| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 01/08/2015 | US20150007573 Annular-combustion-chamber bypass |
| 01/08/2015 | US20150007571 Gas turbine combustor |
| 01/08/2015 | US20150007547 Combustion device |
| 01/07/2015 | EP2821706A1 Combustor and gas turbine |
| 01/07/2015 | EP2821627A1 Afterburner and aircraft engine |
| 01/07/2015 | CN204084467U 燃气轮机燃烧室轴向两级方向相反的旋流喷嘴 Instead of a two-stage gas turbine combustor axial direction of the swirl nozzle |
| 01/07/2015 | CN204084466U 一种燃气轮机燃烧室轴向两级旋流喷嘴 A gas turbine combustor two axial swirl nozzle |
| 01/07/2015 | CN204084465U 燃气轮机燃烧室喷嘴结构 Gas turbine combustor nozzle structure |
| 01/07/2015 | CN204084464U 燃气轮机双燃料喷嘴结构 Dual fuel gas turbine nozzle structure |
| 01/07/2015 | CN204084463U 一种带冷却装置的燃烧室头部结构 Combustor head structure with a cooling device |
| 01/07/2015 | CN204084462U 一种燃气轮机燃烧室火焰筒 A gas turbine combustor liner |
| 01/07/2015 | CN204084461U 一种具有冷却功能的燃气轮机燃烧室的导流衬套 Having a cooling gas turbine combustor liner diversion |
| 01/07/2015 | CN204084460U 一种燃气轮机燃烧室头部配气冷却结构 A gas turbine combustor cooling structure of the gas distribution head |
| 01/07/2015 | CN204084459U 一种燃气轮机燃烧室的导流衬套 A gas turbine combustor liner diversion |
| 01/07/2015 | CN104266228A 燃气轮机燃烧室轴向两级方向相反的旋流喷嘴 Instead of a two-stage gas turbine combustor axial direction of the swirl nozzle |
| 01/07/2015 | CN104266227A 一种燃气轮机燃烧室轴向两级旋流喷嘴 A gas turbine combustor two axial swirl nozzle |
| 01/07/2015 | CN104266226A 一种贫燃料多孔喷射燃烧系统 One kind of porous lean fuel injection combustion system |
| 01/07/2015 | CN102859282B 用于燃烧器的旋流生成器 The swirling flow generator for the burner |
| 01/06/2015 | US8925331 Annular combustion chamber of a turbomachine |
| 01/06/2015 | US8925326 System and method for turbine combustor mounting assembly |
| 01/06/2015 | US8925325 Recirculating product injection nozzle |
| 01/06/2015 | US8925324 Turbomachine including a mixing tube element having a vortex generator |
| 01/06/2015 | CA2608479C Gas turbine floating collar arrangement |
| 01/01/2015 | US20150000299 System and method for a fuel nozzle |
| 01/01/2015 | US20150000291 Gas turbine engine combustor heat exchanger |
| 01/01/2015 | US20150000288 Abradable liner for a gas turbine engine |
| 01/01/2015 | US20150000287 Combustor assembly including a transition inlet cone in a gas turbine engine |
| 01/01/2015 | US20150000286 System for supporting a bundled tube fuel injector within a combustor |
| 01/01/2015 | US20150000284 Cap assembly for a bundled tube fuel injector |
| 01/01/2015 | US20150000283 Combustor apparatus in a gas turbine engine |
| 01/01/2015 | US20150000282 Annular helmholtz damper |
| 01/01/2015 | US20150000251 System, Method and Apparatus for Lean Combustion with Plasma from an Electrical Arc |
| 12/31/2014 | CN204063129U 扩散型燃烧器燃料喷嘴 Diffusion burner fuel nozzle |
| 12/31/2014 | CN204063128U 微混合器系统 Micromixer system |
| 12/31/2014 | CN204063127U 燃气涡轮机及用于控制压缩工作流体流速的系统 Gas turbine and means for controlling the flow rate of the compressed working fluid system |
| 12/31/2014 | CN204063126U 用于管水平气流调节的系统 For horizontal damper tube system |
| 12/31/2014 | CN102901125B 燃烧器、燃烧嘴及燃气轮机 Burner, and a gas turbine burner |
| 12/31/2014 | CN102575844B 用于涡轮发动机的燃烧室的多点喷射器 Turbine engine combustor for multi-point injectors |
| 12/31/2014 | CN102165263B 燃烧器及具备该燃烧器的燃气轮机 Burner and a gas turbine combustor comprising the |
| 12/31/2014 | CN101709660B 用于加热和热回收系统的低btu燃料流量比导管燃烧器 Low btu fuel for heating and heat recovery system flow ratio of duct burners |
| 12/30/2014 | US8919673 Apparatus and method for a fuel nozzle |
| 12/30/2014 | US8919137 Assemblies and apparatus related to integrating late lean injection into combustion turbine engines |
| 12/30/2014 | US8919132 Method of operating a gas turbine engine |
| 12/30/2014 | US8919127 System and method for flow control in gas turbine engine |
| 12/30/2014 | US8919126 Cooled pilot fuel lance |
| 12/30/2014 | US8919125 Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines |
| 12/30/2014 | US8919095 Injection element |
| 12/30/2014 | CA2572852C Multimode injection apparatus for combustion chambers, namely a turbojet engine |
| 12/25/2014 | US20140373548 Combustion chamber of a combustor for a gas turbine |
| 12/24/2014 | CN204042975U 一种旋转爆震燃烧室 A rotating detonation combustor |
| 12/24/2014 | CN204042974U 燃烧器的燃烧筒 Combustion in a burner tube |
| 12/24/2014 | CN104246373A 燃气涡轮机 Gas turbine |
| 12/24/2014 | CN104246372A 燃烧器 Burner |
| 12/24/2014 | CN104246371A 涡轮机燃烧器组装件 Turbine combustor assembly |
| 12/24/2014 | CN104235879A 燃气轮机燃烧室过渡段结构 Gas turbine combustor transition section structure |
| 12/24/2014 | CN103343983B 基于强磁场稳定电弧的超声速稳定燃烧方法 Based on the strong magnetic field stable arc stable supersonic combustion method |
| 12/24/2014 | CN102980206B 火焰稳定器及包含该火焰稳定器的发动机燃烧室 Flame stabilizer and the engine combustion chamber comprising the flame holder |
| 12/24/2014 | CN102944027B 一种斯特林发动机用燃气燃烧室 Stirling engine with one kind of gas chamber |
| 12/24/2014 | CN102575843B 用于涡轮发动机燃烧室的多点喷油装置 Multi-point fuel injection system for a turbine engine combustor |
| 12/23/2014 | US8915089 System and method for detecting and controlling flashback and flame holding within a combustor |
| 12/23/2014 | US8915087 Methods and systems for transferring heat from a transition nozzle |
| 12/23/2014 | US8915059 Fuel gas pressure control system and method for reducing gas turbine fuel supply pressure requirements |
| 12/18/2014 | US20140367925 Hot gas seal |
| 12/18/2014 | US20140367495 Fuel injection nozzle and method of manufacturing the same |
| 12/18/2014 | US20140367494 Additively manufactured nozzle tip for fuel injector |
| 12/18/2014 | US20140366553 Combustion chamber for a gas turbine and gas turbine and a method of use |
| 12/18/2014 | US20140366551 Continuous ignition |
| 12/18/2014 | US20140366544 Combustor exit duct for gas turbine engines |
| 12/18/2014 | US20140366543 Combustion equipment for use in a gas turbine engine |
| 12/18/2014 | US20140366542 Fuel Air Premix Chamber For a Gas Turbine Engine |
| 12/17/2014 | CN204026742U 用于将燃料供应到燃烧器的系统 Is used to supply fuel to the burner system |
| 12/17/2014 | CN204026741U 火焰保持构件及燃烧器 Holding member and the burner flame |
| 12/17/2014 | CN104214800A 燃气轮机燃烧室轴向进气喷嘴 Gas turbine combustor axial inlet nozzle |
| 12/17/2014 | CN104214799A 燃气轮机燃烧室轴向旋流喷嘴 Axial swirl gas turbine combustor nozzle |
| 12/17/2014 | CN104213986A 用于将燃料空气混合物加入燃烧室的喷射器 For the combustion of the fuel-air mixture is added to the ejector |
| 12/17/2014 | CN103175223B 一种气路轴向分级式双燃料喷嘴 One kind of gas path axially graded dual fuel nozzle |
| 12/17/2014 | CN103175222B 一种用于化学回热循环的空气助燃双燃料喷嘴 Air for combustion chemistry regenerative cycle dual fuel nozzle |
| 12/17/2014 | CN103175219B 一种用于化学回热循环燃烧室头部的文氏管装置 Venturi apparatus for chemical regenerative cycle combustion head |
| 12/17/2014 | CN103134079B 一种双油路燃油喷嘴 A dual fuel nozzle oil passage |
| 12/17/2014 | CN102947650B 透平燃烧器 Turbine combustor |
| 12/17/2014 | CN102741615B 用于燃气涡轮衬套的碳化钨插件和方法 Tungsten plug and method for gas turbine liner |
| 12/17/2014 | CN102356276B 热屏元件的装配设备 Heat shield assembly equipment components |
| 12/16/2014 | US8910485 Stoichiometric exhaust gas recirculation combustor with extraction port for cooling air |
| 12/16/2014 | US8910483 Lean premix burner for a gas-turbine engine |
| 12/16/2014 | US8910481 Advanced quench pattern combustor |
| 12/16/2014 | US8910480 Fuel injector with radially inclined vanes |
| 12/11/2014 | US20140361447 Turbomachine fuel-air mixer component including an additively manufactured portion joined to a non-additively manufactured portion and method |
| 12/11/2014 | US20140360203 Rijke type combustion arrangement and method |
| 12/11/2014 | US20140360202 Fuel injector and a combustion chamber |
| 12/11/2014 | US20140360197 Afterburner and aircraft engine |
| 12/11/2014 | US20140360196 Shell and tiled liner arrangement for a combustor |
| 12/11/2014 | US20140360195 Low Calorific Fule Combustor For Gas Turbine |
| 12/11/2014 | US20140360194 Toroidal heat exchanger |
| 12/11/2014 | US20140360193 Support frame and method for assembly of a combustion module of a gas turbine |
| 12/11/2014 | US20140360156 Asymmetric Baseplate Cooling with Alternating Swirl Main Burners |
| 12/10/2014 | CN204006124U 燃气轮机燃烧室火焰筒与过渡段的双层夹式密封连接结构 Double gas turbine combustor liner and transition section connecting clip-seal structure |
| 12/10/2014 | CN204006123U 一种多级低污染燃烧系统及燃烧室 A multi-stage combustion system and combustion chamber cleaner |
| 12/10/2014 | CN204006122U 一种用于燃气轮机燃烧室的联焰管 Union flame tube for a gas turbine combustor |
| 12/10/2014 | CN204006121U 一种大深宽比变截面换热通道 One kind of high aspect ratio variable cross-channel heat exchanger |
| 12/10/2014 | CN204006120U 一种环形燃烧室 A toroidal chamber |