| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
|---|
| 06/13/1995 | US5423173 Fuel injector and method of operating the fuel injector |
| 06/08/1995 | DE4341450A1 Flow guide baffle for gas turbine combustion chamber |
| 06/07/1995 | EP0656512A1 Dual fuel gas turbine combustor |
| 06/07/1995 | EP0656511A1 Pneumatic valve for combustion air in gasturbine |
| 06/06/1995 | US5421158 Segmented centerbody for a double annular combustor |
| 06/04/1995 | CA2137200A1 Dual fuel gas turbine combustor |
| 06/04/1995 | CA2137184A1 System for controlling combustion in a gas combustion-type turbine |
| 06/01/1995 | WO1995014854A1 Gas valve |
| 06/01/1995 | DE4340530A1 Thin cylindrical liner support |
| 05/31/1995 | CN1028663C Means and method for reducing differential pressure loading in augmented gas turbine engine |
| 05/30/1995 | US5419681 Film cooled wall |
| 05/30/1995 | US5419115 Bulkhead and fuel nozzle guide assembly for an annular combustion chamber |
| 05/30/1995 | US5419114 Thermoelastic connection of the injector tube and the flame tube of a gas turbine |
| 05/24/1995 | EP0654639A1 Adjustable swirl vanes for combustor of gas turbine |
| 05/24/1995 | DE4441507A1 Cooling structure for gas turbine blade |
| 05/23/1995 | US5417070 For use in the combustion apparatus of a gas turbine engine |
| 05/23/1995 | US5417069 Separator for an annular gas turbine combustion chamber |
| 05/23/1995 | US5417054 Fuel purging fuel injector |
| 05/18/1995 | WO1995005063A3 Method of converting thermal energy to mechanical energy and a device for carrying out the same |
| 05/18/1995 | DE4339094A1 Damping of thermal-acoustic vibrations resulting from combustion of fuel |
| 05/17/1995 | EP0653040A1 Dual fuel injector nozzel for use with a gas turbine engine |
| 05/17/1995 | EP0577618B1 Gas turbine combustor |
| 05/17/1995 | EP0548143B1 Gas turbine with a gaseous fuel injector and injector for such a gas turbine |
| 05/17/1995 | EP0491877B1 Integrated power unit combustion apparatus and method |
| 05/16/1995 | US5415000 Low NOx combustor retro-fit system for gas turbines |
| 05/09/1995 | US5413647 Superalloy with nickel, chromium, cobalt, tungsten, niobium, tantalum, titanium, aluminum and carbon with melting and centrifuging |
| 05/09/1995 | US5412938 Combustion chamber of a gas turbine having premixing and catalytic burners |
| 05/04/1995 | DE4438495A1 Injection system and associated tri-coaxial injection elements |
| 05/03/1995 | EP0651207A1 Diffuser with a varying circumferential supply |
| 05/03/1995 | EP0651144A1 Method for conversion of heat energy into mechanical energy in a gas-turbine engine, and gas-turbine engine |
| 05/02/1995 | US5410884 Combustor for gas turbines with diverging pilot nozzle cone |
| 04/28/1995 | CA2134419A1 Gas turbine combustor |
| 04/27/1995 | WO1995011409A1 Fuel supply system for a staged combustor |
| 04/27/1995 | WO1995011408A1 Fuel injector |
| 04/27/1995 | WO1995011374A1 Pilot fuel cooled flow divider valve for a staged combustor |
| 04/25/1995 | US5408830 Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines |
| 04/25/1995 | US5408825 Dual fuel gas turbine combustor |
| 04/25/1995 | US5408824 Rotary heat engine |
| 04/20/1995 | DE4335412A1 Method and device for fuel distribution in annular combustion chambers of gas turbine plants |
| 04/19/1995 | EP0648979A1 Method and means for cooling a gas turbine combustion chamber |
| 04/18/1995 | US5406799 Combustion chamber |
| 04/18/1995 | US5406798 Pilot fuel cooled flow divider valve for a staged combustor |
| 04/12/1995 | EP0647817A1 Double-walled combustion chamber |
| 04/11/1995 | US5404711 Dual fuel injector nozzle for use with a gas turbine engine |
| 04/05/1995 | EP0646228A1 Catalytic combustion. |
| 04/04/1995 | US5402635 Gas turbine combustor with cooling cross-flame tube connector |
| 04/04/1995 | US5402634 Fuel supply system for a staged combustor |
| 04/04/1995 | US5402633 Premix gas nozzle |
| 03/30/1995 | DE4434515A1 Oxide dispersion strengthened alloy, and high-temperature equipment produced from this alloy |
| 03/29/1995 | EP0645527A1 Method of reducing ignition temperature in exothermic catalytic reaction |
| 03/29/1995 | EP0644994A1 Combustion chamber apparatus and method for performing combustion. |
| 03/28/1995 | US5400968 Injector tip cooling using fuel as the coolant |
| 03/28/1995 | US5400589 Afterburner for a turbofan engine |
| 03/28/1995 | US5400587 Gas turbine annular combustion chamber having radially displaced groups of oppositely swirling burners. |
| 03/28/1995 | US5400586 Self-accommodating brush seal for gas turbine combustor |
| 03/28/1995 | US5400491 Apparatus for repairing a combustion chamber assembly |
| 03/28/1995 | CA1334893C Gas turbine engine combustors |
| 03/22/1995 | EP0644375A2 Fuel purging fuel injector |
| 03/21/1995 | US5398509 Gas turbine engine combustor |
| 03/21/1995 | US5398496 Gas turbine engines |
| 03/21/1995 | US5398495 Combustion chamber with variable oxidizer intakes |
| 03/16/1995 | WO1995007408A1 Method of operating a gas turbine using an additive feed |
| 03/16/1995 | DE4330612A1 Method and device for driving a gas turbine |
| 03/15/1995 | EP0643267A1 Premixed gas burning method and combustor |
| 03/14/1995 | US5396763 Cooled spraybar and flameholder assembly including a perforated hollow inner air baffle for impingement cooling an outer heat shield |
| 03/14/1995 | US5396761 Gas turbine engine ignition flameholder with internal impingement cooling |
| 03/14/1995 | US5396759 Gas turbine engine combustor |
| 03/10/1995 | CA2131663A1 Gas turbine combustor |
| 03/08/1995 | EP0641235A1 Small gas turbine |
| 03/07/1995 | US5394688 Gas turbine combustor swirl vane arrangement |
| 03/01/1995 | EP0640745A1 Component cooling method |
| 03/01/1995 | EP0584263B1 Method and system for combusting hydrocarbon fuels with low pollutant emissions |
| 03/01/1995 | EP0584216B1 Method and system for staged rich/lean combustion |
| 02/28/1995 | US5392596 Combustor assembly construction |
| 02/23/1995 | WO1995005561A1 Injector tip cooling using fuel as the coolant |
| 02/23/1995 | WO1995005063A2 Method of converting thermal energy to mechanical energy and a device for carrying out the same |
| 02/23/1995 | CA2145774A1 Injector tip cooling using fuel as the coolant |
| 02/15/1995 | EP0638768A2 Fuel nozzle with non-axisymmetrical secondary spray |
| 02/14/1995 | US5388412 Gas turbine combustion chamber with impingement cooling tubes |
| 02/14/1995 | US5388396 Low carbon particle producing gas turbine combustor |
| 02/09/1995 | WO1995004244A1 Fuel injector and method of operating the fuel injector |
| 02/08/1995 | CN1098491A Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer |
| 02/02/1995 | DE4325802A1 Method for operating a gas turbine system having liquid or gaseous fuel |
| 02/01/1995 | EP0636835A2 Swirl mixer for a combustor |
| 01/31/1995 | US5385015 Augmentor burner |
| 01/26/1995 | WO1995002752A1 Apparatus for repairing a combustion chamber assembly |
| 01/26/1995 | WO1995002751A1 Method for repairing a combustion chamber assembly |
| 01/25/1995 | EP0635681A1 Single stage premixed constant fuel/air ratio combustor |
| 01/19/1995 | DE4339724C1 Gas fitting |
| 01/17/1995 | US5381652 Combustion system with low pollutant emission for gas turbines |
| 01/12/1995 | WO1995001501A1 Starting fuel pressure schedule for a gas turbine |
| 01/05/1995 | DE4321393A1 Wall structure, in particular for a ram-jet engine (ram-jet, ram engine, athodyd) |
| 01/04/1995 | EP0631656A1 Catalytic combustion process using supported palladium oxide catalysts |
| 01/03/1995 | US5377483 Process for single stage premixed constant fuel/air ratio combustion |
| 12/28/1994 | EP0631093A1 Combustion chamber with a gas separator |
| 12/27/1994 | US5375995 Burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or firing installation |
| 12/27/1994 | US5375420 Segmented centerbody for a double annular combustor |
| 12/27/1994 | US5375411 Bypass line of a premixing burner in gas turbine combustion chambers |
| 12/22/1994 | WO1994029647A1 Dual fuel injector nozzel for use with a gas turbine engine |
| 12/22/1994 | DE4320428A1 Probe lead-through for a combustion chamber |