Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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10/18/2001 | US20010029738 Combustion apparatus |
10/18/2001 | US20010029701 Sub-critical water-fuel composition and combustion system |
10/18/2001 | DE10017429A1 Verbundkeramiksubstrat mit gradierter thermochemischer Schutzschicht Composite ceramic substrate with graded thermochemical protective layer |
10/17/2001 | EP1146289A1 Cooling structure of combustor tail tube |
10/17/2001 | EP1144916A1 Burner and process for operating gas turbines |
10/17/2001 | CN1317634A Method and appts. for reducing discharge of gas turbine |
10/17/2001 | CN1317633A Method and appts. for reducing heat stress in gas turbine |
10/16/2001 | US6301900 Gas turbine combustor with fuel and air swirler |
10/16/2001 | US6301899 Mixer having intervane fuel injection |
10/11/2001 | US20010027653 Cooling system for gas turbine combustor |
10/11/2001 | US20010027639 Fuel injection for a staged gas turbine combustion chamber |
10/11/2001 | US20010027638 Method and apparatus for minimizing thermoacoustic vibrations in gas-turbine combustion chambers |
10/11/2001 | US20010027637 Gas-turbine engine combustion system |
10/10/2001 | EP1143201A2 Cooling system for gas turbine combustor |
10/10/2001 | EP1143199A1 Methods and apparatus for reducing gas turbine engine emissions |
10/10/2001 | EP1143196A1 Methods and apparatus for reducing thermal stresses within turbine engines |
10/10/2001 | EP1143107A2 Gas turbine transition duct end frame cooling |
10/10/2001 | EP1142852A2 Composite ceramic material having graded thermochemical protective coating |
10/09/2001 | US6298667 Modular combustor dome |
10/09/2001 | US6298659 Vortex flow field and apparatus and method for producing the same |
10/09/2001 | US6298654 Ambient pressure gas turbine system |
10/04/2001 | US20010025491 Burner configuration |
10/04/2001 | EP1139021A2 Liquid fuel injection nozzles |
10/04/2001 | EP1139020A1 Gas turbine engine combustion system |
10/04/2001 | EP1137899A1 Combustion device and method for burning a fuel |
10/04/2001 | EP0776444B1 Low-emission combustion chamber for gas turbine engines |
10/03/2001 | CN1072304C Gas-turbine generating equipment |
10/02/2001 | US6295801 Fuel injector bar for gas turbine engine combustor having trapped vortex cavity |
10/02/2001 | CA2070518C Combustor dome assembly |
09/27/2001 | WO2001071252A1 Method and apparatus for a fuel-rich catalytic reactor |
09/27/2001 | US20010024774 Burner configuration with primary and secondary pilot burners |
09/27/2001 | US20010023590 Three-dimensional swirler in a gas turbine combustor |
09/26/2001 | EP0995066B1 Arrangement of burners for heating installation, in particular a gas turbine combustion chamber |
09/26/2001 | EP0956475B1 Burner for fluid fuels |
09/25/2001 | US6294261 (i) a metal-based substrate; (ii) a ceramic-based protective coating applied over the substrate; and (iii) a ceramic-based slurry/gel overcoat over the surface of the protective coating. |
09/20/2001 | US20010022088 Gas turbine combustor |
09/20/2001 | DE10008809A1 Method of damping combustion-chamber combustion fluctuations in gas-turbine |
09/19/2001 | EP1134494A1 Gas turbine combustor |
09/18/2001 | US6289677 Gas turbine fuel injector |
09/18/2001 | US6289676 Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles |
09/18/2001 | US6289668 Arrangement for the selective introduction of fuel and/or water into combustion chamber |
09/18/2001 | US6289667 Combustion chamber and a method of operation thereof |
09/14/2001 | CA2330262A1 Gas turbine combustor |
09/13/2001 | US20010020364 Gas turbine combustor |
09/13/2001 | US20010020359 Low NOX gas turbine combustor liner |
09/13/2001 | US20010020358 Method of operating a gas turbine and corresponding gas turbine |
09/12/2001 | EP1132687A1 Methods and apparatus for reducing thermal stresses in an augmentor |
09/12/2001 | EP1132686A1 Methods and apparatus for reducing heat load in combustor panels |
09/11/2001 | US6286317 Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity |
09/11/2001 | US6286302 Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein |
09/11/2001 | US6286300 Combustor with fuel preparation chambers |
09/11/2001 | US6286298 Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity |
09/07/2001 | WO2001065073A1 Turbine installation |
09/06/2001 | US20010019781 Brazing alloy and plasma spraying bonding coating |
09/06/2001 | DE10000415A1 Verfahren und Vorrichtung zur Unterdrückung von Strömungswirbeln innerhalb einer Strömungskraftmaschine Method and apparatus for suppressing flow vortices within a turbomachine |
09/05/2001 | EP1130322A1 Multi-stage multi-plane combustion system for a gas turbine engine |
09/05/2001 | EP1130321A1 Combustor liner cooling thimbles and related method |
09/05/2001 | EP1130219A1 Turbine engine with sealing means between panels |
09/04/2001 | US6284323 Thermal barrier coating systems and materials |
09/04/2001 | US6282905 Gas turbine combustor cooling structure |
09/04/2001 | US6282904 Full ring fuel distribution system for a gas turbine combustor |
09/04/2001 | US6282886 Gas turbine combustor |
09/04/2001 | US6282885 Gas turbine engine |
08/30/2001 | WO2001063177A1 Heat shield element, combustor and gas turbine |
08/30/2001 | US20010018173 Method of operating a hybrid burner |
08/30/2001 | US20010018172 Combustors with improved dynamics |
08/30/2001 | US20010017034 Wall elements for gas turbine engine combustors |
08/29/2001 | EP1128131A1 Heat shield element, combustion chamber and gas turbine |
08/28/2001 | US6280140 Method and apparatus for cooling an airfoil |
08/28/2001 | US6279323 Low emissions combustor |
08/28/2001 | US6279313 Combustion liner for gas turbine having liner stops |
08/28/2001 | US6279310 Gas turbine starting method using gas and liquid fuels |
08/23/2001 | WO2001061250A1 Thermal shield stone and device for lining a combustion chamber, and gas turbine |
08/22/2001 | EP1126221A1 Padded refactory tile as liner for a gas turbine combustor |
08/22/2001 | EP1125087A1 Burner assembly |
08/22/2001 | EP0910776B1 Burner with atomiser nozzle |
08/22/2001 | CA2299746A1 Jet engine catalytic converter |
08/21/2001 | US6276142 Cooled heat shield for gas turbine combustor |
08/16/2001 | WO2001059369A1 Device in a burner for gas turbines |
08/16/2001 | EP1123457A2 Gas turbine engine |
08/14/2001 | US6272865 Swirler scoop and bearing plate for combustor |
08/14/2001 | US6272864 Combustor for a gas turbine |
08/14/2001 | US6272863 Premixed combustion method background of the invention |
08/14/2001 | US6272847 Centrifugal direct injection engine |
08/14/2001 | US6272842 Combustor tuning |
08/14/2001 | US6272840 Piloted airblast lean direct fuel injector |
08/09/2001 | DE10003728A1 Hitzeschildanordnung für eine Heißgas führende Komponente, insbesondere für Strukturteile von Gasturbinen A heat shield arrangement for a hot gas-carrying component, in particular for structural parts of gas turbines |
08/08/2001 | EP1121561A1 Fuel injection system for the radial or slinger combustion chamber in a small gas turbine |
08/07/2001 | US6270338 Method for operating a premix burner |
08/07/2001 | US6269646 Combustors with improved dynamics |
08/07/2001 | US6269625 Methods and apparatus for igniting a catalytic converter in a gas turbine system |
08/07/2001 | CA2255883C Combustor tail tube cooling structure |
08/02/2001 | WO2001055646A1 Low cost, low emissions natural gas combustor |
08/02/2001 | WO2001055273A2 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
07/31/2001 | US6266961 Film cooled combustor liner and method of making the same |
07/26/2001 | WO2001053729A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall |
07/26/2001 | WO2001018371A8 Ambient pressure gas turbine system |
07/25/2001 | EP1118806A1 Thermally charged wall structure and method to seal gaps in such a structure |
07/25/2001 | EP0813668B1 Method of burning fuel in a gas turbine and a corresponding gas turbine |
07/24/2001 | US6263664 Combined steam and gas turbine engine with magnetic transmission |