| 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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| 06/15/2005 | CN1626629A Method of inhibiting deposit formation in a jet fuel at high temperatures |
| 06/15/2005 | CN1206449C Turnine and its operation method |
| 06/15/2005 | CA2489655A1 Mounting of the rotor of a gas turbine |
| 06/14/2005 | US6906479 Gas turbine engine starter generator with multiple windings on each exciter stator pole |
| 06/14/2005 | US6906432 Electrical power generation system and method |
| 06/14/2005 | US6905559 Nickel-base superalloy composition and its use in single-crystal articles |
| 06/14/2005 | US6905308 Turbine nozzle segment and method of repairing same |
| 06/14/2005 | US6905302 Network cooled coated wall |
| 06/14/2005 | US6904756 Transition duct support bracket wear cover |
| 06/14/2005 | US6904747 Heat exchanger for power generation equipment |
| 06/14/2005 | US6904676 Methods for replacing a portion of a combustor liner |
| 06/11/2005 | CA2490759A1 Thermal gas compression engine |
| 06/09/2005 | WO2005052450A1 Method for determining fluctuating fuel properties during the operation of a power plant |
| 06/09/2005 | WO2005040580A3 Fluid-cooled mechanical face seal rotor |
| 06/09/2005 | US20050121916 Integrated microturbine gearbox generator assembly |
| 06/09/2005 | US20050121905 Sealing device for connection of a pipe in a hole |
| 06/09/2005 | US20050121532 System and method for district heating with intercooled gas turbine engine |
| 06/09/2005 | US20050120719 Internally insulated turbine assembly |
| 06/09/2005 | US20050120717 Fuel injection method and apparatus for a combustor |
| 06/09/2005 | US20050120699 Heat recovery apparatus with aerodynamic diffusers |
| 06/09/2005 | DE102004054294A1 Kühlsystem für Plattformkanten von Leitradsegmenten Cooling system for platform edges of nozzle segments |
| 06/08/2005 | EP1538318A1 System and method for district heating with intercooled gas turbine engine |
| 06/08/2005 | EP1538306A1 Joining device between a vane and its cooling fluid supply in a turbomachine |
| 06/08/2005 | EP1538305A2 Airfoil with variable density array of pedestals at the trailing edge |
| 06/08/2005 | EP1537363A1 Gas turbine |
| 06/08/2005 | EP1537349A1 Multidirectional turbine shim seal |
| 06/08/2005 | EP1537296A1 Gas turbine sealing air supply system |
| 06/08/2005 | EP1537248A1 Producing metallic articles by reduction of nonmetallic precursor compounds and melting |
| 06/08/2005 | CN1625648A Equipment and method for cooling combustion turbine inlet air using liquid hydrocarbon fuel |
| 06/08/2005 | CN1624307A Cooling system for high-temperature unit of aircraft engine and aircraft engine mounted with the system |
| 06/07/2005 | US6902692 Process for making a fiber reinforced article |
| 06/07/2005 | US6902633 A castable and weldable nickel-base superalloy that exhibits desirable properties suitable for gas turbine engine applications |
| 06/07/2005 | US6902371 Internal low pressure turbine case cooling |
| 06/07/2005 | US6902096 Method of joining material |
| 06/07/2005 | US6901761 System and method for regulating pressure of pilot air to combustor of gas turbine |
| 06/07/2005 | US6901759 Method for operating a partially closed, turbocharged gas turbine cycle, and gas turbine system for carrying out the method |
| 06/07/2005 | US6901737 Air intake for an auxiliary power unit in an aircraft |
| 06/07/2005 | US6901736 Gas turbine electric power generation equipment and air humidifier |
| 06/07/2005 | US6901735 Modular fuel conditioning system |
| 06/05/2005 | CA2488434A1 System and method for district heating with intercooled gas turbine engine |
| 06/02/2005 | US20050118331 Depositing ceramic particles to fix spalling in barrier coatings, using yttritia and zirconia with nickel for turbines |
| 06/02/2005 | US20050118023 Hot gas path component with mesh and impingement cooling |
| 06/02/2005 | US20050118016 Gas turbine arrangement |
| 06/02/2005 | US20050116689 Method and apparatus for starting a gas turbine using a polyphase electric power generator |
| 06/02/2005 | US20050116114 Normally open reverse flow flapper valve |
| 06/02/2005 | US20050116061 Method and apparatus for arresting a crack within a body |
| 06/02/2005 | DE202004000929U1 Air inlet housing for induction side of combustion engine, especially gas turbine, has arrangements for sound damping that operate on absorption and resonance principles arranged between sound inlet and outlet openings |
| 06/01/2005 | EP1536222A2 Methods and apparatus for evaluating rotary machinery |
| 06/01/2005 | EP1536102A2 Rotor for a steam turbine |
| 06/01/2005 | EP1536101A2 Turbine drum rotor for a turbine engine and method of installation |
| 06/01/2005 | EP1535839A1 Underwing aircraft engine mounting structure |
| 06/01/2005 | EP1534936A1 Fan case design with metal foam between kevlar |
| 06/01/2005 | EP1534934A1 Method for manufacturing a stator component |
| 06/01/2005 | EP1534878A1 Highly oxidation resistant component |
| 06/01/2005 | EP1272736A4 Turbine engine foreign object damage detection system |
| 06/01/2005 | CN1623031A Method for operating a turbine group |
| 06/01/2005 | CN1622446A Method and apparatus for starting a gas turbine using a polyphase electric power generator |
| 06/01/2005 | CN1621671A Method and device for monitoring gas turbine combustion dynamics |
| 06/01/2005 | CN1204335C Operation method for combined circular electricity generator |
| 05/31/2005 | US6899926 Alloy coating, method for forming the same, and member for high temperature apparatuses |
| 05/31/2005 | US6899531 Secondary air turbocharger with sound absorbing insulating material |
| 05/31/2005 | US6899520 Methods and apparatus to reduce seal rubbing within gas turbine engines |
| 05/31/2005 | US6899339 Abradable seal having improved durability |
| 05/31/2005 | US6898938 Differential pressure induced purging fuel injector with asymmetric cyclone |
| 05/31/2005 | US6898935 System and method of cooling steam turbines |
| 05/31/2005 | US6898926 Cooled purging fuel injectors |
| 05/26/2005 | WO2005047789A2 Method for efficient, nonsynchronous lng production |
| 05/26/2005 | WO2005047670A2 Method and apparatus for actuating fuel trim valves in a gas turbine |
| 05/26/2005 | WO2005021950A3 Atomization and injection system, and method for operating the same |
| 05/26/2005 | US20050111988 Pump health monitoring |
| 05/26/2005 | US20050111977 Triple circuit turbine blade |
| 05/26/2005 | US20050111976 Dual coolant turbine blade |
| 05/26/2005 | US20050111975 Method for assembling gas turbine engine components |
| 05/26/2005 | US20050111970 Turbine durm rotor for a turbine engine |
| 05/26/2005 | US20050111967 Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine |
| 05/26/2005 | US20050111965 Turbine shroud asymmetrical cooling elements |
| 05/26/2005 | US20050111964 Triple circuit turbine cooling |
| 05/26/2005 | US20050111963 Turbine blade/vane and casting system for manufacturing a turbine blade/vane |
| 05/26/2005 | US20050110991 Methods and apparatus for evaluating rotary machinery |
| 05/26/2005 | US20050109557 Soundproofing panel with beads, and a method of manufacture |
| 05/26/2005 | US20050109034 Method for operation of a power generation plant |
| 05/26/2005 | US20050109033 Method for operating a gas turbine group |
| 05/26/2005 | US20050109011 De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanes |
| 05/25/2005 | EP1533787A1 Sound insulation panel containing balls and method for producing it |
| 05/25/2005 | EP1533481A2 Hot gas path component with a meshed and dimpled cooling structure |
| 05/25/2005 | EP1533478A2 Turbine shroud asymmetrical cooling elements |
| 05/25/2005 | EP1533477A2 Dual coolant turbine blade |
| 05/25/2005 | EP1533476A2 Method for assembling gas turbine engine components |
| 05/25/2005 | EP1533475A2 Hot gas path component with mesh and dimpled cooling |
| 05/25/2005 | EP1533474A2 Triple circuit turbine blade |
| 05/25/2005 | EP1533473A1 Triple circuit turbine cooling |
| 05/25/2005 | EP1533396A2 Method for repairing coated components using NiAl bond coats |
| 05/25/2005 | EP1533071A2 Method for repairing gas turbine rotor blades |
| 05/25/2005 | EP1532358A2 Orbiting combustion nozzle engine |
| 05/25/2005 | DE102004051260A1 Gas turbine assembly for a power plant comprises, downstream of a pump, a line leading to a spraying device that branches off from a line leading from the pump to a liquid injection site |
| 05/25/2005 | CN1619109A Seal assembly and method for sealing interface between rotating and stationary components of a turbine |
| 05/25/2005 | CN1619108A Variable density array of pedestals at airfoil trailing edge |
| 05/24/2005 | US6898540 System and method for displaying real-time turbine corrected output and heat rate |
| 05/24/2005 | US6897578 Integrated microturbine gearbox generator assembly |
| 05/24/2005 | US6897401 Non-separating diffuser for holes produced by a two step process |