F23R 3 - Continuous combustion chambers using liquid or gaseous fuel

Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
12/2011
12/28/2011	CN1609427B 膜式冷却燃气轮机燃烧器的方法和装置 Film cooling method and a gas turbine combustor apparatus
12/28/2011	CN102301107A 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
12/28/2011	CN101113820B 燃烧器衬垫及其制造方法 Burner pad and manufacturing method thereof
12/27/2011	US8082738 Diffuser arranged between the compressor and the combustion chamber of a gas turbine
12/22/2011	WO2011157548A1 Damping device for damping pressure oscillations within a combustion chamber of a turbine
12/22/2011	WO2011157458A1 Turbine burner
12/22/2011	WO2011157418A1 Gas turbine combustion chamber arrangement of axial type of construction
12/22/2011	WO2011156871A1 Indirectly fired gas turbine assembly
12/22/2011	US20110308254 Turbine Engine Fuel Injector
12/21/2011	EP2397764A1 Turbine burner
12/21/2011	EP2397763A1 Fuel nozzle, burner and gas turbine
12/21/2011	EP2397762A1 Damping device for damping pressure oscillations within a combustion chamber of a turbine
12/21/2011	CN202082953U 一种部分预混预蒸发燃烧室 A partially premixed combustion chamber pre-evaporator
12/21/2011	CN102287854A 补燃式超临界压力气液燃料发生器燃烧室冗余冷却装置 Complement fired supercritical pressure gas and liquid fuel combustion generator redundant cooling device
12/21/2011	CN102287853A 用于燃气轮机NOx排放物控制的稀释剂喷射的备选方法 Alternative gas turbine NOx emission control for diluent injection
12/15/2011	WO2011156078A1 Cooled conduit for conveying combustion gases in a gas turbine engine
12/15/2011	DE102010023816A1 Gasturbinenbrennkammeranordnung Gas turbine combustor assembly
12/14/2011	EP2394027A1 Turbine component having easily removable protective layer, set of turbine components, a turbine and a method for protecting a turbine component
12/14/2011	EP2394025A1 Diffuser/rectifier assembly for a turbine engine
12/14/2011	CN202073642U 涡旋复合式热机 Vortex composite heat engine
12/14/2011	CN102282423A 具有用于主空气和稀释空气的单一环形行入孔的涡轮机燃烧室壁 With a single ring for the main air line into the hole and dilution air turbine combustion chamber wall
12/14/2011	CN101949550B 基于射流等离子体活化的超声速稳定燃烧方法 Based on the supersonic jet plasma activation stable combustion method
12/14/2011	CN101218416B 导引热燃气的机匣元件、轴保护套和燃气轮机装置 Hot gas casing element guide shaft protective sleeve and a gas turbine plant
12/13/2011	US8074452 Nested channel ducts for nozzle construction and the like
12/08/2011	US20110296842 Control of axial thrust by guidance of the air drawn off from a centrifugal compressor
12/08/2011	US20110296840 Gas turbine combustor injection assembly, and combustor fuel mixture feed method
12/07/2011	EP2392858A2 Extruded fluid manifold for gas turbomachine combustor casing
12/07/2011	CN1847674B 安装两个合成物制成部件的方法及完成安装的插入物 Installation methods and compositions made of two parts to complete the installation of the insert
12/07/2011	CN1784574B 截流涡流式燃烧器 Closure vortex burner
12/07/2011	CN102272428A 发动机 Engine
12/07/2011	CN102272427A 发动机 Engine
12/07/2011	CN101743442B 燃气轮机燃烧器 A gas turbine combustor
12/07/2011	CN101566353B 双涡燃烧室 Double vortex combustor
12/01/2011	WO2011149973A1 Tangential combustor with vaneless turbine for use on gas turbine engines
12/01/2011	US20110289898 Combined cycle power plant with flue gas recirculation
11/2011
11/30/2011	EP2390572A2 Hybrid prefilming airblast, prevaporizing, lean-premixing dual-fuel nozzle for gas turbine combustor
11/30/2011	EP2390568A2 Turbomachine fuel nozzle
11/30/2011	CN102265091A 用于燃烧器的燃料喷管 A fuel nozzle for a burner
11/30/2011	CN102261674A 减小压力损失的过渡支承件 Reduce the pressure loss of the transition support member
11/30/2011	CN102261673A 用于燃气轮机燃烧器的混合式双燃料喷嘴 Hybrid dual fuel nozzle for a gas turbine combustor
11/30/2011	CN101029739B 用于燃气轮机的燃烧室及燃气轮机 And a gas turbine combustor for a gas turbine
11/29/2011	US8066509 Method and device for combusting hydrogen in a premix burner
11/29/2011	CA2586548C Testing rig and method for a fuel nozzle assembly
11/24/2011	WO2011104304A3 Injection system for a turbine engine combustion chamber, including air injection means improving the air-fuel mixture
11/23/2011	EP2388525A2 Late lean injection injector
11/23/2011	EP2388524A2 System for cooling turbine combustor transition piece
11/23/2011	EP2388520A1 Lance of a gas turbine burner
11/23/2011	EP1543272B1 Turbine engine fuel nozzle
11/23/2011	CN1828140B One-piece can combustor
11/23/2011	CN102252345A Tangential combustor
11/23/2011	CN101784841B Gas turbine combustor
11/23/2011	CN101382297B Gas turbine combustion chamber with helicoidal air circulation
11/22/2011	CA2599113C Fuel injection valve, combustor using the fuel injection valve, and fuel injection method for the fuel injection valve
11/16/2011	EP2386798A2 Gas turbine engine combustor with CMC heat shield and methods therefor
11/16/2011	CN102242940A Three-stage structured pre-mixing and pre-evaporating low-pollution combustor
11/16/2011	CN102242939A Prefilming three-stage pre-mixing and pre-evaporating low-pollution combustor
11/16/2011	CN102242931A Gas turbine combustor injection assembly, and combustor fuel mixture feed method
11/16/2011	CN101354142B Fuel nozzle component and method
11/15/2011	US8056346 Combustor
11/15/2011	US8056342 Hole pattern for gas turbine combustor
11/15/2011	CA2470928C Turbomachine annular combustion chamber
11/10/2011	US20110271654 Diffuser for gas turbine system
11/10/2011	DE102011018937A1 Verbrennungsvorrichtung für eine Gasturbine A combustion apparatus for a gas turbine
11/10/2011	DE102010019773A1 Magervormischbrenner eines Gasturbinentriebwerks mit Strömungsleitelement Lean premix burner of a gas turbine engine having flow guide
11/10/2011	DE102010019772A1 Magervormischbrenner eines Gasturbinentriebwerks mit einem konzentrischen, ringförmigen Zentralkörper Lean premix burner in a gas turbine engine with a concentric, annular central body
11/10/2011	CA2738312A1 Gas turbine engine combustor with cmc heat shield and methods therefor
11/09/2011	EP2385308A2 Reduced pressure loss transition support
11/09/2011	EP2385307A1 Gas turbine combustor injection assembly, and combustor fuel mixture feed method
11/09/2011	EP2385306A2 Lean pre-mix burner of a gas turbine engine with flow guidance element
11/09/2011	EP2385305A2 Turbomachine injection nozzle assembly
11/09/2011	EP2385304A2 Lean pre-mix burner of a gas turbine engine with a concentric, ring-shaped central body
11/09/2011	EP2385303A1 Combustion Device for a Gas Turbine
11/09/2011	EP2385233A1 Method for the operation of a gas turbine unit based on the combustor wall temperature
11/09/2011	EP2384414A2 Cooled flameholder swirl cup
11/09/2011	EP2384413A1 Acoustic damper
11/09/2011	EP1706594B1 Sliding joint between combustor wall and nozzle platform
11/09/2011	CN202032613U Partial pre-mixing & pre-evaporation combustion chamber
11/09/2011	CN202032612U Partial premixing and pre-evaporating combustion chamber
11/09/2011	CN202032611U Aeroengine flame tube housing structure
11/09/2011	CN102235267A Gas turbine engine modified by using exservice turbofan engine through low-pressure crest truncation
11/09/2011	CN101713550B Flame tube with central cyclone
11/09/2011	CN101278152B Fuel nozzle having swirler-integrated radial fuel jet
11/08/2011	US8052155 High temperature seal and methods of use
11/05/2011	CA2739130A1 Gas turbine combustor injection assembly, and combustor fuel mixture feed method
11/03/2011	WO2011137110A1 Dynamically auto-tuning a gas turbine engine
11/03/2011	WO2011136834A2 Gas turbine engine having dome panel assembly with bifurcated swirler flow
11/03/2011	WO2011134706A1 Burner system and method for damping such a burner system
11/03/2011	US20110265484 Combustion device for a gas turbine
11/03/2011	US20110265481 Dual fuel can combustor with automatic liquid fuel purge
11/02/2011	EP2383518A2 Tangential combustor
11/02/2011	EP2383517A2 Fluid cooled injection nozzle assembly for a gas turbomachine
11/02/2011	EP2383516A2 Pocketed air and fuel mixing tube
11/02/2011	EP2383515A1 Combustion system and method for dampening such a combustion system
11/02/2011	EP2383451A2 Alternate method for diluent injection for gas turbine NOx emissions control
11/02/2011	EP2382377A2 Synthesis gas-based fuel system including admixture of a second fuel, and method for the operation of a synthesis gas-based fuel system
11/02/2011	CN202023635U Reheating vortex combined type heat engine
11/01/2011	US8047001 Media mixing insert for turbine blade in turbine engine
10/2011
10/27/2011	WO2011132426A1 Fuel supply device for gas turbine engine
10/27/2011	US20110259976 Fuel injector purge tip structure
10/27/2011	US20110259015 Tangential Combustor

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