Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
02/2002
02/07/2002WO2002010090A1 Fiber coating compounds for reinforced ceramic matrix composites
02/07/2002WO2001055273A3 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines
02/07/2002US20020014079 Multi-circuit, multi-injection point atomizer
02/07/2002US20020014078 Fuel discharge member, a burner, a premixing nozzle of a combustor, a combustor, a gas turbine, and a jet engine
02/07/2002DE10036211A1 Combustion chamber shingle for aviation gas turbine has plate-form base component with hole for threaded bolt with head fixed in recess by clamping connection formed by deformation of edge section of head recess or bolt head
02/07/2002DE10035676A1 Gasturbine und Verfahren zum Betrieb einer Gasturbine Gas turbine and method of operating a gas turbine
01/2002
01/31/2002WO2002008592A1 Gas turbine and method for operating a gas turbine
01/31/2002WO2001049394A3 Air separation method and plant
01/31/2002US20020011070 Combustor, a gas turbine, and a jet engine
01/31/2002US20020011064 Fuel injector with bifurcated recirculation zone
01/29/2002US6341485 Gas turbine combustion chamber with impact cooling
01/23/2002EP1174662A1 Apparatus to reduce the vibrations of a turbine combustor
01/23/2002EP1174209A1 Method of repairing combustion chamber liners
01/23/2002EP1060349A4 Pre-mixed combustion method
01/22/2002US6339925 Hybrid catalytic combustor
01/22/2002US6339923 Fuel air mixer for a radial dome in a gas turbine engine combustor
01/17/2002WO2002004794A2 Partitioned multi-channel combustor
01/17/2002US20020005037 Measurement method for detecting and quantifying combustor dynamic pressures
01/17/2002DE10032471A1 Method for adapting the operating status of a stepped combustion chamber for gas turbines feeds an overall fuel mass flow rate into a combustion chamber through a control valve adapted to a defined operating point for a power mechanism.
01/16/2002EP1172611A1 Gas turbine combustor having dome-to-line joint
01/16/2002EP1172610A1 Fuel nozzle for premix turbine combustor
01/15/2002US6338240 Control method for gas turbine load
01/13/2002CA2352811A1 A fuel discharge member, a burner, a premixing nozzle of a combustor, a combustor, a gas turbine, and a jet engine
01/10/2002US20020002820 Gas turbine apparatus with heat exchanger
01/10/2002US20020002818 Apparatus for fuel nozzle staging for gas turbine engines
01/09/2002EP1169557A1 Biomass combustion chamber for gas turbine
01/02/2002EP1167882A1 Methods and apparatus for decreasing combustor emissions with spray bar assembly
01/02/2002EP1167881A1 Methods and apparatus for decreasing combustor emissions with swirl stabilized mixer
01/02/2002EP1167697A1 Turbine engine
01/02/2002EP1165941A1 High temperature erosion resistant, abradable thermal barrier composite coating
01/01/2002US6335105 For forming part for a gas turbine engine, heat resistance
01/01/2002US6334769 Catalytic combustor and method of operating same
01/01/2002US6334310 Fracture resistant support structure for a hula seal in a turbine combustor and related method
01/01/2002US6334309 Liquid fuel injector for burners in gas turbines
01/01/2002US6334303 Flameholder device for afterburners in gas turbine engines
01/01/2002US6334298 Gas turbine combustor having dome-to-liner joint
01/01/2002US6334297 Combuster arrangement
01/01/2002US6334294 Combustion crossfire tube with integral soft chamber
12/2001
12/27/2001WO2001098713A1 Fuel injector for low emissions premixing gas turbine combustor
12/26/2001CN1076786C 燃烧室 Combustor
12/25/2001US6332313 Combustion chamber with separate, valved air mixing passages for separate combustion zones
12/20/2001WO2001096785A1 Method for operating a burner and burner with stepped premix gas injection
12/20/2001US20010052229 Burner with uniform fuel/air premixing for low emissions combustion
12/20/2001DE10029607A1 Method to operate burner; involves operating burner with two groups of fuel outlets to supply different amounts of same fuel, where outlet groups are supplied independently and controlled separately
12/19/2001EP0988441B1 Combustion turbine cooling panel
12/18/2001US6331110 External dilution air tuning for dry low NOx combustors and methods therefor
12/18/2001US6331109 Premix burner
12/18/2001US6330791 Burner for operating gas turbines with minimal NOx emissions
12/18/2001US6330789 Methods of operation a dual-fuel injector for a gas turbine with simultaneous liquid and gaseous fuels injection during transients
12/18/2001CA2076102C Aero-slinger combustor
12/18/2001CA2016346C Fringed thermal protection device and method of manufacturing it
12/13/2001US20010050318 Integrated fuel injection and mixing system with impingement cooling face
12/13/2001US20010049932 Premixing dry low NOx emissions combustor with lean direct injection of gas fuel
12/11/2001US6327861 Gas turbine combustor
12/11/2001US6327860 Fuel injector for low emissions premixing gas turbine combustor
12/11/2001US6327845 Gas turbine combustor by-pass valve device
12/06/2001WO2001092787A1 Flame-passage device for non-annular gas turbine combustion chambers
12/06/2001WO2001092786A1 Catalytic combustor having reduced light-off temperature
12/06/2001US20010048036 Integrated fluid injection air mixing system
12/06/2001US20010047650 Method of operating a gas-turbine chamber with gaseous fuel
12/05/2001EP1160512A2 Fracture resistant support structure for a hula seal in a turbine combustor and related method
12/05/2001EP1160511A1 Gas turbine combustor by-pass valve device
12/05/2001EP1160432A1 Gas turbine engine
12/05/2001EP0960308B1 Gas turbine installation with a ceramic-covered combustion chamber housing
12/04/2001US6325618 Fuel lance for spraying liquid and/or gaseous fuels into a combustion chamber
12/04/2001US6324830 Gas turbine engines
12/04/2001US6324827 Method of generating power in a dry low NOx combustion system
11/2001
11/29/2001WO2001090652A1 Combustor dome assembly and method of assembling the same
11/29/2001WO2001051787A8 Piloted airblast lean direct fuel injector
11/29/2001US20010046651 External dilution air tuning for dry low NOX combustors and methods therefor
11/29/2001US20010046650 Method and apparatus for a fuel-rich catalytic reactor
11/29/2001US20010045474 Liquid fuel injection nozzles
11/29/2001US20010045094 Gas turbine engine combustion system
11/28/2001EP1158246A2 Retainer segment for swirler assembly
11/27/2001US6321541 Multi-circuit multi-injection point atomizer
11/22/2001US20010042375 Gas turbine combustor
11/21/2001EP1156281A2 Gas turbine combustor
11/21/2001EP1156280A2 Gas turbine engine liner
11/21/2001EP0928396B1 Thermal shield component with cooling fluid recirculation and heat shield arrangement for a component circulating hot gas
11/21/2001EP0900351B1 Fuel injection method for a stepped gas turbine combustion chamber
11/21/2001CN2460879Y flat bell-jar type vortex combustion chamber
11/13/2001US6314739 Brazeless combustor dome assembly
11/13/2001US6314717 Electricity generating system having an annular combustor
11/13/2001US6314716 Serial cooling of a combustor for a gas turbine engine
11/08/2001WO2001084061A2 Miniature pulsed heat source
11/08/2001WO2001083963A1 Annular combustor for use with an energy system
11/08/2001US20010037646 Cooling structure of combustor tail tube
11/08/2001CA2407717A1 Annular combustor for use with an energy system
11/07/2001EP1152191A2 Combustor having a ceramic matrix composite liner
11/07/2001EP0796986B1 Gas-turbine engine
11/06/2001US6313544 Self-contained energy center for producing mechanical, electrical, and heat energy
11/06/2001US6313361 Formation of a stable wax slurry from a Fischer-Tropsch reactor effluent
11/06/2001US6311496 Gas turbine fuel/air mixing arrangement with outer and inner radial inflow swirlers
11/06/2001US6311471 Steam cooled fuel injector for gas turbine
10/2001
10/31/2001EP1150072A2 Gas turbine combustion chamber with supply openings
10/25/2001US20010032453 Ceramic member support structure for gas turbine
10/25/2001DE10018602A1 Calibrating device to determine through-flow characteristic of fuel nozzle has injection orifice of fuel nozzle located in pressure chamber filled with fluid and which has outlet with through-flow adjustable to pressure in pressure chamber
10/24/2001EP1148300A1 Ceramic member support structure for gas turbine
10/24/2001EP1148299A1 Method and apparatus for increasing heat transfer from combustors
10/23/2001US6305172 Scroll for a combustion system