| 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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| 05/05/2005 | US20050095123 Turboshaft engine comprising two elements connected to each other with the interposition of a seal |
| 05/05/2005 | US20050095122 Main gas duct internal seal of a high-pressure turbine |
| 05/05/2005 | US20050095117 Methods and apparatus for operating gas turbine engines |
| 05/05/2005 | US20050093214 Spring mass damper system for turbine shrouds |
| 05/05/2005 | US20050092717 Fusion welding method and welded article |
| 05/05/2005 | US20050092566 Support apparatus and method for ceramic matrix composite turbine bucket shroud |
| 05/05/2005 | US20050091985 Gas-turbine power generating installation and method of operating the same |
| 05/05/2005 | US20050091984 Heat shield for gas turbine engine |
| 05/05/2005 | US20050091847 Method for repairing gas turbine compressor rotor blades |
| 05/04/2005 | EP1528350A2 Plate fin type recuperator and gas turbine power system |
| 05/04/2005 | EP1528239A1 Methods and apparatus for operating gas turbine engines with intercoolers between compressors |
| 05/04/2005 | EP1528238A2 Gas turbine plant and method of cooling gas turbine plant |
| 05/04/2005 | EP1528237A2 Gas-turbine power generating installation and method of operating the same |
| 05/04/2005 | EP1528224A2 Method and apparatus for cooling gas turbine engine rotor blade |
| 05/04/2005 | EP1528118A2 Gas turbine component with a protective coating and process for its manufacture |
| 05/04/2005 | EP1527997A2 Flade gas turbine engine with fixed geometry inlet |
| 05/04/2005 | EP1527845A2 Method for repairing gas turbine compressor rotor blades |
| 05/04/2005 | EP1527839A1 Fusion welding method and welded article |
| 05/04/2005 | DE4435322B4 Verfahren und Vorrichtung zur Wellendichtung und zur Kühlung auf der Abgasseite einer axialdurchströmten Gasturbine Method and apparatus for shaft sealing and cooling on the exhaust side of an axial-flow type gas turbine |
| 05/04/2005 | DE19961540B4 Zuluftkanal für Dampferzeuger mit Wärmerückgewinnung Supply air duct for steam generators with heat recovery |
| 05/04/2005 | DE19815914B4 Verteiler Distributor |
| 05/04/2005 | CN1612978A Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 05/04/2005 | CN1612977A Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 05/04/2005 | CN1611839A Gas turbine control apparatus, gas turbine system and gas turbine control method |
| 05/04/2005 | CN1611754A Methods and apparatus to reduce seal rubbing within gas turbine engines |
| 05/04/2005 | CN1611748A Method and apparatus for cooling gas turbine engine rotor blade |
| 05/04/2005 | CN1611747A Methods and apparatus for cooling gas turbine rotor blades |
| 05/03/2005 | US6888263 Gas turbine generator |
| 05/03/2005 | US6887530 Thermal spray compositions for abradable seals |
| 05/03/2005 | US6887529 Method of applying environmental and bond coatings to turbine flowpath parts |
| 05/03/2005 | US6887044 Gas turbine blade |
| 05/03/2005 | US6887043 Methods and apparatus for assembling gas turbine engines |
| 05/03/2005 | US6887041 Airfoil shape for a turbine nozzle |
| 05/03/2005 | US6887039 Stationary blade in gas turbine and gas turbine comprising the same |
| 05/03/2005 | US6887038 Methods and apparatus to facilitate sealing between rotating turbine shafts |
| 05/03/2005 | US6887033 Cooling system for nozzle segment platform edges |
| 05/03/2005 | US6886346 Gas turbine fuel pilot nozzle |
| 05/03/2005 | US6886345 Electrostatic evaporative cooling system |
| 05/03/2005 | US6886343 Methods and apparatus for controlling engine clearance closures |
| 05/03/2005 | US6886341 Gas-turbine engine combustor |
| 05/03/2005 | US6886326 Quasi-isothermal brayton cycle engine |
| 05/03/2005 | US6886324 Apparatus for reducing coking in gas turbine bearings |
| 05/03/2005 | CA2326992C Profiled surface used as an abradable in flow machines |
| 04/28/2005 | US20050091393 Method and apparatus for selective data control |
| 04/28/2005 | US20050089399 Low-pressure turbine of a turbomachine |
| 04/28/2005 | US20050089395 Cooled gas turbine engine vane |
| 04/28/2005 | US20050089390 Abradable device on the blower casing of a gas turbine engine |
| 04/28/2005 | US20050087330 Recuperator construction for a gas turbine engine |
| 04/28/2005 | US20050087319 Refractory metal core wall thickness control |
| 04/28/2005 | US20050086945 Combustion chamber, in particular of a gas turbine |
| 04/28/2005 | US20050086944 Turbine engine fuel injector |
| 04/28/2005 | US20050086943 Turbine compartment ventilation control system and method using variable speed fan |
| 04/28/2005 | US20050086942 Approach to extending life of gas turbine engine |
| 04/28/2005 | US20050086939 Gas-turbine installation |
| 04/28/2005 | US20050086804 Process for machining axial blade slots in turbine disks for jet engines |
| 04/27/2005 | EP1526333A1 Turbine engine fuel injector |
| 04/27/2005 | EP1526285A1 Turbo engine blade, particularly compressor blade and its fabrication method |
| 04/27/2005 | EP1526253A1 Labyrinth seal for a turbo machine |
| 04/27/2005 | EP1525380A1 System for cooling cooling air in a gas turbine, and method for cooling cooling air |
| 04/27/2005 | EP1204818A4 Efficiency enhanced turbine engine |
| 04/27/2005 | CN2695652Y Pipe assembling component |
| 04/27/2005 | CN1609426A Methods and apparatus for cooling turbine engine combustor exit temperatures |
| 04/27/2005 | CN1609060A Article comprising silicon substrate and bond layer |
| 04/27/2005 | CN1608771A Refractory metal core wall thickness control |
| 04/26/2005 | US6884279 Producing metallic articles by reduction of nonmetallic precursor compounds and melting |
| 04/26/2005 | US6884275 Mixing and heating two alloy powders with different melting points; high temperature parts in gas turbines and jet engines |
| 04/26/2005 | US6884036 Complementary cooled turbine nozzle |
| 04/26/2005 | US6884026 Turbine engine shroud assembly including axially floating shroud segment |
| 04/26/2005 | US6884023 Integral swirl knife edge injection assembly |
| 04/26/2005 | US6883807 Multidirectional turbine shim seal |
| 04/26/2005 | US6883507 System and method for generating and sustaining a corona electric discharge for igniting a combustible gaseous mixture |
| 04/26/2005 | US6883331 Method and arrangement for providing a gas turbine, and engine-braking therefore |
| 04/26/2005 | US6883330 Variable geometry inlet design for scram jet engine |
| 04/26/2005 | US6883329 Method of fuel nozzle sizing and sequencing for a gas turbine combustor |
| 04/26/2005 | US6883301 Apparatus for reducing gas turbine engines emissions |
| 04/26/2005 | US6883234 Process for machining axial blade slots in turbine disks for jet engines |
| 04/26/2005 | CA2376163C Efficiency enhanced turbine engine |
| 04/26/2005 | CA2372623C Axial flow turbine having stepped portion formed in axial-flow turbine passage |
| 04/21/2005 | WO2005035990A1 Formed disk plate heat exchanger |
| 04/21/2005 | WO2005001260A3 Blade cooling in a gas turbine engine |
| 04/21/2005 | US20050084377 Turbomachine blade, in particular a fan blade, and its method of manufacture |
| 04/21/2005 | US20050084190 Variable vane electro-graphitic bushing |
| 04/21/2005 | US20050082768 Seal device |
| 04/21/2005 | US20050082112 Annular acoustic panel |
| 04/21/2005 | US20050081992 Process for making a panel with a protected acoustic damping layer |
| 04/21/2005 | US20050081529 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 04/21/2005 | US20050081526 Methods and apparatus for cooling turbine engine combustor exit temperatures |
| 04/21/2005 | US20050081525 Cooling of liquid fuel components to eliminate coking |
| 04/21/2005 | US20050081509 Flade gas turbine engine with fixed geometry inlet |
| 04/21/2005 | US20050081508 Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance |
| 04/21/2005 | US20050081507 Fluid system |
| 04/21/2005 | DE102004012929B3 Noise reduction system for gas turbine engine for aircraft has surface cladding for hot gas channel downstream of turbine, with circular perforated plates covering large ends of frustoconical spaces |
| 04/20/2005 | EP1524817A1 Method and apparatus for selective data control |
| 04/20/2005 | EP1524471A1 Methods and apparatus for cooling turbine engine combuster exit temperatures |
| 04/20/2005 | EP1524412A2 Variable vane electro-graphitic bushing |
| 04/20/2005 | EP1524328A1 Method of selective region vapor phase aluminizing |
| 04/20/2005 | EP1204450B1 Powered air precleaner device and method for providing a clean air flow |
| 04/20/2005 | CN1607766A Method and apparatus for selective data control |
| 04/19/2005 | US6881036 Composite integrally bladed rotor |
| 04/19/2005 | US6881029 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing |