| Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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| 08/09/2005 | US6926496 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing |
| 08/09/2005 | US6925811 modifications of components of gas turbine engines to reduce the temperature of boundary walls of the hot section portions of the components by optical reflection of radiation generated by combustion. |
| 08/09/2005 | US6925809 Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
| 08/09/2005 | US6925808 Combustion chamber with a closed cooling system for a turbine |
| 08/04/2005 | WO2005071320A1 Thermal shield |
| 08/04/2005 | US20050166599 Gas turbine combustion apparatus |
| 08/04/2005 | US20050166596 Resonator adopting counter-bored holes and method of suppressing combustion instabilities |
| 08/04/2005 | US20050166595 Method and system for controlling fuel supply in a combustion turbine engine |
| 08/04/2005 | DE102005002527A1 Kraftstoffzuführungsdurchgang und Verfahren zu dessen Ausbildung im Zuführungsarm eines Kraftstoff-Injektors Fuel supply passage and method of education in the feed arm of a fuel injector |
| 08/03/2005 | EP1559955A2 Burner |
| 08/03/2005 | EP1558876A1 Integrated combustor and nozzle for a gas turbine combustion system |
| 08/03/2005 | EP1558875A1 Liner for a gas turbine engine combustor having trapped vortex cavity |
| 08/03/2005 | EP1558443A1 Method for producing a porous, plate-type metallic composite |
| 08/02/2005 | US6924040 Ceramic containing hafnia, germanium oxide on metallic substrate |
| 08/02/2005 | US6924002 comprises nickel/aluminum based intermetallics; for promoting heat transfer |
| 08/02/2005 | US6923002 Combustion liner cap assembly for combustion dynamics reduction |
| 08/02/2005 | US6923001 Pilotless catalytic combustor |
| 08/02/2005 | CA2193724C Method and apparatus for increasing the flow rate of a liquid through an orifice |
| 08/02/2005 | CA2159929C Segmented centerbody for a double annular combustor |
| 07/28/2005 | WO2005068913A1 Premixing burner arrangement for operating a combustion chamber in addition to a method for operating a combustion chamber |
| 07/28/2005 | WO2004065763A3 Thermodynamic cycles using thermal diluent |
| 07/28/2005 | US20050164138 Premixed exit ring pilot burner |
| 07/28/2005 | US20050160739 Method for operating a gas turbine combustion chamber |
| 07/28/2005 | US20050160738 Side-fed shielded internal fuel manifold inlet tube |
| 07/28/2005 | US20050160737 Rotary combustor, and electrical generator comprising a combustor of this type |
| 07/28/2005 | US20050160717 Combustion wave ignition for combustors |
| 07/28/2005 | US20050160715 Rotary combustor, and electricity generator comprising such a combustor |
| 07/28/2005 | DE10360951A1 Wärmekraftanlage mit sequentieller Verbrennung und reduziertem CO2-Ausstoß sowie Verfahren zum Betreiben einer derartigen Anlage Thermal power plant with sequential combustion and reduced CO2 emissions and method for operating such a system |
| 07/27/2005 | EP1557611A1 Flow barrier, lining and combustion chamber |
| 07/27/2005 | EP1557607A1 Burner with cooled component, gas turbine and method for cooling the component |
| 07/27/2005 | EP1557553A1 Monobloc arm for a postcombustion device of a double flow turboengine |
| 07/27/2005 | CA2764342A1 Side-fed shielded internal fuel manifold inlet tube |
| 07/26/2005 | US6921034 Fuel nozzle assembly |
| 07/26/2005 | US6921014 Method for forming a channel on the surface of a metal substrate |
| 07/26/2005 | US6920762 Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner |
| 07/26/2005 | US6920758 Gas turbine and the combustor thereof |
| 07/21/2005 | US20050158511 Conductor can be operatively connected to a power source to form an electrical circuit, resistance across the conductor can be measured, as component contacts a second component, the component can begin to wear, once the wear progresses to the conductor, changes in the measured resistance can result |
| 07/21/2005 | US20050155351 Combustion chamber with flameless oxidation |
| 07/21/2005 | US20050155339 Rotary combustor, and electricity generator comprising such a combustor |
| 07/21/2005 | US20050155224 Method of forming a fuel feed passage in the feed arm of a fuel injector |
| 07/20/2005 | EP1555484A2 Process to operate a gas turbine combustor |
| 07/20/2005 | EP1555443A1 Attachment device for turbine combustor liner |
| 07/20/2005 | EP1555407A1 Method and system for controlling gas turbine engine |
| 07/20/2005 | EP1554524A1 A fuel injector |
| 07/19/2005 | US6918256 Method for the reduction of combustion-driven oscillations in combustion systems and premixing burner for carrying out the method |
| 07/14/2005 | WO2005064239A1 Combustion system with low polluting emissions |
| 07/14/2005 | WO2005064232A1 Thermal power plant with sequential combustion and reduced co2 emissions and method for operating a plant of this type |
| 07/14/2005 | US20050150632 Extended impingement cooling device and method |
| 07/14/2005 | US20050150233 Attachment device for turbin combustor liner |
| 07/14/2005 | US20050150231 Control of gas turbine for catalyst activation |
| 07/14/2005 | DE102004057985A1 Gas-turbine combustion apparatus for use in vehicle, has turbine bypass mechanism has a shut-off valve which controls displacement of exhaust by the circular pipe out of the compartment through the exhaust gas opening material |
| 07/14/2005 | CA2550675A1 Thermal power plant with sequential combustion and reduced-co2 emission, and a method for operating a plant of this type |
| 07/13/2005 | EP1553345A2 Control of gas turbine for catalyst activation |
| 07/13/2005 | EP1553344A2 Fuel system |
| 07/13/2005 | EP1553343A1 Method for reduction of combustor dynamic pressure during operation of gas turbine engines |
| 07/13/2005 | EP1552132A1 Turbine engine apparatus and method |
| 07/13/2005 | EP1466037B1 High-temperature protective coating |
| 07/13/2005 | CN1639512A 燃气轮机 Gas turbine |
| 07/13/2005 | CN1637347A A rotary combustor, and electrical generator comprising a combustor of this type |
| 07/13/2005 | CN1637346A A rotary combustor, and electrical generator comprising a combustor of this type |
| 07/13/2005 | CN1637345A Rotary combustor, and electricity generator comprising such a combustor |
| 07/13/2005 | CN1637261A Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith |
| 07/13/2005 | CN1637248A Apparatus and methods for minimizing and/or eliminating dilution air leakage in a combustion liner assembly |
| 07/13/2005 | CN1637247A Extended impingement cooling device and method |
| 07/12/2005 | US6915637 Gas turbine combustor |
| 07/12/2005 | US6915636 Dual fuel fin mixer secondary fuel nozzle |
| 07/07/2005 | WO2005061964A1 Helical channel fuel distributor and method |
| 07/07/2005 | US20050144955 Method and apparatus for reduction of combustor dynamic pressure during operation of gas turbine engines |
| 07/07/2005 | US20050144954 Apparatus and methods for minimizing and/or eliminating dilution air leakage in a combustion liner assembly |
| 07/07/2005 | US20050144953 Flow sleeve for a law NOx combustor |
| 07/07/2005 | US20050144952 Helical channel fuel distributor and method |
| 07/07/2005 | US20050144950 Gas turbine |
| 07/07/2005 | US20050144929 Device for a combustion chamber of a gas turbine |
| 07/07/2005 | DE4325802B4 Verfahren zum Betrieb einer Gasturbinenanlage mit flüssigem oder gasförmigem Brennstoff A method of operating a gas turbine plant with liquid or gaseous fuel |
| 07/07/2005 | DE10348447A1 Assembly and maintenance platform for a gas turbine esp. a stationary gas turbine with a walk in flame tube where the platform can be disassembled |
| 07/07/2005 | DE102004052433A1 Gasturbinen-Steuer- bzw. Regelungsvorrichtung, Gasturbinensystem und Gasturbinensteuer- bzw. Regelungsverfahren Gas turbine control or control apparatus, gas turbine system and Gasturbinensteuer- or regulatory procedure |
| 07/06/2005 | EP1550644A1 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
| 07/06/2005 | EP1549881A2 System for vaporization of liquid fuels for combustion and method of use |
| 07/06/2005 | EP1549880A2 Combustion method and apparatus |
| 07/06/2005 | EP1549782A1 A thermal barrier coating and a method of applying such a coating |
| 07/06/2005 | EP1165941B1 High temperature erosion resistant, abradable thermal barrier composite coating |
| 07/06/2005 | CN1209553C Fuel injector with replaceable sensor |
| 07/05/2005 | US6912854 Gas turbine combustor |
| 07/05/2005 | US6912838 Coated crossfire tube assembly |
| 07/05/2005 | US6912782 Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engine |
| 06/30/2005 | WO2005059442A1 Combustor for gas turbine |
| 06/30/2005 | WO2005059441A1 A system for damping thermo-acoustic instability in a combustor device for a gas turbine |
| 06/30/2005 | US20050142395 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
| 06/30/2005 | US20050139695 Fuel supply method and fuel supply system for fuel injection device |
| 06/30/2005 | US20050139694 Fuel supply method and fuel supply system |
| 06/30/2005 | US20050138931 Bulkhead panel for use in a combustion chamber of a gas turbine engine |
| 06/29/2005 | EP1548365A2 Rotary combustor, and electricity generator comprising such a combustor |
| 06/29/2005 | EP1548364A2 A rotary combustor, and electrical generator comprising a combustor of this type |
| 06/29/2005 | EP1548363A2 Rotary combuster, and electricity generator comprising such a combuster |
| 06/29/2005 | EP1548362A1 Fuel supply method and fuel supply system for fuel injection device |
| 06/29/2005 | EP1548361A1 Fuel supply method and fuel supply system |
| 06/29/2005 | EP1548266A1 Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith |
| 06/29/2005 | EP1546527A1 Nested channel ducts for nozzle construction and the like |
| 06/29/2005 | CN1633554A Ejector based engines |
| 06/28/2005 | US6910853 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion |