Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
07/2001
07/24/2001US6263663 Variable-throat gas-turbine combustion chamber
07/24/2001US6263660 Apparatus and method for fuel-air mixing before supply of low pressure lean pre-mix to combustor for rotating ramjet engine driving a shaft
07/19/2001WO2001051787A1 Piloted airblast lean direct fuel injector
07/19/2001US20010008070 Air impingement cooling system
07/18/2001EP1116918A1 Combustor swirler assembly
07/18/2001EP1116805A2 Method and apparatus for increasing the flow rate of a liquid through an orifice
07/17/2001US6260359 Offset dilution combustor liner
07/12/2001WO2001049394A2 Air separation method and plant
07/12/2001US20010007719 Mixed oxide overcoating metal or alloy; gas turbine engine
07/12/2001CA2389546A1 Air separation method and plant
07/11/2001EP1114967A1 Method and device for suppressing whirls in a turbo-engine
07/11/2001EP1114279A1 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same
07/11/2001CN1068408C Power apparatus
07/10/2001US6256995 Simple low cost fuel nozzle support
07/10/2001CA2229218C Gas-turbine engine
07/04/2001EP1112462A1 Method for operating a gas turbine and corresponding gas turbine
07/03/2001US6253555 Combustion chamber comprising mixing ducts with fuel injectors varying in number and cross-sectional area
07/03/2001US6253538 Variable premix-lean burn combustor
06/2001
06/28/2001WO2000045398A9 Injector mixer
06/28/2001US20010004835 Combustion chamber for a gas turbine engine
06/28/2001US20010004827 Fuel system configuration for staging fuel for gas turbines utilizing both gaseous and liquid fuels
06/27/2001EP1111219A2 Mounting an igniter in an augmenter
06/27/2001EP1110034A1 Burner arrangement with primary and secondary pilot burners
06/26/2001US6250082 Combustor rear facing step hot side contour method and apparatus
06/26/2001US6250066 Combustor with dilution bypass system and venturi jet deflector
06/26/2001US6250063 Fuel staging apparatus and methods for gas turbine nozzles
06/26/2001US6250062 Fuel nozzle centering device and method for gas turbine combustors
06/21/2001WO2001044720A1 Fluid distributor, burner device, gas turbine engine, and cogeneration system
06/21/2001US20010004515 Combustion chamber
06/21/2001CA2394397A1 Fluid distributor, burner device, gas turbine engine, and cogeneration system
06/20/2001EP1108958A1 Fuel nozzle for gas turbine engine and method of assembling
06/20/2001EP1108957A1 A combustion chamber
06/20/2001EP1108184A1 Arrangement for reduction of acoustinc vibrations in a combustion chamber
06/20/2001CN1067460C Pumping device
06/19/2001US6247317 Fuel nozzle helical cooler
06/19/2001US6247300 Gas turbine engine
06/19/2001US6247299 Method for feeding a gas turbine with both liquid and gaseous fuels
06/14/2001US20010003226 Method for the manufacture of a combustion chamber of a gas-turbine engine
06/13/2001EP1106928A1 Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels
06/13/2001EP1106927A1 Method of manufacturing a gas turbine engine combustion chamber
06/13/2001EP1106919A1 Methods and apparatus for decreasing combustor emissions
06/13/2001EP1105678A1 Operating method for a hybrid burner
06/13/2001DE19959292A1 Verfahren zum Herstellen einer Brennkammer eines Gasturbinen-Triebwerks A method of manufacturing a combustor of a gas turbine engine
06/13/2001CN1299456A Support structures for catalyst
06/13/2001CN1299032A Shaping method and apparatus for stairs-like heating side of hurner back lining
06/12/2001US6244051 Burner with atomizer nozzle
06/12/2001CA2048727C Gas turbine engine multi-hole film cooled combustor liner
06/07/2001WO2001040713A1 Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor
06/07/2001WO2001040710A1 Simple low cost fuel nozzle support
06/06/2001EP1104872A1 Method for decreasing a heat load on a combustor liner
06/06/2001EP1104871A1 Combustion chamber for a gas turbine engine
06/06/2001CN1298076A Air jet engine with rotating combustion chamber with specific heat converting effect
06/05/2001US6240883 Sub-critical water-fuel composition and combustion system
06/05/2001US6240732 Fluid manifold
06/05/2001US6240731 Low NOx combustor for gas turbine engine
05/2001
05/31/2001WO2000045398A3 Injector mixer
05/30/2001EP1103767A1 Gas turbine and gas turbine combustor
05/30/2001EP1103699A2 Gas turbine combined cycle system
05/30/2001EP1103628A2 A coating system for providing environmental protection to a metal substrate
05/29/2001US6237344 Dimpled impingement baffle
05/29/2001US6237343 Combustion chamber and a method of operation thereof
05/29/2001US6237323 Gas turbine combustor by-pass valve device
05/29/2001CA2246218C Gas turbine combustor
05/23/2001EP1101899A1 Method and apparatus for cooling an airfoil
05/22/2001US6235370 High temperature erosion resistant, abradable thermal barrier composite coating
05/17/2001US20010001171 Coal gasification combined cycle power generation plant and an operating method thereof
05/16/2001CN1065947C Gas turbine engine with improved convectively coded single stage, fully premixed fuel/air combustion system
05/15/2001US6231991 Ceramic on superalloy turbine
05/15/2001US6230482 Appliance for operating a gas turbine installation combustion chamber with liquid fuel
05/10/2001WO2001033138A1 Burner
05/09/2001EP1098141A1 Wall elements for gas turbine engine combustors
05/09/2001EP1098140A1 Methods and apparatus for fuel nozzle staging for gas turbine engines
05/08/2001US6226977 Bypass air volume control device for combustor used in gas turbine
05/03/2001US20010000563 Gas turbine combustor by-pass valve device
05/02/2001EP1096207A1 Combustor mounting for a gas turbine engine
05/02/2001EP1096206A1 Low emissions combustor
05/02/2001EP1096205A1 Offset dilution combustion liner
05/02/2001EP1096201A1 Burner
05/02/2001EP1095228A1 Igniter with porous sleeve
05/01/2001US6223538 Ceramic lining
05/01/2001US6223537 Catalytic combustor for gas turbines
04/2001
04/26/2001WO2001029484A1 Gas turbine combustor, pre-mixer for gas turbine combustors, and premixing method for gas turbine combustors
04/26/2001DE19950417A1 Component for gas turbine, with base body and protective covering made of ceramic material
04/24/2001US6220036 Cooling structure for combustor tail pipes
04/24/2001US6220035 Annular combustor tangential injection flame stabilizer
04/24/2001US6220034 Convectively cooled, single stage, fully premixed controllable fuel/air combustor
04/24/2001US6220015 Gas-turbine engine combustion system
04/19/2001WO2001027534A1 Combustor and method of burning fuel
04/19/2001WO2000025067A9 Fuel air mixer for a radial dome in a gas turbine engine combustor
04/18/2001EP1092925A1 Film cooled combustor liner and method of making the same
04/17/2001US6217832 Support structures for a catalyst
04/17/2001US6216644 Flow duct with cross-sectional step
04/17/2001US6216466 Fuel-injection arrangement for a gas turbine combustor
04/17/2001US6216442 Supports for connecting a flow sleeve and a liner in a gas turbine combustor
04/12/2001DE19948956A1 Mounting system for burner duct in gas turbine cylinder comprises internal groove in cylinder into which lugs on top and bottom retaining components fit, side pieces being fitted between retaining components and bolted into place
04/12/2001DE19948673A1 Procedure to produce hot gases in combustion unit, especially for driving of gas turbines, entails creating in gas stream areas with different mean flow speeds, and injecting into these areas fuel
04/11/2001EP1090256A1 Fuel injector for gas turbine engine
04/11/2001EP0943069A4 An electricity generating system having an annular combustor
04/10/2001US6212878 Gas generator module
04/10/2001US6212874 Propulsion system