Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
09/2002
09/19/2002DE10112864A1 Verfahren zum Zünden einer thermischen Turbomaschine Method for igniting a thermal turbomachine
09/18/2002EP1241413A2 Replaceable afterburner heat shield
09/18/2002EP1241334A1 Ignition method for a turbomachine
09/17/2002US6449956 Bypass air injection method and apparatus for gas turbines
09/17/2002US6449952 Removable cowl for gas turbine combustor
09/17/2002US6449951 Combustion device for generating hot gases
09/12/2002US20020125336 Air assist fuel nozzle
09/12/2002US20020124572 Combustion apparatus
09/11/2002EP1239219A1 Fluid distributor, burner device, gas turbine engine, and cogeneration system
09/11/2002EP1239117A2 Gas turbine combustor transition piece outlet structure, transition piece, combustor and gas turbine
09/11/2002CN1368600A Heating device of external-burning engine
09/11/2002CN1090730C Combustion apparatus of gas turbine and method for controlling combustion of same
09/10/2002US6446439 Pre-mix nozzle and full ring fuel distribution system for a gas turbine combustor
09/10/2002US6446438 Combustion chamber/venturi cooling for a low NOx emission combustor
09/10/2002US6446426 Miniature pulsed heat source
09/06/2002WO2002068867A2 Control strategy for flexible catalytic combustion system
09/05/2002DE10108561A1 Thermische Turbomaschine und Verfahren zum Zünden der thermischen Turbomaschine A thermal turbo-machine and method for starting the thermal turbomachine
09/05/2002DE10108560A1 Verfahren zum Betrieb einer Ringbrennkammer sowie eine diesbezügliche Ringbrennkammer Method for operating an annular combustion chamber and an annular combustion chamber in this respect
09/04/2002EP0968355B1 Cooling supply manifold assembly for cooling combustion turbine components
09/04/2002EP0961907B1 Combustor arrangement
09/04/2002EP0766754B1 Method and apparatus for increasing the flow rate of a liquid through an orifice
09/04/2002CN1367815A Sub-critical water-fuel composition and combustion system
09/03/2002US6442946 Three degrees of freedom aft mounting system for gas turbine transition duct
09/03/2002US6442940 Gas-turbine air-swirler attached to dome and combustor in single brazing operation
09/03/2002US6442939 Diffusion mixer
09/03/2002US6442928 Control system for gas turbine
09/03/2002CA2089272C Impact resistant combustor
08/2002
08/29/2002WO2002066898A1 Combustion chamber of a gas-turbine engine
08/29/2002US20020116929 Low emissions combustor for a gas turbine engine
08/28/2002EP1235033A2 Annular combustor and method of operating the same
08/28/2002EP1235032A2 Low emissions combustor for a gas turbine engine
08/28/2002EP1234963A1 Turbomachine ignition device and ignition method
08/28/2002EP1234144A1 Simple low cost fuel nozzle support
08/28/2002CN1089796C Dimethyl ether fuel and method of generating power in dry low NOx combustion system
08/27/2002US6438963 Liquid fuel and water injection purge systems and method for a gas turbine having a three-way purge valve
08/27/2002US6438961 Swozzle based burner tube premixer including inlet air conditioner for low emissions combustion
08/27/2002US6438959 Combustion cap with integral air diffuser and related method
08/27/2002US6438958 Apparatus for reducing heat load in combustor panels
08/27/2002US6438940 Methods and apparatus for providing uniform ignition in an augmenter
08/27/2002CA2091497C Dry low nox multi-nozzle combustion liner cap assembly
08/22/2002US20020112483 Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure
08/22/2002US20020112482 Methods for decreasing combustor emissions
08/22/2002US20020112480 Gas turbine engine combustion system
08/21/2002EP0904512B1 Heat-shield arrangement, especially for structural components of gas turbine plants
08/20/2002US6435816 Gas injector system and its fabrication
08/20/2002US6434945 Dual fuel nozzle
08/20/2002US6434926 Combustion chamber for gas turbines
08/20/2002US6434821 Method of making a combustion chamber liner
08/15/2002WO2002063156A1 Bulkhead for dual fuel industrial and aeroengine gas turbines
08/15/2002US20020110501 For providing axial support for catalytic converter catalysts
08/15/2002US20020108378 Liner supporting structure for annular combuster
08/15/2002US20020108375 Method and apparatus for enhancing heat transfer in a combustor liner for a gas turbine
08/15/2002US20020108374 Slot cooled combustor liner
08/14/2002EP1231435A2 Slot cooled combustor liner
08/14/2002EP1231369A2 Gas turbine control system compensating water content in combustion air
08/14/2002EP1084368B1 Fuel injector
08/14/2002EP0875721B1 Spring seal unit of combustor
08/13/2002US6430933 Oscillation attenuation in combustors
08/13/2002US6430932 Low NOx combustion liner with cooling air plenum recesses
08/13/2002US6430930 Arrangement for reduction of acoustic vibrations in a combustion chamber
08/13/2002CA2056498C Double dome combustor and method of operation
08/08/2002WO2002061339A1 Premix burner and method for operating such a premix burner
08/08/2002US20020106599 Premix burner arrangement with catalytic combustion as well as method for its operation
08/08/2002US20020106001 System and method for determining gas turbine firing and combustion reference temperatures having correction for water content in fuel
08/08/2002US20020104316 Ultra low emissions gas turbine cycle using variable combustion primary zone airflow control
08/08/2002DE10104695A1 Vormischbrenner sowie Verfahren zum Betrieb eines derartigen Vormischbrenners Premix burner and method of operation of such a premix burner
08/07/2002EP1229290A2 Afterburner heat shield
08/07/2002EP1032791B1 Combustion chamber and method for cooling a combustion chamber with vapour
08/06/2002US6427930 Device for connection of a nozzle of a pre-mixing chamber of a gas turbine, to a housing of the pre-mixing chamber
08/06/2002US6427447 Bulkhead for dual fuel industrial and aeroengine gas turbines
08/06/2002US6427446 Low NOx emission combustion liner with circumferentially angled film cooling holes
08/06/2002US6427435 Retainer segment for swirler assembly
08/01/2002WO2002059238A2 Sub-critical water-fuel composition and combustion system
08/01/2002US20020100270 Heating device for external combustion engine
07/2002
07/31/2002EP1227272A2 Cloth ring seal
07/31/2002EP1226896A2 Nickel-base braze material and braze repair method
07/31/2002EP0807213B1 Flow-guiding body for gas turbine combustion chambers
07/30/2002US6425240 Combustor for gas turbine engine
07/30/2002US6425239 Method of operating a gas turbine
07/24/2002EP1225392A2 Combustor mixer having plasma generating nozzle
07/24/2002EP1224423A1 Burner
07/24/2002CN1088172C Method and equipment for starting combustion chamber of gas turbine
07/24/2002CN1088151C Gas turbine annular shape combustion chamber
07/18/2002WO2002055754A2 Method and device for gas phase diffusion coating of metal components
07/18/2002US20020092303 Methods and apparatus for supplying air to turbine engine combustors
07/18/2002US20020092302 Combustor mixer having plasma generating nozzle
07/17/2002EP1223383A1 Gas turbine combustor, pre-mixer for gas turbine combustors, and premixing method for gas turbine combustors
07/17/2002EP1223382A2 Methods and apparatus for supplying air to turbine engine combustors
07/16/2002US6418726 Method and apparatus for controlling combustor emissions
07/16/2002US6418725 Gas turbine staged control method
07/16/2002US6418709 Gas turbine engine liner
07/16/2002CA2122148C Turbine engine control system
07/11/2002US20020089298 Apparatus for robotically inspecting gas turbine combustion components
07/11/2002US20020088234 Fuel injectors
07/11/2002US20020088233 Gas turbine combustor
07/11/2002US20020088221 Method and device for generating hot combustion waste gases
07/11/2002DE10051221A1 Brenner mit gestufter Brennstoff-Eindüsung Burner with staged fuel injection
07/10/2002EP1221574A2 Gas turbine combustor
07/10/2002CN1357706A Combustor with stepped fuel spray and its running process
07/09/2002US6415610 Apparatus and method for replacement of combustor basket swirlers