustor for gas turbine engine and gas turbine
10/04/2012WO2012132898A1 Combustor and gas turbine provided with same
10/04/2012US20120247118 Combustor crossfire tube
10/04/2012US20120247108 Combustor probe for gas turbine
10/04/2012US20120247081 Fuel nozzle to withstand a flameholding incident and a method of forming the same
10/04/2012DE112009000780T5 Brennstoffdüse Fuel nozzle
10/04/2012CA2831281A1 Combustor for gas turbine engine and gas turbine
10/04/2012CA2830729A1 Turbine combustion system liner
10/03/2012EP2505921A2 Combustor crossfire tube having purge holes
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