Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
02/2015
02/05/2015WO2015017427A1 Heat shield with standoffs
02/05/2015WO2015017180A1 Attachment scheme for a ceramic bulkhead panel
02/05/2015WO2015017084A1 Combustor having a nonmetallic body with external electrodes
02/05/2015WO2015017078A1 Transition duct with convection cooled upstream portion and impingement cooled downstream portion
02/05/2015WO2015017002A2 Swirler mount interface for gas turbine engine combustor
02/05/2015US20150033752 Gas turbine combustion system and method of flame stabilization in such a system
02/05/2015US20150033749 System and method of controlling combustion and emissions in gas turbine engine with exhaust gas recirculation
02/05/2015DE112013002290T5 Spülverfahren und Spüleinheit für Gasturbinenbrennkammer Rinsing and flushing unit for gas turbine combustor
02/05/2015DE102013219187B3 Demontagewerkzeug für ein Hitzeschildelement Removal tool for a heat shield element
02/04/2015EP2833071A2 Methods and apparatus for inspecting cooling holes
02/04/2015EP2831508A1 Gas turbine combustor
02/04/2015EP2831507A2 Mixing arrangement for mixing a fuel with a stream of oxygen containing gas
02/04/2015EP2831506A1 An improved hole arrangement of liners of a combustion chamber of a gas turbine engine with low combustion dynamics and emissions
02/04/2015EP2831505A1 Turbomachine combustor assembly
02/04/2015EP2831504A1 Combustion chamber seal segments equipped with damping devices
02/04/2015CN104334972A 燃料喷射装置 Fuel injection device
02/04/2015CN104329689A 一种采用旋流叶片尾缘预膜雾化方式的燃烧室 The trailing edge of the blade using a pre-film atomization swirl combustion chamber
02/04/2015CN104329688A 一种设置在燃气轮机燃烧室喷嘴中的空气旋流装置 Air swirl means disposed in a gas turbine combustor nozzle
02/04/2015CN102686949B 燃烧器与涡轮部的连通结构及燃气轮机 Communication structure and a gas turbine combustor and a turbine section
02/03/2015US8944173 Apparatus and method of extinguishing a fire using a vapor explosion process
02/03/2015US8943835 Gas turbine engine combustor with CMC heat shield and methods therefor
02/03/2015US8943834 Pre-mixing injector with bladeless swirler
02/03/2015US8943832 Fuel nozzle assembly for use in turbine engines and methods of assembling same
02/03/2015US8943831 Lance of a burner
02/03/2015US8943829 Lean premix burner of a gas-turbine engine provided with a flow-guiding element
02/03/2015US8943828 Lean premix burner of a gas-turbine engine provided with a concentric annular central body
02/03/2015US8943826 Engine
02/03/2015US8943825 Helmholtz damper for a combustor of a gas turbine and a method for installing the helmholtz damper
02/03/2015CA2613268C Chamber end, method for producing same, combustion chamber comprising same and turbojet equipped with same
01/2015
01/29/2015WO2015012908A2 Single-fitting, dual-circuit fuel nozzle
01/29/2015WO2015011623A1 Product having a high alumina content
01/29/2015US20150028133 Enhanced Mixing Tube Elements
01/29/2015US20150027128 Heat-shield element for a compressor-air bypass around the combustion chamber
01/29/2015US20150027127 Combustion chamber tile of a gas turbine
01/29/2015US20150027126 System for providing fuel to a combustor
01/29/2015DE112012006144T5 Brennkammeranordnung einer Turbomaschine Combustor assembly of a turbomachine
01/29/2015DE102014110166A1 System zur Belieferung einer Brennkammer mit Brennstoff System for the supply of combustion chamber with fuel
01/29/2015DE102013214487A1 Brennkammerschindel einer Gasturbine A gas turbine combustion chamber tile
01/28/2015EP2829805A1 System for performing staging control of a multi-stage combustor
01/28/2015EP2829804A1 Combustion chamber shingle of a gas turbine and method for their preparation
01/28/2015EP2828581A1 Combustion device
01/28/2015EP2828580A2 Simultaneous broadband damping at multiple locations in a combustion chamber
01/28/2015EP2828579A1 Annular helmholtz damper
01/28/2015EP2828506A1 Gas turbine power plant with non-homogeneous input gas
01/28/2015CN204127994U 燃气轮机燃烧室过渡段结构 Gas turbine combustor transition section structure
01/28/2015CN204127993U 一种锯齿状壁面文氏管流道壁面结构 One kind of jagged wall venturi flow channel wall structure
01/28/2015CN104315542A 一种燃气涡轮发动机用火焰筒及其加工方法 Flame tube and a processing method for a gas turbine engine
01/28/2015CN104315541A 燃烧室值班级喷嘴及使用该喷嘴的方法 Value classes nozzle combustor nozzle method using the same
01/28/2015CN104315540A 燃气轮机燃烧室预混燃料喷嘴 Premixed gas turbine combustor fuel nozzle
01/28/2015CN104315539A 燃气轮机燃烧室喷嘴及使用该喷嘴的方法 Gas turbine combustor nozzle and use the nozzle method
01/28/2015CN102748776B 燃气涡轮发动机内的燃料的燃烧方法和装置 Method and apparatus for combustion within the gas turbine engine fuel
01/28/2015CN102510977B 燃烧设备 Combustion equipment
01/28/2015CN101725985B 多管预混合装置 Multiple pre-mixing device
01/27/2015US8938978 Gas turbine engine combustor with lobed, three dimensional contouring
01/27/2015US8938976 Structural frame for gas turbine combustion cap assembly
01/27/2015US8938974 Method for determining optimum injector inlet geometry
01/27/2015US8938971 Flow straightener and mixer
01/27/2015US8938970 Gas-turbine combustion chamber with starter film for cooling the combustion chamber wall
01/27/2015US8938969 Combustor and rotating machine
01/27/2015US8938968 Burner of a gas turbine
01/27/2015CA2610263C Combustor heat shield with variable cooling
01/27/2015CA2608869C Combustor liner and heat shield assembly
01/27/2015CA2570633C Methods and apparatus for assembling turbine engines
01/26/2015CA2856995A1 Gas turbine facility
01/22/2015WO2015010047A1 Method and apparatus for reducing particulate matter emissions in jet engines by injection of hydrogen produced by on-board electrolysis
01/22/2015WO2015009488A1 Combustion system, apparatus and method
01/22/2015WO2015009396A1 Cooling cover for gas turbine damping resonator
01/22/2015US20150020528 Fuel manifold and fuel injector arrangement for a combustion chamber
01/22/2015US20150020501 An annular combustion chamber in a turbine engine
01/22/2015US20150020498 Cooling cover for gas turbine damping resonator
01/22/2015DE102013213860A1 Brennerdüsenträger mit Resonatoren Burner nozzle holder with resonators
01/21/2015EP2827063A1 A duct and method for damping pressure waves caused by thermoacoustic instability
01/21/2015EP2825824A1 Fuel air premixer for gas turbine engine
01/21/2015EP2825823A1 Gas turbine combustion system and method of flame stabilization in such a system
01/21/2015CN204114996U 预混合值班喷嘴 Premixed duty nozzle
01/21/2015CN204114995U 一种贫燃料多孔喷射燃烧系统 One kind of porous lean fuel injection combustion system
01/21/2015CN104296160A 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
01/21/2015CN102966974B 超声速燃烧室壁面凹腔结构及包含其的发动机燃烧室 Supersonic combustion chamber wall cavity structure and containing its engine combustor
01/21/2015CN102200292B 带凹腔的支板火焰稳定装置及火焰稳定方法 Support plate with a cavity flame stabilizer and flame stabilization method
01/20/2015US8935925 Stress reduction feature to improve fuel nozzle sheath durability
01/20/2015US8935911 Fuel spray apparatus for gas turbine engine
01/20/2015CA2608622C Combustor liner and heat shield assembly
01/15/2015WO2015004642A1 Gas turbine combustion chamber with reversible fastening device for thermoinsulating tiles
01/15/2015US20150016971 Compartmentalization of cooling air flow in a structure comprising a cmc component
01/15/2015US20150013340 Gas turbine engine combustor liner
01/15/2015US20150013339 Mixing arrangement for mixing a fuel with a stream of oxygen containing gas
01/14/2015EP2824391A1 Air-cooled swirler-head
01/14/2015CN204100296U 一种采用变截面台阶形多斜孔冷却结构的航空发动机燃烧室 One kind with variable cross-section stepped cooling structure more inclined hole aeroengine combustor
01/14/2015CN204100289U 气体燃料喷嘴及燃气轮机 Gas fuel nozzles and turbine
01/14/2015CN102901126B 燃烧组织结构 Burning structure
01/14/2015CN102695919B 燃气轮机用燃烧头 Gas turbine combustion head
01/14/2015CN102459849B 通过步进式调整稳定燃气轮机发动机 Stable gas turbine engine by stepping adjustment
01/14/2015CN101946063B 燃气轮机 Gas turbine
01/14/2015CN101799160B 用于燃烧器的稀释剂罩 Diluent shroud for the burner
01/13/2015US8931283 Reformed multi-fuel premixed low emission combustor and related method
01/13/2015US8931280 Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities
01/13/2015CA2582624C Flame-retention arm of a post-combustion chamber
01/08/2015WO2015002686A2 Gas turbine engine combustor liner panel
01/08/2015WO2015001517A1 Tile for covering combustion chambers, in particular for gas turbine energy production power plant and combustion chamber comprising said tile
01/08/2015US20150007576 Gas turbine power plant with non-homogeneous input gas
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