Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
11/2013
11/21/2013US20130305739 Fuel nozzle cap
11/21/2013US20130305734 Fuel Plenum Premixing Tube with Surface Treatment
11/21/2013US20130305726 Injector for the combustion chamber of a gas turbine having a dual fuel circuit, and combustion chamber provided with at least one such injector
11/21/2013US20130305725 Fuel nozzle cap
11/20/2013EP2664854A2 Secondary combustion system
11/20/2013EP2664853A2 Fuel plenum premixing tube with surface treatment
11/20/2013EP2664852A2 Fuel Nozzle Cap
11/20/2013EP2664851A2 Fuel nozzle cap
11/20/2013EP2664767A1 Fuel nozzle, gas turbine combustor equipped with same, and gas turbine equipped with this gas turbine combustor
11/20/2013EP2664410A2 Methods of fabricating fuel injectors using laser additive deposition
11/20/2013CN103398398A Double-seal connection structure of flame tube and transition section of combustion gas turbine combustion chamber
11/14/2013WO2013139868A3 Simultaneous broadband damping at multiple locations in a combustion chamber
11/14/2013WO2013135859A3 Annular-combustion-chamber bypass
11/14/2013WO2013135702A3 Heat-shield element for a compressor-air bypass around the combustion chamber
11/14/2013WO2013135568A3 Gas turbine and method for operating it
11/14/2013US20130299472 Method for perforating a wall of a combustion chamber
11/14/2013US20130298564 Cooling system and method for turbine system
11/14/2013US20130298563 Secondary Combustion System
11/14/2013US20130298561 Multi-tube fuel nozzle with mixing features
11/14/2013US20130298560 System for supplying a working fluid to a combustor
11/14/2013DE102006007087B4 Gasturbinen-Brennkammer A gas turbine combustor
11/13/2013EP2662627A2 Fuel injector with mixing circuit
11/13/2013EP2662626A2 System and method having multi-tube fuel nozzle with differential flow
11/13/2013EP2662625A1 Multi-tube fuel nozzle with mixing features
11/13/2013EP2662624A2 System for supplying a working fluid to a combustor
11/13/2013CN103388839A Multi-tube fuel nozzle with mixing feature
11/13/2013CN103388838A System and method having multi-tube fuel nozzle with differential flow
11/13/2013CN103388837A System for supplying working fluid to combustor
11/12/2013CA2586433C Flameholder fuel shield
11/12/2013CA2586431C Purged flameholder fuel shield
11/12/2013CA2551711C Augmentor radial fuel spray bar with counterswirling heat shield
11/07/2013WO2013166060A1 High velocity combustor
11/07/2013WO2013165868A1 Gas turbine engine combustor surge retention
11/07/2013US20130291544 Gas turbine engine combustor surge retention
11/07/2013US20130291543 Acoustic Resonator Located at Flow Sleeve of Gas Turbine Combustor
11/06/2013EP2660523A2 System and method for assembling an end cover of a combustor
11/06/2013EP2660522A2 Combustion nozzle and a related method thereof
11/06/2013EP2660521A2 A Fuel Nozzle
11/06/2013EP2660520A2 Fuel/air premixing system for turbine engine
11/06/2013EP2660519A1 Transition duct with late lean injection for a gas turbine
11/06/2013EP2660518A2 Acoustic resonator located at flow sleeve of gas turbine combustor
11/06/2013EP2659187A1 Engine and combustion system
11/06/2013EP2659184A2 Method and apparatus for isolating inactive fluid passages
11/06/2013CN203273947U Multifunctional gas wall surface protective coating
11/06/2013CN103383114A System and method for assembling an end cover of a combustor
11/06/2013CN103383113A Acoustic resonator located at flow sleeve of gas turbine combustor
11/06/2013CN101676632B Reusable weld joint for syngas fuel nozzles
11/05/2013US8572982 Diffuser having distribution element for providing part-flow
11/05/2013US8572981 Self-oscillating fuel injection jets
10/2013
10/31/2013WO2012063127A3 Ultra low emissions gas turbine combustor
10/31/2013US20130283810 Combustion nozzle and a related method thereof
10/31/2013US20130283807 System and method for supplying a working fluid to a combustor
10/31/2013US20130283806 Combustor and a method for repairing the combustor
10/31/2013US20130283805 Fuel/air premixing system for turbine engine
10/31/2013US20130283803 Device for injecting a mixture of air and fuel into a turbine engine combustion chamber
10/31/2013US20130283802 Combustor
10/31/2013US20130283801 System for supplying fuel to a combustor
10/31/2013US20130283800 System for supplying fuel to a combustor
10/31/2013US20130283799 Resonance damper for damping acoustic oscillations from combustor
10/31/2013US20130283798 Combustor and a method for assembling the combustor
10/30/2013EP2657611A2 System for supplying fuel to a combustor
10/30/2013EP2657610A2 A combustor and a method for assembling the combustor
10/30/2013EP2657609A1 Combustor cap mounting structure for a turbine engine
10/30/2013EP2657608A2 A Combustor
10/30/2013EP2657607A2 Combustor apparatus for stoichiometric combustion
10/30/2013EP2657606A2 A combustor and a method for repairing the combustor
10/30/2013EP2657605A2 System and Method for Supplying a Working Fluid to a Combustor
10/30/2013EP2657483A2 System for supplying fuel to a combustor
10/30/2013CN103375820A Combustor and method for assembling the combustor
10/30/2013CN103375819A Fuel/air premixing system for turbine engine
10/30/2013CN103375818A Combustion nozzle and a related method thereof
10/30/2013CN103375817A A fuel nozzle
10/30/2013CN103375816A System for supplying fuel to a combustor
10/30/2013CN103375815A System for supplying fuel to a combustor
10/30/2013CN103375814A Turbine combustor system having aerodynamic feed cap
10/30/2013CN103375813A System and method for supplying a working fluid to a combustor
10/30/2013CN103375812A Gas turbine combustor and a method for controlling air flow in the gas turbine combustor
10/30/2013CN103375811A Combustor
10/30/2013CN103375810A Combustor apparatus for stoichiometric combustion
10/30/2013CN103375265A Turboshaft engine and use method thereof
10/24/2013WO2013157976A1 Combustor liner stop
10/24/2013US20130276451 Combustion system including a transition piece and method of forming using a cast superalloy
10/24/2013US20130276450 Combustor apparatus for stoichiometric combustion
10/24/2013US20130276449 Combustor cap mounting structure for a turbine engine
10/24/2013DE102012007832A1 Verfahren zum Betrieb einer Gasturbineneinheit A method of operating a gas turbine unit
10/23/2013EP2653784A2 Micromixer assembly of a turbine system and method of assembly
10/23/2013EP2653783A2 Turbine combustor system having aerodynamic feed cap
10/23/2013EP2653782A2 Combustor flow sleeve with supplemental air supply
10/23/2013EP2525071B1 Continuous detonation wave engine and aircraft provided with such an engine
10/23/2013CN103363550A Swirler for combustion chambers
10/23/2013CN103363549A Combustor and method for supplying fuel to combustor
10/23/2013CN103363548A System and method for supporting fuel nozzles inside a combustor
10/23/2013CN103363547A Systems and methods for preventing flashback in a combustor assembly
10/23/2013CN103363546A Transition nozzle combustion system
10/23/2013CN103363545A Combustor with non-circular head end
10/23/2013CN101666496B Multi-tube arrangement for combustor and method of making multi-tube arrangement
10/22/2013US8561409 Quarls in a burner
10/22/2013CA2507190C Methods and apparatus for cooling turbine engine combustor ignition devices
10/17/2013WO2013155363A1 Combustion instability suppression system using heat insulating flameholding material
10/17/2013WO2013044197A8 A combustor resonator section with an internal thermal barrier coating and method of fabricating the same
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