Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
07/1994
07/26/1994US5331816 Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles
07/26/1994US5331815 Impact resistant combustor
07/26/1994US5331814 Gas turbine combustion chamber with multiple fuel injector arrays
07/26/1994US5331805 Reduced diameter annular combustor
07/26/1994US5331803 Method of obtaining a desired temperature profile in a turbine engine and turbine engine incorporating the same
07/19/1994US5329773 Turbine combustor cooling system
07/19/1994US5329772 Cast slot-cooled single nozzle combustion liner cap
07/19/1994US5329761 Combustor dome assembly
07/19/1994US5329759 Method for regulating fuel flow in a gas turbine engine
07/14/1994DE4300275A1 Operation of turbocompressor system
07/12/1994US5328355 Combustor and combustion apparatus
07/12/1994US5328101 Gas turbine fuel nozzle seal
07/12/1994US5327727 For use in a gas turbine engine
07/12/1994US5327718 Gas turbine apparatus and method of control thereof
07/06/1994EP0605158A1 Fuel trim system for a multiple chamber gas turbine combustion system
07/05/1994US5325660 Method of burning a premixed gas in a combustor cap
06/1994
06/30/1994DE4244302A1 Impact cooling system for cooling surface e.g. of combustion chamber wall
06/29/1994EP0604279A1 Injector with porous wall for a rocket combustion chamber
06/29/1994EP0604021A1 Individually removable combustor liner panel for a gas turbine engine
06/28/1994US5323614 Combustor for gas turbine
06/28/1994US5323605 Double dome arched combustor
06/28/1994US5323604 Triple annular combustor for gas turbine engine
06/28/1994US5323602 Fuel/air distribution and effusion cooling system for a turbine engine combustor burner
06/28/1994US5323601 Individually removable combustor liner panel for a gas turbine engine
06/28/1994US5323600 Liner stop assembly for a combustor
06/22/1994EP0602942A1 Pulsed fuel injection system for reducing NOx emissions
06/22/1994EP0602901A1 Tertiary fuel injection system for use in a dry low NOx combustion system
06/22/1994EP0602404A1 Gas turbine combustor
06/22/1994EP0602384A1 Gasturbine combustor
06/21/1994US5321951 Integral combustor splash plate and sleeve
06/21/1994US5321948 Fuel staged premixed dry low NOx combustor
06/21/1994US5321947 Lean premix combustion system having reduced combustion pressure oscillation
06/17/1994CA2110560A1 Pulsed fuel injection system for reducing nox emissions
06/16/1994DE4242099A1 Appts., esp. gas turbine appts. - having coating on its operating parts in contact with fuel gas or waste gas to reduce pollutant emissions
06/14/1994US5319936 Combustor system for stabilizing a premixed flame and a turbine system using the same
06/14/1994US5319935 Staged gas turbine combustion chamber with counter swirling arrays of radial vanes having interjacent fuel injection
06/14/1994US5319931 Fuel trim method for a multiple chamber gas turbine combustion system
06/14/1994US5319923 Air staged premixed dry low NOx combustor
06/14/1994US5319919 Method for controlling gas turbine combustor
06/08/1994EP0600041A1 Low emission combustion nozzle for use with a gas turbine engine.
06/08/1994CN1024940C Circuit combustor fuel nozzle arrangement
06/07/1994US5317865 Gas generating apparatus
06/07/1994US5317864 Tangentially directed air assisted fuel injection and small annular combustors for turbines
06/07/1994US5317863 Gas turbine combustion chamber with adjustable primary oxidizer intake passageways
06/07/1994CA1329992C Hypersonic scramjet engine fuel injector
06/01/1994EP0599055A1 Gasturbine combustor
05/1994
05/31/1994US5315815 Mechanism for controlling the rate of mixing in combusting flows
05/25/1994EP0598662A1 Aerodynamic injection system for a combustion chamber
05/24/1994US5313785 Dynamic pressure machine
05/24/1994US5313781 Gasification-combined power plant
05/19/1994DE4336096A1 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
05/19/1994DE4238323A1 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
05/18/1994EP0597138A1 Combustion chamber for gas turbine
05/18/1994EP0597137A1 Combustion chamber for gas turbine
05/17/1994US5311743 Gas separator for a combustion chamber
05/17/1994US5311742 Gas turbine combustor with nozzle pressure ratio control
05/17/1994US5311735 Jet engine
05/11/1994WO1994010436A1 Augmentor flame holder construction
05/11/1994EP0349635B1 Turbine combustor with tangential fuel injection and bender jets
05/10/1994US5309718 Liquid fuel turbocharged power plant and method
05/10/1994US5309710 Gas turbine combustor having poppet valves for air distribution control
05/10/1994US5309709 Low emission combustion system for a gas turbine engine
05/04/1994EP0595026A1 Method for a multistage combustion in gas turbines
05/03/1994US5307637 Angled multi-hole film cooled single wall combustor dome plate
05/03/1994US5307635 Fuel nozzle with combined radial and axial bellows
05/03/1994US5307634 Premix gas nozzle
05/03/1994US5307633 Low carbon particle producing gas turbine combustor
04/1994
04/28/1994WO1994009269A1 Combustor heat shield for a turbine containment ring
04/27/1994EP0594127A1 Combustor for gas turbines
04/26/1994US5305609 Fuel injector arrangement
04/26/1994US5305608 Liquid fuel power plant and method
04/20/1994EP0539359B1 Flame tube with a cooled supporting frame for a heat-resistant lining
04/19/1994US5303554 Low NOx injector with central air swirling and angled fuel inlets
04/19/1994US5303544 Gas turbine system with a tube-nested combustion chamber type combustor
04/19/1994US5303543 Annular combustor for a turbine engine with tangential passages sized to provide only combustion air
04/19/1994US5303542 Fuel supply control method for a gas turbine engine
04/14/1994WO1994008179A1 Multiple passage cooling circuit for gas turbine fuel injector nozzle
04/13/1994EP0592305A1 Post-combustor for bypass gas turbine
04/13/1994EP0592223A1 Auto-ignition system and method for premixed gas turbine combustors
04/13/1994EP0592161A1 Gas turbine engine combustor
04/12/1994US5302795 Welding equipment for fabricating a combustion liner
04/08/1994CA2107842A1 Auto-ignition system for premixed gas turbine combustors
04/06/1994EP0590338A1 Gas turbine combustion chamber
04/06/1994EP0590297A1 Gasturbine combustion chamber
03/1994
03/30/1994EP0589520A1 Combustion system with low pollutant emission for gas turbines
03/29/1994US5297515 Fuel supply systems for engines and combustion processes therefor
03/29/1994US5297391 Fuel injector for a turbojet engine afterburner
03/29/1994US5297390 Fuel injection nozzle having tip cooling
03/29/1994US5297385 For a gas turbine engine
03/27/1994CA2105692A1 Gas turbine group
03/23/1994EP0588629A1 Gas turbine fuel nozzle with replaceable cap
03/23/1994EP0587580A1 Gas turbine engine combustor.
03/22/1994US5295773 Self-locking pressed in insert arrangement
03/22/1994US5295354 Low pollution combustion chamber for a turbojet engine
03/22/1994US5295352 Dual fuel injector with premixing capability for low emissions combustion
03/19/1994CA2106424A1 Gas turbine fuel nozzle with replaceable cap
03/16/1994CN1083899A Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors
03/08/1994US5291733 Liner mounting assembly
03/08/1994US5291732 Combustor liner support assembly
03/08/1994CA1327455C Breach-cooled structure