Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
06/2014
06/26/2014DE102012223913A1 Component used for fired ceramic shaped component used as fuel aid or heat shield, comprises unfired ceramic stripes in which stripe vertical to longitudinal edge comprises slot which is not extended over respective plate whole width
06/25/2014EP2746666A2 System for supplying fuel to a combustor
06/25/2014EP2746665A2 Fuel distribution and mixing plate
06/25/2014EP2745054A1 Combustion arrangement and turbine comprising a damping facility
06/25/2014EP2745051A1 Staged cooling flow nozzle valve
06/25/2014EP2744996A1 Split control unit
06/25/2014CN203671658U 一种燃气轮机的燃烧室及具有该燃烧室的燃气轮机 A gas turbine combustor and a gas turbine combustor having the
06/25/2014CN203671657U 一种火焰筒及包括该火焰筒的燃气轮机燃烧室 A gas turbine combustor liner and including the flame tube
06/25/2014CN203671656U 航空发动机燃烧室 Aero-engine combustion chamber
06/25/2014CN203671655U 一种燃烧室燃油喷射与混合系统 One kind of fuel injection and combustion hybrid system
06/25/2014CN203671654U 燃气轮机的燃烧室 Gas turbine combustor
06/25/2014CN203671653U 用于燃气轮机的燃烧室 The combustor for a gas turbine
06/25/2014CN203671652U 一种用于燃气轮机燃烧室的分散式进气的帽罩 A gas turbine combustor intake air distributed cap
06/25/2014CN203671651U 燃气轮机燃烧室用的帽罩组件 Gas turbine combustor cap assembly with
06/25/2014CN103890366A 用于附接中空部件的设备 A device for attaching the hollow member
06/25/2014CN103890350A 密封组装体及具备该密封组装体的燃气涡轮 The seal assembly and the seal assembly comprising a gas turbine
06/25/2014CN103884024A 一种能够组织燃烧并将火焰传导到外涵道气流的联焰装置 A way to organize the flame burning and conduction ducted airflow to the outer joint flame device
06/25/2014CN102721081B 一种等离子强化雾化喷嘴 A plasma enhanced atomizing nozzle
06/25/2014CN101981380B 燃烧器中的导引燃烧室 The pilot combustor burner
06/24/2014US8756934 Combustor cap assembly
06/19/2014WO2014092185A1 Multi-fuel-capable gas turbine combustor
06/19/2014WO2014090741A1 Gas turbine comprising at least one tubular combustion chamber
06/19/2014WO2014090495A1 Air directed fuel injection
06/19/2014WO2014090493A1 Recessed fuel injector positioning
06/19/2014US20140165577 Systems and Methods for Late Lean Injection Premixing
06/19/2014US20140165573 Process for producing refractory ceramics for gas turbine plants
06/18/2014EP2743588A1 Recessed fuel injector positioning
06/18/2014EP2743587A2 A fuel injector and a gas turbine engine combustion chamber
06/18/2014EP2743586A2 Systems and methods for late lean injection premixing
06/18/2014EP2743585A1 A combustion chamber
06/18/2014EP2743581A1 Air directed fuel injection
06/18/2014EP2743458A2 Apparatus and method for installing and removing a turbine transition piece
06/18/2014EP2743457A2 Turbine transition piece alignment apparatus and method
06/18/2014EP2742292A1 Combustor
06/18/2014EP2742291A1 System for injecting fuel in a gas turbine engine
06/18/2014EP2742290A1 Improved multi-fuel injection nozzle
06/18/2014EP2742289A2 Ceramic tile for combustion chambers lining, in particular of gas turbines, and manufacturing method thereof
06/18/2014CN203656984U 一种可变旋流数旋流器 A variable swirl number cyclone
06/18/2014CN103874887A Annular combustion chamber in a turbomachine
06/18/2014CN103868099A Aerial engine combustion chamber and aerial engine comprising same
06/18/2014CN103868098A Film cooled flame stabilizer
06/18/2014CN103868095A Active air flow control and adjustment device and engine combustion chamber including same
06/18/2014CN102282423B Wall for combustion chamber in a turbine engine with single annular row of intake openings for primary and dilution air
06/18/2014CN101818907B System and method for suppressing combustion instability in a turbomachine
06/18/2014CN101368739B Combustion method and device of fuel in gas turbine engine
06/12/2014WO2014086731A1 Method for operating a combustion system and combustion system
06/12/2014WO2014027005A3 Burner comprising a fuel plenum formed in a base
06/12/2014US20140157783 System for Protecting an Inner Wall of a Combustor
06/12/2014US20140157782 Spherical Collet for Mounting a Gas turbine Engine Liner
06/12/2014US20140157781 Fuel injector and a gas turbine engine combustion chamber
06/12/2014US20140157779 SYSTEM FOR REDUCING COMBUSTION DYNAMICS AND NOx IN A COMBUSTOR
06/12/2014DE102012023297A1 Schindelbefestigungsanordnung einer Gasturbinenbrennkammer Shingle mounting arrangement of a gas turbine combustor
06/11/2014EP2741005A1 A fuel nozzle for a combustor of a gas turbine engine
06/11/2014EP2741004A2 System for protecting an inner wall of a combustor
06/11/2014EP2741003A2 Controlling combustion system with fuel chemical induction time
06/11/2014EP2741001A1 Supporting structure for gas turbine combustion chamber heat-insulating tiles, heat-insulating module, and gas turbine combustion chamber
06/11/2014EP2739909A1 Cast manifold for dual fuel stage dry low nox gas turbine engine
06/11/2014EP2739905A2 A combustor resonator section with an internal thermal barrier coating and method of fabricating the same
06/11/2014CN103851647A Fuel injection and mixing system for combustion chamber and combustion chamber with same
06/11/2014CN103851646A Gas Turbine Combustion Chamber
06/11/2014CN103851645A Damping device for gas turbine combustor
06/11/2014CN103850796A A gas turbine engine system and an associated method thereof
06/11/2014CN102721083B Plasma-catalysis gaseous swirl nozzle
06/11/2014CN102679401B Asymmetric preheating combustion chamber
06/11/2014CN102538014B Dual-fuel swirling atomizing nozzle for chemical regenerative cycle
06/11/2014CN102272428B Engine
06/10/2014US8745989 Reverse flow ceramic matrix composite combustor
06/05/2014WO2014084965A1 Cooled combustor seal
06/05/2014WO2014084753A1 Transition piece for a gas turbine system
06/05/2014US20140150445 System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
06/05/2014US20140150442 Gas turbine centripetal annular combustion chamber and method for flow guidance
06/05/2014US20140150436 Gas turbine part comprising a near wall cooling arrangement
06/05/2014US20140150435 Damping device for a gas turbine combustor
06/04/2014EP2738471A1 Crossfire tube assembly between adjacent combustors
06/04/2014EP2738470A1 Shingle attachment assembly of a gas turbine combustion chamber
06/04/2014EP2738469A1 Gas turbine part comprising a near wall cooling arrangement
06/04/2014EP2738355A1 A gas turbine engine system and an associated method thereof
06/04/2014EP2737252A2 Gas turbine centripetal annular combustion chamber and method for flow guidance
06/04/2014CN103842728A Annular combustion chamber for a turbine engine
06/04/2014CN103842727A Combustor cap for damping low frequency dynamics
06/04/2014CN103836647A Venturi tube flow channel wall face structure
06/04/2014CN103836646A Gas turbine combustor
06/04/2014CN103835772A Turbomachine with trapped vortex feature
06/03/2014US8739547 Gas turbine engine joint having a metallic member, a CMC member, and a ceramic key
05/2014
05/30/2014WO2014081496A1 Apparatus and method to reduce wear and friction between cmc-to-metal attachment and interface
05/30/2014WO2014081334A1 Anti-coking liquid fuel cartridge
05/30/2014WO2014080758A1 Power generation system, method for powering power generation system, and combustor
05/30/2014WO2014055435A3 Flow divider mechanism for a multi-stage combustor
05/30/2014WO2014044654A3 Device for cooling a supporting structure of a heat shield, and heat shield
05/30/2014CA2835575A1 Damping device for a gas turbine combustor
05/29/2014US20140144150 Fuel nozzle for use in a turbine engine and method of assembly
05/29/2014US20140144149 Fuel Plenum Annulus
05/29/2014US20140144146 Tile fastening arrangement of a gas-turbine combustion chamber
05/29/2014US20140144145 Gas turbine combustion chamber
05/29/2014US20140144144 Gas Turbine Combustor
05/29/2014US20140144143 Combustion apparatus and gas turbine engine
05/29/2014US20140144142 Fuel nozzle for use in a turbine engine and method of assembly
05/29/2014US20140144141 Premixer with diluent fluid and fuel tubes having chevron outlets
05/29/2014US20140144138 Combustion Chamber Housing and Gas Turbine Equipped Therewith
05/29/2014US20140144122 Crossfire tube assembly between adjacent combustors
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