| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 05/07/2014 | EP2726439A2 Pressure casting slip and refractory ceramic produced therefrom for gas turbine units |
| 05/07/2014 | CN203586284U 一种带直流孔的轴向叶片式旋流器 An axial vane swirler holes with DC |
| 05/07/2014 | CN203586283U 一种燃气轮机气体燃料干式低氮燃烧装置 A gas turbine gas fuel dry low NOx combustion system |
| 05/07/2014 | CN103782103A 燃气轮机 Gas turbine |
| 05/07/2014 | CN103782102A 用于燃烧室衬里特别是燃气轮机的燃烧室衬里的陶瓷砖及其制造方法 In particular, the combustor liner and the method for manufacturing ceramic tiles in the combustor liner for a gas turbine |
| 05/07/2014 | CN103776061A 用于减少燃烧室脉动的消声器组件 A combustion chamber for reducing the pulsation muffler assembly |
| 05/07/2014 | CN103776060A 再热喷燃器布置 Reheat burner arrangement |
| 05/07/2014 | CN103776059A 用于筒式燃烧器的喷燃器 Burner for barrel burner |
| 05/07/2014 | CN103776058A 喷燃器 Burner |
| 05/07/2014 | CN103776057A 燃烧器过渡件 Combustor transition piece |
| 05/07/2014 | CN103775213A 燃烧器过渡件 Combustor transition piece |
| 05/07/2014 | CN102301107B 燃烧器结构部件的制造方法、燃烧器结构部件、燃气轮机用燃烧器及燃气轮机 The method of manufacturing the structural component burner, the burner structural components, the gas turbine and a gas turbine burner |
| 05/07/2014 | CN102177326B 控制燃烧产物的方法与装置 Control method and apparatus for combustion products |
| 05/01/2014 | WO2014063835A1 Sequential combustion with dilution gas mixer |
| 05/01/2014 | WO2013173162A3 Multistaged lean prevaporizing premixing fuel injector |
| 05/01/2014 | US20140116066 Combustor cap assembly |
| 05/01/2014 | US20140116059 Hot gas segment arrangement |
| 05/01/2014 | US20140116058 Assemblies and apparatus related to combustor cooling in turbine engines |
| 05/01/2014 | US20140116057 Push-lock pin |
| 05/01/2014 | US20140116056 Gas turbine diffuser with flow separator |
| 05/01/2014 | US20140116055 Combustion system |
| 05/01/2014 | US20140116054 Radial flow fuel nozzle for a combustor of a gas turbine |
| 05/01/2014 | US20140116053 Fuel injection assemblies in combustion turbine engines |
| 04/30/2014 | EP2725303A2 Reheat burner arrangement |
| 04/30/2014 | EP2725302A1 Reheat burner arrangement |
| 04/30/2014 | EP2725301A1 Burner for a can combustor |
| 04/30/2014 | EP2725300A1 Damper arrangement for reducing combustion-chamber pulsations |
| 04/30/2014 | EP2725296A1 Systems and methods for adverse combustion avoidance and correction |
| 04/30/2014 | CN103765108A Combustion chamber wall |
| 04/30/2014 | CN103765107A Combustion chamber for a gas turbine plant |
| 04/30/2014 | CN103765105A Combustion chamber for a gas turbine plant |
| 04/30/2014 | CN103765099A Staged cooling flow nozzle valve |
| 04/30/2014 | CN103764974A Combustor tail pipe, gas turbine with tail pipe, and method for manufacturing tail pipe |
| 04/30/2014 | CN103764955A Device for installing and removing a component on or in a stationary gas turbine and method for installing and removing a component of a stationary gas turbine |
| 04/30/2014 | CN103759293A Heat shield element of a heat shield |
| 04/30/2014 | CA2830925A1 Hot gas segment arrangement |
| 04/29/2014 | US8707707 Late lean injection fuel staging configurations |
| 04/29/2014 | US8707671 Fuel control method and fuel control apparatus for gas turbine and gas turbine |
| 04/25/2014 | CA2830681A1 Reheat burner arrangement |
| 04/24/2014 | WO2014060758A1 Heat engine |
| 04/24/2014 | WO2013175126A3 Turbomachine combustion chamber shell ring |
| 04/24/2014 | WO2013153013A3 Burner |
| 04/24/2014 | US20140109595 Annular combustion chamber of a turbomachine |
| 04/24/2014 | US20140109588 Burner for a can combustor |
| 04/24/2014 | US20140109587 System and method for reducing modal coupling of combustion dynamics |
| 04/24/2014 | US20140109584 Modulating electric liquid metering valve with flow sensing |
| 04/24/2014 | US20140109583 Burner |
| 04/24/2014 | US20140109582 Self-stabilized micromixer |
| 04/24/2014 | US20140109581 Reverse-flow annular combustor for reduced emissions |
| 04/24/2014 | US20140109579 Combustor transition |
| 04/24/2014 | US20140109578 Combustor transition |
| 04/24/2014 | US20140109577 Ducting arrangement for cooling a gas turbine structure |
| 04/24/2014 | DE102012015452A1 Gas turbine combustion chamber wall for gas turbine engine, has mixed air openings formed by tubular air guide elements, which are fastened at wall and penetrate shingles arranged at inner side of wall |
| 04/24/2014 | CA2830690A1 Combustor transition |
| 04/24/2014 | CA2830683A1 Combustor transition |
| 04/24/2014 | CA2829989A1 Damper arrangement for reducing combustion-chamber pulsation |
| 04/23/2014 | EP2722593A2 Reverse-flow annular combustor for reduced emissions |
| 04/23/2014 | EP2722592A1 Multiple cone gas turbine burner |
| 04/23/2014 | EP2722591A1 Multiple cone gas turbine burner |
| 04/23/2014 | EP2721347A1 Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same |
| 04/23/2014 | EP2721273A1 Combustion systems and combustion system components for rotary ramjet engines |
| 04/23/2014 | CN103748338A Split control unit |
| 04/23/2014 | CN101889133B Gas turbine controlling method, and gas turbine power generating apparatus |
| 04/23/2014 | CA2830031A1 Burner for a can combustor |
| 04/22/2014 | US8701418 Late lean injection for fuel flexibility |
| 04/22/2014 | US8701383 Late lean injection system configuration |
| 04/22/2014 | US8701382 Late lean injection with expanded fuel flexibility |
| 04/22/2014 | CA2829613A1 Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method |
| 04/17/2014 | WO2014029512A3 Sequential combustion with dilution gas mixer |
| 04/16/2014 | EP2719953A2 Multipoint injectors with auxiliary stage |
| 04/16/2014 | EP2719952A2 Fuel nozzle and method of assembling the same |
| 04/16/2014 | EP2719951A1 Air management arrangement for a late lean injection combustor system and method of routing an airflow |
| 04/16/2014 | EP2719950A2 System and method for separating fluids |
| 04/16/2014 | EP2718627A2 Annular combustion chamber of a turbomachine |
| 04/16/2014 | CN103732992A Combustion arrangement and turbine comprising a damping facility |
| 04/16/2014 | CN103732886A Member-assembling device for rotary machine |
| 04/16/2014 | CN103732560A Pressure casting slip and refractory ceramic produced therefrom for gas turbine units |
| 04/16/2014 | CN103727562A Fuel supporting plate for improving non-premixed combustion of RBCC (rocket-based combined cycle) bimodal combustion chamber |
| 04/16/2014 | CN103727561A System and method for separating fluids |
| 04/16/2014 | CN103727534A Air management arrangement for a late lean injection combustor system and method of routing an airflow |
| 04/15/2014 | US8695989 Hot gas seal |
| 04/15/2014 | US8695322 Thermally decoupled can-annular transition piece |
| 04/15/2014 | CA2830049A1 Combustor skin assembly for gas turbine engine |
| 04/15/2014 | CA2567533C Externally fueled trapped vortex cavity augmentor |
| 04/15/2014 | CA2566802C Methods and apparatus for injecting fluids into turbine engines |
| 04/10/2014 | WO2014055437A1 Method of operating a multi-stage flamesheet combustor |
| 04/10/2014 | WO2014055435A2 Variable flow divider mechanism for a multi-stage combustor |
| 04/10/2014 | WO2014055427A2 Flamesheet combustor dome |
| 04/10/2014 | WO2014055425A1 Variable length combustor dome extension for improved operability |
| 04/10/2014 | WO2014055151A2 Method of casting parts using heat reservoir, gating used by such method, and casting made thereby |
| 04/10/2014 | WO2014055116A1 Combustor with grommet having projecting lip |
| 04/10/2014 | WO2014053760A1 Annular chamber end wall for an aircraft turbomachine combustion chamber, provided with perforations that allow for cooling by gyratory flow |
| 04/10/2014 | WO2014053730A2 Two-circuit injector for a turbine engine combustion chamber |
| 04/10/2014 | WO2014053728A1 Combustion chamber comprising a flame tube fixed by means of three centring members |
| 04/10/2014 | WO2014053724A1 Turbine engine combustion assembly with a variable air supply |
| 04/10/2014 | WO2013028164A8 Tangential annular combustor with premixed fuel and air for use on gas turbine engines |
| 04/10/2014 | US20140099591 Duct burner of hrsg with liner film cooling |
| 04/10/2014 | US20140096530 Air management arrangement for a late lean injection combustor system and method of routing an airflow |
| 04/10/2014 | US20140096529 System and method for fuel and steam injection within a combustor |
| 04/10/2014 | US20140096527 Gas turbine engine combustor liner |