| 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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| 12/12/2001 | EP1162346A2 Cooling for turbine shroud segments |
| 12/12/2001 | EP1162286A1 A method for removing a coating from a substrate |
| 12/12/2001 | EP1161622A1 Method of operation of a gas turbine engine power plant and a gas turbine engine power plant |
| 12/12/2001 | EP1090222B1 Driving mechanism with counter-rotating rotors |
| 12/12/2001 | EP0941383B1 Manufacture of paper |
| 12/12/2001 | EP0865593B1 Improved method and apparatus for the destruction of volatile organic compounds |
| 12/12/2001 | CN1076140C Electrical system for turbin/alternator on common shaft |
| 12/11/2001 | US6329633 Method and material for processing a component for laser machining |
| 12/11/2001 | US6328526 Gas turbine starting method |
| 12/11/2001 | US6328311 Dual-contact brush seal |
| 12/11/2001 | US6328293 Multi-linkage suspension system including outboard isolators |
| 12/11/2001 | US6328258 Air intake structure for aircraft engine |
| 12/11/2001 | US6328056 Proportional bypass valve with dual variable orifice |
| 12/11/2001 | US6327857 Device, method and application in connection with a turbomachine and pumping and lubricating arrangement in connection with such a machine |
| 12/11/2001 | CA2256597C Steam cooled type gas turbine |
| 12/06/2001 | WO2001092702A1 Integrated gas compressor |
| 12/06/2001 | WO2001092701A1 Heat engines and associated methods of producing mechanical energy and their application to vehicles |
| 12/06/2001 | WO2001057364A8 Frangible cover for turbofan engine blade removal and access |
| 12/06/2001 | US20010048876 Casing structure of metal construction |
| 12/06/2001 | US20010047763 Masking fixture and method |
| 12/06/2001 | US20010047651 Device for supplying seal air to bearing boxes of a gas turbine engine |
| 12/06/2001 | US20010047650 Method of operating a gas-turbine chamber with gaseous fuel |
| 12/06/2001 | US20010047649 Method and apparatus for power augmentation for gas turbine power cycles |
| 12/06/2001 | US20010047648 Turbo-machines |
| 12/06/2001 | US20010047646 Apparatus and methods of reheating gas turbine cooling steam and hp steam turbine exhaust in a combined cycle power generating system |
| 12/06/2001 | CA2410952A1 Heat engines and associated methods of producing mechanical energy and their application to vehicles |
| 12/05/2001 | EP1160551A1 Sensors and methodology for improved turbine exhaust gas temperature measurements |
| 12/05/2001 | EP1160418A2 Steam exit flow design for aft cavities of an airfoil |
| 12/05/2001 | EP0960308B1 Gas turbine installation with a ceramic-covered combustion chamber housing |
| 12/04/2001 | US6324828 Gas turbine engine and a method of controlling a gas turbine engine |
| 12/04/2001 | US6324827 Method of generating power in a dry low NOx combustion system |
| 11/29/2001 | WO2001051787A8 Piloted airblast lean direct fuel injector |
| 11/29/2001 | US20010046441 Axial thermal medium delivery tubes and retention plates for a gas turbine rotor |
| 11/29/2001 | DE10026121A1 Vorrichtung zur Dämpfung akustischer Schwingungen in einer Brennkammer Apparatus for damping acoustic vibrations in a combustion chamber |
| 11/28/2001 | EP1158247A2 Apparatus to reduce acoustic vibrations in a combustion chamber |
| 11/28/2001 | EP1158246A2 Retainer segment for swirler assembly |
| 11/28/2001 | EP1158142A2 Reducing cracking adjacent shell flange connecting bolts |
| 11/28/2001 | EP1158140A2 Exit joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles |
| 11/28/2001 | EP1156962A2 Tangentially directed acoustic jet controlling boundary layers |
| 11/28/2001 | EP0852665B1 Mounting for sound-absorbing members |
| 11/28/2001 | EP0764267B1 Method for measuring and extending the service life of fatigue-limited metal components |
| 11/28/2001 | CN1324433A Gas turbine engine |
| 11/27/2001 | US6323625 Turbine/alternator on a common shaft with an associated electrical system |
| 11/27/2001 | US6322897 Metal-ceramic gradient material, product made from a metal-ceramic gradient material and process for producing a metal-ceramic gradient material |
| 11/27/2001 | US6322353 Ignition appliance for a heat generator |
| 11/27/2001 | US6321539 Retrofit equipment for reducing the consumption of fossil fuel by a power plant using solar insolation |
| 11/27/2001 | US6321528 Turbine, for a liquid-propellant rocket engine mainly |
| 11/27/2001 | US6321526 Gas turbine starting control system |
| 11/27/2001 | US6321447 Concentric wrench for blind access opening in a turbine |
| 11/22/2001 | WO2001088361A1 Recuperator for use with turbine/turbo-alternator |
| 11/22/2001 | WO2001088354A2 Device for controlling the cooling flows of gas turbines |
| 11/22/2001 | WO2001088342A1 Method and apparatus for power augmentation for gas turbine power cycles |
| 11/22/2001 | WO2001087528A2 Welding superalloy articles |
| 11/22/2001 | US20010042381 Heat and electric power supply system and operation method thereof |
| 11/22/2001 | US20010042375 Gas turbine combustor |
| 11/22/2001 | US20010042367 Method for operating a power plant including a co2 process |
| 11/22/2001 | DE10022967A1 Liquid cooled exhaust gas turbocharger with independent cooling system with pump driven by electric motor rather than engine |
| 11/22/2001 | CA2407609A1 Recuperator for use with turbine/turbo-alternator |
| 11/21/2001 | EP1156281A2 Gas turbine combustor |
| 11/21/2001 | EP1156188A2 A leaf seal for gas turbine stator shrouds and a nozzle band |
| 11/21/2001 | EP1156187A2 Nozzle cavity insert having impingement and convection cooling regions |
| 11/21/2001 | EP1156186A2 Film cooling air pocket in a closed loop cooled airfoil |
| 11/21/2001 | EP1155225A1 Combustion unit for combusting a liquid fuel and a power generating system comprising such combustion unit |
| 11/21/2001 | EP1154876A1 Repair of turbine exhaust case |
| 11/21/2001 | EP0928396B1 Thermal shield component with cooling fluid recirculation and heat shield arrangement for a component circulating hot gas |
| 11/20/2001 | US6319304 For separating the heavier-than-air particulate debris out of an air stream drawn into the device and ejecting the debris back outside |
| 11/20/2001 | US6318963 Gas turbine airfoil internal air system |
| 11/20/2001 | US6318958 Air turbine starter with seal assembly |
| 11/20/2001 | US6318089 Gas turbine inlet air cooling system |
| 11/20/2001 | US6318066 Heat exchanger |
| 11/20/2001 | US6318065 System for chilling inlet air for gas turbines |
| 11/15/2001 | WO2001086122A1 Method and device for cooling the inflow area of the shaft of a steam turbine |
| 11/15/2001 | US20010039796 Method of and apparatus for generating power |
| 11/15/2001 | US20010039794 Methods for operating gas turbine engines |
| 11/15/2001 | DE10023411A1 Wideband sound-absorbing element for channel carrying fluid has first part with low-frequency resonators formed by walls with different resonant frequencies, second with high-frequency resonators |
| 11/14/2001 | EP1154252A1 Temperature measuring system and optical switch used therein |
| 11/14/2001 | EP1154137A2 Monitoring arrangement to determine the status of a valve in a fuel supply system |
| 11/14/2001 | EP1154136A2 Method and apparatus to cool the cooling air for turbine engines |
| 11/14/2001 | EP1154135A2 Methods and apparatus for supplying cooling air to turbine engines |
| 11/14/2001 | EP1154126A2 Closed circuit steam cooled turbine shroud |
| 11/14/2001 | EP1153699A2 Blisk weld repair |
| 11/14/2001 | EP1153681A1 System for casting a metal article using a fluidized bed |
| 11/14/2001 | EP1153204A1 Improved bushing for a jet engine vane |
| 11/14/2001 | EP1153157A1 Thermal barrier coating resistant to sintering |
| 11/14/2001 | EP1152851A1 Die casting of high temperature material |
| 11/14/2001 | EP1152848A1 Method and apparatus for production of a cast component |
| 11/14/2001 | EP1080300B1 Recuperator for gas turbine engine |
| 11/14/2001 | EP1073832B1 Turbine engine with cooled p3 air to impeller rear cavity |
| 11/14/2001 | CN1321825A Method and device for reducing exhaust of gas turbine |
| 11/13/2001 | US6316841 Integrated emergency power and environmental control system |
| 11/13/2001 | US6315518 Stationary blade of gas turbine |
| 11/13/2001 | US6315301 Seal apparatus for rotary machines |
| 11/13/2001 | US6314998 Fuel divider and ecology system for a gas turbine engine |
| 11/13/2001 | US6314719 Ignition system for a propulsion producing engine |
| 11/13/2001 | US6314717 Electricity generating system having an annular combustor |
| 11/13/2001 | US6314715 Modified fuel gas turbo-expander for oxygen blown gasifiers and related method |
| 11/08/2001 | WO2001083965A1 Fuel injection system for a gas turbine |
| 11/08/2001 | WO2001083964A1 Oxygen separation method integrated with gas turbine |
| 11/08/2001 | WO2001083297A2 Aircraft gas turbine engine having a centrifuge |
| 11/08/2001 | WO2001038727A3 Induction static start for a turbine generator with a brushless exciter and associated methods |