| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 07/26/1994 | US5331816 Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles |
| 07/26/1994 | US5331815 Impact resistant combustor |
| 07/26/1994 | US5331814 Gas turbine combustion chamber with multiple fuel injector arrays |
| 07/26/1994 | US5331805 Reduced diameter annular combustor |
| 07/26/1994 | US5331803 Method of obtaining a desired temperature profile in a turbine engine and turbine engine incorporating the same |
| 07/19/1994 | US5329773 Turbine combustor cooling system |
| 07/19/1994 | US5329772 Cast slot-cooled single nozzle combustion liner cap |
| 07/19/1994 | US5329761 Combustor dome assembly |
| 07/19/1994 | US5329759 Method for regulating fuel flow in a gas turbine engine |
| 07/14/1994 | DE4300275A1 Operation of turbocompressor system |
| 07/12/1994 | US5328355 Combustor and combustion apparatus |
| 07/12/1994 | US5328101 Gas turbine fuel nozzle seal |
| 07/12/1994 | US5327727 For use in a gas turbine engine |
| 07/12/1994 | US5327718 Gas turbine apparatus and method of control thereof |
| 07/06/1994 | EP0605158A1 Fuel trim system for a multiple chamber gas turbine combustion system |
| 07/05/1994 | US5325660 Method of burning a premixed gas in a combustor cap |
| 06/30/1994 | DE4244302A1 Impact cooling system for cooling surface e.g. of combustion chamber wall |
| 06/29/1994 | EP0604279A1 Injector with porous wall for a rocket combustion chamber |
| 06/29/1994 | EP0604021A1 Individually removable combustor liner panel for a gas turbine engine |
| 06/28/1994 | US5323614 Combustor for gas turbine |
| 06/28/1994 | US5323605 Double dome arched combustor |
| 06/28/1994 | US5323604 Triple annular combustor for gas turbine engine |
| 06/28/1994 | US5323602 Fuel/air distribution and effusion cooling system for a turbine engine combustor burner |
| 06/28/1994 | US5323601 Individually removable combustor liner panel for a gas turbine engine |
| 06/28/1994 | US5323600 Liner stop assembly for a combustor |
| 06/22/1994 | EP0602942A1 Pulsed fuel injection system for reducing NOx emissions |
| 06/22/1994 | EP0602901A1 Tertiary fuel injection system for use in a dry low NOx combustion system |
| 06/22/1994 | EP0602404A1 Gas turbine combustor |
| 06/22/1994 | EP0602384A1 Gasturbine combustor |
| 06/21/1994 | US5321951 Integral combustor splash plate and sleeve |
| 06/21/1994 | US5321948 Fuel staged premixed dry low NOx combustor |
| 06/21/1994 | US5321947 Lean premix combustion system having reduced combustion pressure oscillation |
| 06/17/1994 | CA2110560A1 Pulsed fuel injection system for reducing nox emissions |
| 06/16/1994 | DE4242099A1 Appts., esp. gas turbine appts. - having coating on its operating parts in contact with fuel gas or waste gas to reduce pollutant emissions |
| 06/14/1994 | US5319936 Combustor system for stabilizing a premixed flame and a turbine system using the same |
| 06/14/1994 | US5319935 Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection |
| 06/14/1994 | US5319931 Fuel trim method for a multiple chamber gas turbine combustion system |
| 06/14/1994 | US5319923 Air staged premixed dry low NOx combustor |
| 06/14/1994 | US5319919 Method for controlling gas turbine combustor |
| 06/08/1994 | EP0600041A1 Low emission combustion nozzle for use with a gas turbine engine. |
| 06/08/1994 | CN1024940C Circuit combustor fuel nozzle arrangement |
| 06/07/1994 | US5317865 Gas generating apparatus |
| 06/07/1994 | US5317864 Tangentially directed air assisted fuel injection and small annular combustors for turbines |
| 06/07/1994 | US5317863 Gas turbine combustion chamber with adjustable primary oxidizer intake passageways |
| 06/07/1994 | CA1329992C Hypersonic scramjet engine fuel injector |
| 06/01/1994 | EP0599055A1 Gasturbine combustor |
| 05/31/1994 | US5315815 Mechanism for controlling the rate of mixing in combusting flows |
| 05/25/1994 | EP0598662A1 Aerodynamic injection system for a combustion chamber |
| 05/24/1994 | US5313785 Dynamic pressure machine |
| 05/24/1994 | US5313781 Gasification-combined power plant |
| 05/19/1994 | DE4336096A1 Device for redn. of vibrations in combustion chamber for gas turbine systems - has equal number of burners in flow direction of gases displaced by specific distance which is determined by formula |
| 05/19/1994 | DE4238323A1 Mixer for gases and liquids has two mirror image centrifugal mixing chambers - releasing contra-rotating product into a common mixing chamber and single output maximising the mixing with no rifled mixer unit |
| 05/18/1994 | EP0597138A1 Combustion chamber for gas turbine |
| 05/18/1994 | EP0597137A1 Combustion chamber for gas turbine |
| 05/17/1994 | US5311743 Gas separator for a combustion chamber |
| 05/17/1994 | US5311742 Gas turbine combustor with nozzle pressure ratio control |
| 05/17/1994 | US5311735 Jet engine |
| 05/11/1994 | WO1994010436A1 Augmentor flame holder construction |
| 05/11/1994 | EP0349635B1 Turbine combustor with tangential fuel injection and bender jets |
| 05/10/1994 | US5309718 Liquid fuel turbocharged power plant and method |
| 05/10/1994 | US5309710 Gas turbine combustor having poppet valves for air distribution control |
| 05/10/1994 | US5309709 Low emission combustion system for a gas turbine engine |
| 05/04/1994 | EP0595026A1 Method for a multistage combustion in gas turbines |
| 05/03/1994 | US5307637 Angled multi-hole film cooled single wall combustor dome plate |
| 05/03/1994 | US5307635 Fuel nozzle with combined radial and axial bellows |
| 05/03/1994 | US5307634 Premix gas nozzle |
| 05/03/1994 | US5307633 Low carbon particle producing gas turbine combustor |
| 04/28/1994 | WO1994009269A1 Combustor heat shield for a turbine containment ring |
| 04/27/1994 | EP0594127A1 Combustor for gas turbines |
| 04/26/1994 | US5305609 Fuel injector arrangement |
| 04/26/1994 | US5305608 Liquid fuel power plant and method |
| 04/20/1994 | EP0539359B1 Flame tube with a cooled supporting frame for a heat-resistant lining |
| 04/19/1994 | US5303554 Low NOx injector with central air swirling and angled fuel inlets |
| 04/19/1994 | US5303544 Gas turbine system with a tube-nested combustion chamber type combustor |
| 04/19/1994 | US5303543 Annular combustor for a turbine engine with tangential passages sized to provide only combustion air |
| 04/19/1994 | US5303542 Fuel supply control method for a gas turbine engine |
| 04/14/1994 | WO1994008179A1 Multiple passage cooling circuit for gas turbine fuel injector nozzle |
| 04/13/1994 | EP0592305A1 Post-combustor for bypass gas turbine |
| 04/13/1994 | EP0592223A1 Auto-ignition system and method for premixed gas turbine combustors |
| 04/13/1994 | EP0592161A1 Gas turbine engine combustor |
| 04/12/1994 | US5302795 Welding equipment for fabricating a combustion liner |
| 04/08/1994 | CA2107842A1 Auto-ignition system for premixed gas turbine combustors |
| 04/06/1994 | EP0590338A1 Gas turbine combustion chamber |
| 04/06/1994 | EP0590297A1 Gasturbine combustion chamber |
| 03/30/1994 | EP0589520A1 Combustion system with low pollutant emission for gas turbines |
| 03/29/1994 | US5297515 Fuel supply systems for engines and combustion processes therefor |
| 03/29/1994 | US5297391 Fuel injector for a turbojet engine afterburner |
| 03/29/1994 | US5297390 Fuel injection nozzle having tip cooling |
| 03/29/1994 | US5297385 For a gas turbine engine |
| 03/27/1994 | CA2105692A1 Gas turbine group |
| 03/23/1994 | EP0588629A1 Gas turbine fuel nozzle with replaceable cap |
| 03/23/1994 | EP0587580A1 Gas turbine engine combustor. |
| 03/22/1994 | US5295773 Self-locking pressed in insert arrangement |
| 03/22/1994 | US5295354 Low pollution combustion chamber for a turbojet engine |
| 03/22/1994 | US5295352 Dual fuel injector with premixing capability for low emissions combustion |
| 03/19/1994 | CA2106424A1 Gas turbine fuel nozzle with replaceable cap |
| 03/16/1994 | CN1083899A Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors |
| 03/08/1994 | US5291733 Liner mounting assembly |
| 03/08/1994 | US5291732 Combustor liner support assembly |
| 03/08/1994 | CA1327455C Breach-cooled structure |