Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
07/2002
07/09/2002US6415609 Replaceable afterburner heat shield
07/09/2002US6415608 Piloted rich-catalytic lean-burn hybrid combustor
07/09/2002US6415594 Methods and apparatus for reducing gas turbine engine emissions
07/04/2002WO2002052201A1 Burner comprising a graduated fuel injection
07/04/2002WO2002052194A1 Ultrasonically enhanced continuous flow fuel injection apparatus and method
07/04/2002WO2002052134A2 Diffusion premixer
07/04/2002WO2000073701A9 A swirling flashback arrestor
07/04/2002US20020083715 Method of thermal NOx reduction in catalytic combustion systems
07/04/2002US20020083714 Liquid fuel combustion system and method
07/04/2002US20020083711 Combustion cap with integral air diffuser and related method
07/04/2002DE10064264A1 Anordnung zur Kühlung eines Bauteils Arrangement for cooling a component
07/04/2002CA2430688A1 Ultrasonically enhanced continuous flow fuel injection apparatus and method
07/03/2002EP1219900A2 Gas turbine combustion device
07/03/2002EP1219872A2 Pressure activated cloth seal
07/03/2002EP1073864B1 Combustion chamber assembly
07/03/2002EP1005620B1 Thermal shield component with recirculation of cooling fluid
07/03/2002EP0785975B1 Improvements in the combustion and utilisation of fuel gases
07/02/2002US6414458 Apparatus for robotically inspecting gas turbine combustion components
07/02/2002US6412282 Combustion chamber
07/02/2002US6412272 Fuel nozzle guide for gas turbine engine and method of assembly/disassembly
07/02/2002US6412268 Cooling air recycling for gas turbine transition duct end frame and related method
06/2002
06/27/2002US20020079655 Cloth ring seal
06/27/2002US20020079654 Pressure activated cloth seal
06/27/2002US20020078691 Arrangement for cooling a component
06/27/2002US20020078690 Fuel air premixer having a diffuser assembly and upstream fuel manifold rings
06/27/2002US20020078676 Gas turbine combustion device
06/26/2002EP1217295A2 Burner for generating a hot gas
06/26/2002EP1216797A1 Methods for robotically inspecting gas turbine combustion components
06/26/2002EP1216796A1 Apparatus for robotically inspecting gas turbine combustion components
06/26/2002EP1216385A1 Variable premix-lean burn combustor
06/26/2002CN1086773C Work method of power station equipment
06/25/2002US6408629 Combustor liner having preferentially angled cooling holes
06/25/2002US6408628 Wall elements for gas turbine engine combustors
06/25/2002CA2089285C Segmented centerbody for a double annular combustor
06/20/2002WO2002048610A1 Catalytic combustion device with liquid fuel vaporisation on hot walls
06/20/2002WO2002048527A1 Combustor turbine successive dual cooling
06/20/2002US20020074965 Apparatus for robotically inspecting gas turbine combustion components
06/20/2002US20020073788 Methods for robotically inspecting gas turbine combustion components
06/20/2002US20020073711 Combustor rear facing step hot side contour method
06/20/2002US20020073710 Method of cooling gas only nozzle fuel tip
06/20/2002US20020073709 Gas only nozzle
06/20/2002US20020073708 Method of assembling a fuel injector for the combustion chamber of a turbomachine
06/20/2002US20020073707 Full cooling of main injectors in a two-headed combustion chamber
06/20/2002DE10062253A1 Gas turbine for aircraft has mesh of heat-resistant material, e.g. ceramic, in its combustion chamber
06/20/2002DE10061526A1 Vormischbrenneranordnung zum Betrieb einer Brennkammer Premix burner for operating a combustion chamber
06/19/2002CN1354819A Gas turbine engine
06/18/2002US6405536 Gas turbine combustor burning LBTU fuel gas
06/18/2002US6405523 Method and apparatus for decreasing combustor emissions
06/13/2002US20020069648 Novel design of adiabatic combustors
06/13/2002US20020069645 Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
06/13/2002US20020069644 Combustor turbine successive dual cooling
06/13/2002US20020069636 Hybrid rocket engine and method of propelling a rocket
06/13/2002DE10061527A1 Vormischbrenneranordnung mit katalytischer Verbrennung sowie Verfahren zum Betrieb hierzu Premix burner with catalytic combustion and method for operating this
06/12/2002EP1213541A1 Premix burner with catalytic combustion and method of operating
06/12/2002EP1213539A1 Gas turbine combustor, gas turbine, and jet engine
06/12/2002EP1213536A2 Premix burner with catalytic pilot burner
06/11/2002US6401447 Combustor apparatus for a gas turbine engine
06/06/2002US20020068250 Partitioned multi-channel combustor
06/06/2002US20020066273 Plate fin and combustor using the plate fin
06/06/2002US20020066272 Gas turbine combustor, gas turbine, and jet engine
06/06/2002US20020066268 Mixing enhancement using axial flow
06/05/2002EP1211463A2 Plate fin and combustor using the plate fin
06/05/2002EP0800892B1 Exchanging device for combustor
06/04/2002US6397765 Wall segment for a combustion chamber and a combustion chamber
06/04/2002US6397603 Conbustor having a ceramic matrix composite liner
06/04/2002US6397602 Fuel system configuration for staging fuel for gas turbines utilizing both gaseous and liquid fuels
06/04/2002US6397581 Heat exchanger in composite material and method for making same
06/04/2002US6397576 Gas turbine engine with exhaust compressor having outlet tap control
06/04/2002CA2364238A1 Plate fin and combustor using the plate fin
05/2002
05/30/2002US20020063479 Active turbine combustion parameter control system and method
05/28/2002US6395216 Method and apparatus for ultrasonically assisted melt extrusion of fibers
05/28/2002US6394791 Method and apparatus for a fuel-rich catalytic reactor
05/28/2002US6393828 Protective coatings for turbine combustion components
05/28/2002US6393823 Methods for fuel nozzle staging for gas turbine engines
05/23/2002WO2002004794A3 Partitioned multi-channel combustor
05/23/2002US20020061485 Combustor
05/23/2002DE10056243A1 Brennkammer und Verfahren zum Betrieb dieser Brennkammer Combustor and method of operation of this combustion chamber
05/23/2002DE10056124A1 Brennersystem mit gestufter Brennstoff-Eindüsung und Verfahren zum Betrieb Burner system with staged fuel injection and method of operating
05/23/2002DE10055408A1 Verfahren zur Brenstoffeinspritzung in einen Brenner Method for Brenstoffeinspritzung into a burner
05/23/2002DE10049205A1 Process for supplying fuel to a premix burner for operating a gas turbine comprises introducing premix gas separately via two axially divided regions along the burner shell
05/23/2002DE10049203A1 Verfahren zur Brennstoffeinleitung in einen Vormischbrenner Method for fuel discharge into a premix burner
05/22/2002EP1207350A2 Combustor and method for operating the same
05/22/2002EP1207344A2 Combustor
05/22/2002EP1207273A2 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
05/21/2002US6392313 Microturbomachinery
05/21/2002US6390805 Method of preventing flow instabilities in a burner
05/21/2002US6389815 Fuel nozzle assembly for reduced exhaust emissions
05/21/2002US6389801 Jet propulsion power unit with non-metal components
05/21/2002US6389800 Apparatus for fuel nozzle staging for gas turbine engines
05/21/2002US6389798 Combustor flow controller for gas turbine
05/21/2002US6389797 Gas turbine combined cycle system
05/21/2002US6389792 Combustor rear facing step hot side contour method
05/16/2002WO2002038920A2 Thermally tolerant support structure for a catalytic combustion catalyst
05/16/2002US20020056277 Double wall combustor arrangement
05/16/2002US20020056276 Process and apparatus for control of NOx in catalytic combustion systems
05/15/2002EP1205713A1 Method of fuel injection in a burner
05/15/2002EP1205712A2 Catalytic combustor flow conditioner and method for providing uniform gas velocity distribution
05/15/2002EP1205653A1 Burner with staged fuel injection and method of operation
05/15/2002EP1205635A2 Gas injector system and its fabrication
05/15/2002EP1204727A1 Sub-critical water-fuel composition and combustion system