| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 05/30/2002 | US20020062639 Steam cooling apparatus for gas turbine |
| 05/30/2002 | US20020062544 Method of modifying cooled turbine components and modified component |
| 05/29/2002 | EP1209348A1 Silencing device, particularly for turbocharged engine |
| 05/29/2002 | EP1209338A1 Dosing device having an optimized setting |
| 05/29/2002 | EP1209325A2 Steam cooling apparatus for gas turbine |
| 05/29/2002 | EP1209324A2 Seal structure for a cooling steam passage in a gas turbine |
| 05/29/2002 | EP1208942A1 Peening of cooled turbine blade tip |
| 05/29/2002 | EP1208295A2 Integrated bleed air and engine starting system (ibaness) |
| 05/29/2002 | EP1208294A1 Method and device for increasing the pressure of a gas |
| 05/29/2002 | EP1208293A1 A method and apparatus for vaporizing liquid gas in a combined cycle power plant |
| 05/29/2002 | EP0951614B1 Cooling system for gas turbine vane |
| 05/28/2002 | US6394755 Enhanced coating system for turbine airfoil applications |
| 05/28/2002 | US6394749 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 05/28/2002 | US6393829 Coolant recovery type gas turbine |
| 05/28/2002 | US6393828 Protective coatings for turbine combustion components |
| 05/28/2002 | US6393827 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 05/28/2002 | US6393826 Gas turbine |
| 05/28/2002 | US6393825 System for pressure modulation of turbine sidewall cavities |
| 05/28/2002 | US6393823 Methods for fuel nozzle staging for gas turbine engines |
| 05/28/2002 | US6393822 Cooling steam supply method of a combined cycle power generation plant |
| 05/28/2002 | US6393821 Method for collection and use of low-level methane emissions |
| 05/28/2002 | CA2089278C Gas turbine engine cooling system |
| 05/28/2002 | CA2070440C Heat shield mechanism for turbine engines |
| 05/28/2002 | CA2061939C Cooled shroud support |
| 05/23/2002 | WO2002040884A1 Rotary machine with axial stop incorporating a current generator |
| 05/23/2002 | WO2001058004A3 Combustion control method and system |
| 05/23/2002 | US20020061485 Combustor |
| 05/23/2002 | US20020061110 Actively-controlled sound absorption panel system using movement-controlled reflective plate |
| 05/23/2002 | US20020059869 Spraying with water jet, nozzles |
| 05/23/2002 | US20020059799 Fuel injector with an optimized metering device |
| 05/23/2002 | US20020059791 Combustion system and method |
| 05/23/2002 | DE10056243A1 Brennkammer und Verfahren zum Betrieb dieser Brennkammer Combustor and method of operation of this combustion chamber |
| 05/23/2002 | DE10049205A1 Process for supplying fuel to a premix burner for operating a gas turbine comprises introducing premix gas separately via two axially divided regions along the burner shell |
| 05/22/2002 | EP1207350A2 Combustor and method for operating the same |
| 05/22/2002 | EP1207344A2 Combustor |
| 05/22/2002 | EP1207273A2 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
| 05/22/2002 | EP1207272A2 Replaceable variable stator vane for gas turbines |
| 05/22/2002 | EP1207270A2 Repairing method for a turbine nozzle segment |
| 05/22/2002 | EP1207268A1 Gas turbine blade and a process for manufacturing a gas turbine blade |
| 05/22/2002 | EP1207013A1 Method for increasing the service life of rotor blade locking means |
| 05/22/2002 | EP1207005A1 Heat treatment of weld repaired gas turbine engine components |
| 05/22/2002 | EP1206973A2 Methods and apparatus for injecting water into gas turbine engines |
| 05/22/2002 | EP1206634A1 Supercharging system for gas turbines |
| 05/22/2002 | EP1206384A2 Supersonic external-compression diffuser and method for designing same |
| 05/22/2002 | EP1206383A1 Air intake protection device for aircraft engines |
| 05/21/2002 | US6391479 Coating interlayer for improved compatibility between HR-120 and aluminum-containing oxidation resistant metallic coatings |
| 05/21/2002 | US6391115 Underplatform coating tool |
| 05/21/2002 | US6390774 Gas turbine bucket cooling circuit and related process |
| 05/21/2002 | US6390769 Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud |
| 05/21/2002 | US6390476 Heat-resistant magnetic silicone rubber brush seals in turbomachinery and methods of application |
| 05/21/2002 | US6390418 Tangentially directed acoustic jet controlling boundary layer |
| 05/21/2002 | US6390414 Self-adjusting air intake |
| 05/21/2002 | US6389815 Fuel nozzle assembly for reduced exhaust emissions |
| 05/21/2002 | US6389813 Passive mounted lining system |
| 05/21/2002 | US6389800 Apparatus for fuel nozzle staging for gas turbine engines |
| 05/21/2002 | US6389799 Gas turbine Installation |
| 05/21/2002 | US6389797 Gas turbine combined cycle system |
| 05/21/2002 | US6389796 Gas turbine system and combined plant comprising the same |
| 05/21/2002 | US6389795 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 05/21/2002 | US6389794 Method and apparatus for fuel gas moisturization and heating |
| 05/21/2002 | US6389793 Combustion turbine cooling media supply system and related method |
| 05/21/2002 | US6389792 Combustor rear facing step hot side contour method |
| 05/16/2002 | WO2002039045A2 Annular recuperator |
| 05/16/2002 | WO2002038938A1 Bypass gas turbine engine and cooling method for working fluid |
| 05/16/2002 | WO2002038926A1 Fuel gas moisturization system level control |
| 05/16/2002 | WO2001070424A3 Methods and apparatus for retrofitting compressible flanges |
| 05/16/2002 | US20020056994 Open air filter cooling system for gas turbine inlet cooling |
| 05/16/2002 | US20020056303 Method and apparatus for peening tops of cooled blades |
| 05/16/2002 | DE10052023C1 Austenitische Nickel-Chrom-Cobalt-Molybdän-Wolfram-Legierung und deren Verwendung Austenitic nickel-chromium-cobalt-molybdenum-tungsten alloy and the use thereof |
| 05/16/2002 | CA2361978A1 Gas turbine blade and method for manufacturing a gas turbine blade |
| 05/15/2002 | EP1205736A2 System and method for direct non-intrusive measurement of corrected airflow |
| 05/15/2002 | EP1205641A2 Combined cycle gas turbine system |
| 05/15/2002 | EP1205640A2 Combined system for cooling by water injection and washing of a gas turbine compressor |
| 05/15/2002 | EP1205637A1 Cooling device for stator ring |
| 05/15/2002 | EP1205635A2 Gas injector system and its fabrication |
| 05/15/2002 | EP1204818A1 Efficiency enhanced turbine engine |
| 05/15/2002 | EP1204776A1 High-temperature part and method for producing the same |
| 05/15/2002 | EP1204532A2 One-step noble metal-aluminide coatings |
| 05/15/2002 | EP1204450A1 Powered low restriction air precleaner device and method for providing a clean air flow to an apparatus such as a combustion engine air intake, engine cooling system, ventilation system and cab air intake system |
| 05/14/2002 | US6387527 Article comprising metal-based substrate and foil which comprises at least one bond coating fused to substrate by intervening layer of braze material |
| 05/14/2002 | US6386825 Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment |
| 05/14/2002 | US6386763 Bushing for a jet engine vane |
| 05/14/2002 | US6385987 Heat exchanger for cooling and for a pre-cooler for turbine intake air conditioning |
| 05/14/2002 | US6385975 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 05/14/2002 | US6385962 Fuel divider and ecology system for a gas turbine engine |
| 05/14/2002 | US6385961 Purging air supply system for a gas turbine |
| 05/14/2002 | US6385960 Methods and apparatus for operation of gas turbines |
| 05/14/2002 | US6385958 Method for pressure modulation of turbine sidewall cavities |
| 05/14/2002 | CA2263029C Cooling structure around l-shaped vertical type gas turbine output shaft |
| 05/10/2002 | WO2002037046A2 Turbogenerator cooling system |
| 05/10/2002 | WO2002036951A1 Fan noise reduction by control of nacelle inlet throat |
| 05/10/2002 | WO2002036950A2 Compliant brush shroud assembly for gas turbine engine compressors |
| 05/09/2002 | US20020053837 Stator ring ventilation assembly |
| 05/09/2002 | US20020053208 Fuel divider and ecology system for a gas turbine engine |
| 05/08/2002 | EP1203866A2 Apparatus and methods for controlling the supply of water mist to a gas-turbine compressor |
| 05/08/2002 | EP1203104A2 Superalloys with improved weldability for high temperature applications |
| 05/08/2002 | EP1068161B1 Use of high temperature insulation for ceramic matrix composites in gas turbines |
| 05/08/2002 | CN1348528A Method of operation of a gas turbine engine power plant and a gas turbine enging power plant |
| 05/07/2002 | US6383602 Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
| 05/07/2002 | US6383570 Thermal barrier coating system utilizing localized bond coat and article having the same |