| 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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| 10/03/2002 | WO2002078011A1 A nuclear power plant and a method of operating the same |
| 10/03/2002 | WO2002078010A1 A nuclear power plant and method of operating the same |
| 10/03/2002 | WO2002077515A1 Electric power leveling method and methane hydrate cold-heat utilization power generating system in gas supply business |
| 10/03/2002 | WO2002077500A1 Rotary machine with seal |
| 10/03/2002 | WO2002057632A3 High pressure water pump |
| 10/03/2002 | WO2002053894A3 Installation for the generation of energy |
| 10/03/2002 | WO2002042623A3 Fan-stator interaction tone reduction |
| 10/03/2002 | WO2002042610A3 Metallic honeycomb cellular seal-structure for a turbomachine |
| 10/03/2002 | WO2001027444A9 Bearing housing for a turbomachine |
| 10/03/2002 | US20020142474 Generating test library; obtain substrate, expose to test impurities, monitor activity of test compound on substrate |
| 10/03/2002 | US20020141882 Method and apparatus for increasing the efficiency of a multi-stage compressor |
| 10/03/2002 | US20020141859 Gas turbine engine blade containment assembly |
| 10/03/2002 | US20020139120 Tortuous path quiet exhaust eductor system |
| 10/03/2002 | US20020139105 Gas turbine |
| 10/03/2002 | CA2431556A1 A nuclear power plant and method of operating the same |
| 10/02/2002 | EP1245806A1 Cooled gas turbine balde |
| 10/02/2002 | EP1245805A2 Supercharged gas turbine |
| 10/02/2002 | EP1245804A1 Gas turbine |
| 10/02/2002 | EP1245794A2 A gas turbine engine blade containment assembly |
| 10/02/2002 | EP1245785A1 Turbine airfoil and manufacturing method therefor |
| 10/02/2002 | EP1245327A1 Filler powder for diffusion-brazing of nickel-, cobalt- or iron-based workpieces |
| 10/02/2002 | EP1244881A1 Brush seals |
| 10/02/2002 | EP1244870A1 Silencer for the compressor of an exhaust gas turbocharger |
| 10/02/2002 | EP1000224B1 Distribution of cooling air in a turbine stage of a gas turbine |
| 10/02/2002 | EP0998361B1 Turbine blade and use of a known method for producing such a turbine blade |
| 10/02/2002 | DE10101070C1 Verfahren zum Gasphasendiffusionsbeschichten von metallischen Bauteilen Method for gas phase diffusion coating of metal components |
| 10/02/2002 | CN1372502A Method and device for treating the surface of part |
| 10/01/2002 | US6457939 Profiled surface used as an abradable in flow machines |
| 10/01/2002 | US6457936 Inner shell radial pin geometry and mounting arrangement |
| 10/01/2002 | US6457934 Connector tube for a turbine rotor cooling circuit |
| 10/01/2002 | US6457933 Methods and apparatus for controlling bearing loads within bearing assemblies |
| 10/01/2002 | US6457676 Method and apparatus for aircraft inlet ice protection |
| 10/01/2002 | US6457450 Ju. M. Luzhkov rotary-turbine internal combustion engine |
| 10/01/2002 | US6457315 Hybrid refrigeration cycle for combustion turbine inlet air cooling |
| 09/29/2002 | CA2378632A1 Powder used in diffusion brazing of nickel, cobalt or iron alloys |
| 09/26/2002 | WO2002074621A1 Plenum entry bulk swirl generator |
| 09/26/2002 | WO2002048509A9 A turbine arrangement and a method of operating a turbine arrangement |
| 09/26/2002 | WO2002027167A3 Compressed air steam generator for use in cooling a combustion turbine transition section |
| 09/26/2002 | WO2001020149A9 Methods of igniting a catalytic converter |
| 09/26/2002 | US20020136659 Rotor for a turbomachine, and process for producing a rotor of this type |
| 09/26/2002 | US20020136638 Pre-segmented squealer tip for turbine blades |
| 09/26/2002 | US20020136631 Methods and apparatus for maintaining rotor assembly tip clearances |
| 09/26/2002 | US20020134886 Separate boundary layer engine inlet |
| 09/26/2002 | US20020134085 Process for the operation of a gas turbine plant and related gas turbine plant |
| 09/26/2002 | US20020133949 Recuperator cell assembly procedure |
| 09/26/2002 | DE10211039A1 Verfahren zum Behandeln eines keramischen Kerns A method of treating a ceramic core |
| 09/26/2002 | DE10114612A1 Rotor für eine Turbomaschine sowie Verfahren zur Herstellung eines solchen Rotors Rotor for a turbomachine, as well as method for the production of such a rotor |
| 09/25/2002 | EP1243782A2 Double jet engine inlet |
| 09/25/2002 | EP1243757A1 Process for operating a power plant |
| 09/25/2002 | EP1243756A1 Turbine |
| 09/25/2002 | EP1243754A2 Turbomachine rotor and method of manufacture therefor |
| 09/25/2002 | EP1243630A2 Carbon resistant surface coating |
| 09/25/2002 | EP1242990A1 Fan and compressor noise attenuation |
| 09/25/2002 | EP1242729A1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method |
| 09/25/2002 | EP1204450A4 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 |
| 09/24/2002 | US6455122 Heat-resisting fiber-reinforced composite material and manufacturing method thereof |
| 09/24/2002 | US6454529 Methods and apparatus for maintaining rotor assembly tip clearances |
| 09/24/2002 | US6453674 Method of operation of gas turbine engine |
| 09/24/2002 | US6453673 Method of cooling gas only nozzle fuel tip |
| 09/24/2002 | US6453660 Combustor mixer having plasma generating nozzle |
| 09/24/2002 | US6453659 Device for compressing a gaseous medium and systems comprising such device |
| 09/24/2002 | US6453658 Multi-stage multi-plane combustion system for a gas turbine engine |
| 09/24/2002 | US6453557 Method of joining a vane cavity insert to a nozzle segment of a gas turbine |
| 09/23/2002 | CA2376832A1 Carbon resistant surface coating |
| 09/19/2002 | WO2002073089A1 Air assist fuel nozzle |
| 09/19/2002 | WO2002072287A1 Forced mist cleaning of combustion turbines |
| 09/19/2002 | WO2002059474A3 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes |
| 09/19/2002 | US20020132131 Protective coating for a thermally stressed component, particularly a turbine component |
| 09/19/2002 | US20020131862 Plenum entry bulk swirl generator |
| 09/19/2002 | US20020129925 Method for treating ceramic cores |
| 09/19/2002 | US20020129837 Preparing aqueous cleaning solution for removing contaminants produced during combustion and deposited on internal surfaces of combustion and turbine sections without harming internal surfaces; driving mist through combustion and turbine |
| 09/19/2002 | US20020129608 Compressor discharge bleed air circuit in gas turbine plants and related method |
| 09/19/2002 | DE10112864A1 Verfahren zum Zünden einer thermischen Turbomaschine Method for igniting a thermal turbomachine |
| 09/18/2002 | EP1241334A1 Ignition method for a turbomachine |
| 09/18/2002 | EP1240713A2 Combustion control method and system |
| 09/18/2002 | EP0968317B1 Method of forming internal passages within articles and articles formed by same |
| 09/18/2002 | CN1091211C Gas and steam turbine system, and refrigeration of coolant indended for gas turbine in such system |
| 09/17/2002 | US6450768 Axial thermal medium delivery tubes and retention plates for a gas turbine rotor |
| 09/17/2002 | US6450766 Stator vane blank and method of forming the vane blank |
| 09/17/2002 | US6450763 Replaceable variable stator vane for gas turbines |
| 09/17/2002 | US6450759 Gas turbine nozzle vane insert and methods of installation |
| 09/17/2002 | US6450758 Cooling system for a bearing of a turbine rotor |
| 09/17/2002 | US6449957 Gas turbine generator plant with equipment support |
| 09/17/2002 | US6449955 Method for filling fuel gas in a gas turbine |
| 09/17/2002 | US6449953 Methods for reducing gas turbine engine emissions |
| 09/12/2002 | WO2002070867A1 Methods and apparatus for cooling gas turbine engine blade tips |
| 09/12/2002 | WO2002070772A1 Method for plasma coating a turbine blade and coating device |
| 09/12/2002 | WO2002053900A3 Fluid and fuel delivery system reducing pressure fluctuations |
| 09/12/2002 | US20020128422 Mixable room temperature castable polyurethane system |
| 09/12/2002 | US20020127112 Enhanced coating system for turbine airfoil applications |
| 09/12/2002 | US20020125336 Air assist fuel nozzle |
| 09/12/2002 | US20020125215 Chemical milling of gas turbine engine blisks |
| 09/12/2002 | US20020125067 Method for producing a panel comprising an adapted acoustically resistive layer and panel so obtained |
| 09/12/2002 | US20020124991 Low cost high efficiency automotive turbines |
| 09/12/2002 | US20020124579 Combustion gas turbine engine integrated modular temperature cooling and heating process and apparatus |
| 09/12/2002 | US20020124571 Foil bearing rotary flow compressor with control valve |
| 09/12/2002 | US20020124570 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades |
| 09/12/2002 | US20020124569 Bimetallic high temperature recuperator |
| 09/12/2002 | US20020124402 Method for extending the life of attachments that attach blades to a rotor |
| 09/12/2002 | DE10126632A1 Combination propulsion system pref. for aircraft has thrust vector control, also useable as lifting device, located behind multistage vacuum system or ram jet engines |