Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
12/2012
12/11/2012CA2506208C Device for fastening a fluid conduit onto the casing of a turbojet engine
12/08/2012CA2778624A1 Injector tip assembly and method of fuel injection
12/06/2012WO2012165614A1 Gas turbine combustor
12/06/2012WO2011015285A3 Counter-flow combustor
12/06/2012US20120304660 Turbomachine combustors having different flow paths
12/06/2012US20120304659 Impingement sleeve and methods for designing and forming impingement sleeve
12/06/2012US20120304656 Combustion liner and transition piece
12/06/2012US20120304655 Turbomachine combustor assembly including a liner stop
12/06/2012US20120304650 Injection system for a turbomachine combustion chamber, including air injection means improving the air-fuel mixture
12/06/2012US20120304647 Reverse-flow annular combustor for reduced emissions
12/05/2012EP2530385A2 Turbomachine combustor assembly including a liner stop
12/05/2012EP2530384A2 Fuel injector
12/05/2012EP2530383A1 Gas turbine combustor
12/05/2012EP2530382A2 Fuel injector
12/05/2012EP2530381A2 Load member for transition duct in turbine system
12/05/2012EP2530248A1 Linear transition duct for a gas turbine
12/05/2012EP2530247A2 Mount Device For Transition Duct In Turbine System
12/05/2012CN1467407B Gas turbine engine combustor can with trapped vortex cavity
12/05/2012CN102812297A Turbomachine combustion chamber having a centrifugal compressor with no deflector
12/05/2012CN102809176A Aerodynamic fuel nozzle
12/05/2012CN102809175A Injector
12/05/2012CN102809174A Turbomachine combustor assembly
12/05/2012CN102808949A Hula seal with preferential cooling
12/05/2012CN102007342B Burner element and burner with corrosion-resistant insert
12/05/2012CN101576270B Fuel nozzle for a gas turbine engine and method for fabricating the same
12/04/2012CA2601934C Gas turbine combustor exit duct and hp vane interface
11/2012
11/29/2012WO2012161941A1 Turbine combustion system coupling with adjustable wear pad and corresponding assembling method
11/29/2012WO2012161903A1 Structural frame for gas turbine combustion cap assembly
11/29/2012WO2012161902A1 Gas turbine combustion cap assembly
11/29/2012WO2012161609A1 Combustor with bi-directional manifold for dynamics damping
11/29/2012WO2012161142A1 Hollow curved plate, method for manufacturing same, and burner for gas turbine
11/29/2012US20120297787 Flow straightener and mixer
11/29/2012US20120297786 System and method for flow control in gas turbine engine
11/29/2012US20120297785 System and method for flow control in gas turbine engine
11/29/2012US20120297784 System and method for flow control in gas turbine engine
11/29/2012US20120297783 System and method for flow control in gas turbine engine
11/29/2012US20120297782 System and method for turbine combustor mounting assembly
11/29/2012US20120297777 Reheat burner injection system with fuel lances
11/29/2012DE102011076473A1 Segmentbauteil aus Hochtemperaturgussmaterial für eine Ringbrennkammer, Ringbrennkammer für ein Flugzeugtriebwerk, Flugzeugtriebwerk und Verfahren zur Herstellung einer Ringbrennkammer Segment component from high temperature casting material for an annular combustion chamber, an annular combustion chamber for an aircraft engine, aircraft engine and method for producing an annular combustion chamber
11/28/2012EP2527744A2 System and method for turbine combustor mounting assembly
11/28/2012EP2527743A2 Segment component comprising high temperature cast material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for producing an annular combustion chamber
11/28/2012EP2527742A2 System and method for flow control in gas turbine engine
11/28/2012EP2527741A2 System and method for flow control in gas turbine engine
11/28/2012EP2527740A2 Combustors with quench inserts
11/28/2012EP2527739A2 System and method for flow control in gas turbine engine
11/28/2012EP2527738A2 System and method for flow control in gas turbine engine
11/28/2012EP2526341A1 Injector device and turbine engine combustion chamber provided with such an injector device
11/28/2012EP2526340A1 Resonator device for damping the pressure oscillation within a combustion chamber and a method for operating a combustion arrangement
11/28/2012CN202561810U Combustion chamber wall of aircraft engine
11/28/2012CN102804803A Instrumented component for wireless telemetry
11/28/2012CN102798151A Combustor nozzle and method for supplying fuel to combustor
11/28/2012CN102798150A System and method for flow control in gas turbine engine
11/28/2012CN102798149A Plasma concave-cavity flame stabilizer for engine
11/28/2012CN102798148A System and method for turbine combustor mounting assembly
11/28/2012CN102798147A System and method for flow control in gas turbine engine
11/28/2012CN102798146A System and method for flow control in gas turbine engine
11/28/2012CN102797565A Vortex composite heat engine
11/28/2012CN102797511A System and method for flow control in gas turbine engine
11/27/2012CA2666325C Thermodynamic cycles with thermal diluent
11/27/2012CA2512375C Turbojet with means of protection for a fuel injection unit, the injection unit and the turbojet undershield
11/24/2012CA2741100A1 High pressure oxy-fuel combustion system (hiprox) bottoming cycle
11/22/2012WO2012159067A1 Lean direct fuel injector
11/22/2012WO2012156631A1 Annular combustion chamber for a turbomachine
11/22/2012WO2012156596A1 Continuous detonation wave engine and aircraft provided with such an engine
11/22/2012WO2012156186A1 Combustor insert plate bolted to the combustion chamber side
11/22/2012WO2011163289A3 Secondary water injection for diffusion combustion systems
11/22/2012WO2010078104A3 Cooled flameholder swirl cup
11/22/2012US20120291446 Combustor
11/22/2012US20120291444 Method of operating a gas turbine engine
11/22/2012US20120291442 Wall for a turbomachine combustion chamber including an optimised arrangement of air inlet apertures
11/22/2012US20120291441 Injector device and combustion chamber for a turbomachine provided with such injector device
11/22/2012US20120291440 Gas turbine combustion cap assembly
11/22/2012US20120291439 Lean direct fuel injector
11/22/2012US20120291437 Turbine combustion system coupling with adjustable wear pad
11/22/2012DE102011075865A1 Brennkammerseitig verschraubte Brennereinsatzplatte Combustion chamber side burner insert screw-plate
11/22/2012CA2835361A1 Annular combustion chamber for a turbomachine
11/21/2012EP2525153A1 Flexible combustor fuel nozzle
11/21/2012EP2525152A2 Multipoint injectors
11/21/2012EP2525151A2 Combustor assembly for a turbomachine
11/21/2012EP2525149A2 Combustor
11/21/2012EP2525148A1 A combustor nozzle and method for supplying fuel to a combustor
11/21/2012EP2525071A1 Continuous detonation wave engine and aircraft provided with such an engine
11/21/2012EP2524169A1 Multi-bored combustion chamber having counter-rotating tangential flows
11/21/2012CN102792711A Instrumented component for wireless telemetry
11/21/2012CN102788699A Flame tube structure of thrust combustion chamber used for supercharger test
11/21/2012CN102788369A Flexible combustor fuel nozzle
11/21/2012CN102788368A Combustor nozzle and method for supplying fuel to a combustor
11/21/2012CN102788367A Mild combustor of gas turbine and implement method
11/21/2012CN102788366A Gas and water vapor mixed combustor
11/21/2012CN102788365A Combustor assembly for a turbomachine
11/20/2012US8312725 Vortex combustor for low NOX emissions when burning lean premixed high hydrogen content fuel
11/20/2012US8312723 System for injecting a mixture of air and fuel into a turbomachine combustion chamber
11/20/2012CA2714259C Combustor for a turbine, and gas turbine outfitted with a combustor of this kind
11/20/2012CA2580128C Flexible heat shields and method
11/15/2012WO2012153040A1 Device for mounting a spark plug in a combustion engine of a gas turbine engine
11/15/2012WO2012153003A1 Method for intensifying the combustion process
11/15/2012WO2012152530A1 Heat shield assembly
11/15/2012WO2011023648A3 Swirl blade, burner and gas turbine
11/15/2012US20120285173 Lobed swirler
11/15/2012US20120285172 Premixed burner for a gas turbine combustor
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