| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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| 10/06/2005 | US20050220624 Compressor blade platform extension and methods of retrofitting blades of different blade angles |
| 10/06/2005 | US20050220622 Integral covered nozzle with attached overcover |
| 10/06/2005 | US20050220621 Composite integrally bladed rotor |
| 10/06/2005 | US20050220619 Nozzle guide vanes |
| 10/06/2005 | US20050220618 Counter-bored film-cooling holes and related method |
| 10/06/2005 | US20050220617 Ring unit for decreasing eddy flow area of a fan module |
| 10/06/2005 | US20050220616 Vane and throat shaping |
| 10/06/2005 | US20050220615 Frequency-tuned compressor stator blade and related method |
| 10/06/2005 | US20050220614 Fluid pump apparatus |
| 10/06/2005 | US20050220611 Hybrid seal and system and method incorporating the same |
| 10/06/2005 | US20050220610 Sealing device and method for turbomachinery |
| 10/06/2005 | US20050217277 Cavity on-board injection for leakage flows |
| 10/06/2005 | US20050217131 Template for evaluating parts and method of using same |
| 10/06/2005 | US20050217110 Deposition repair of hollow items |
| 10/06/2005 | DE102004016221A1 Cooling system for HP turbine of aviation jet engine has low pressure chamber for receiving of LP compressed air for additional cooling of guide vane segments and means for dilution-free cross-over of HP and LP compressed air flows |
| 10/06/2005 | DE102004011607A1 Verdichter einer Gasturbine sowie Gasturbine Compressor of a gas turbine and gas turbine |
| 10/06/2005 | CA2503800A1 Deposition repair of hollow items |
| 10/05/2005 | EP1582862A1 Method and apparatus for the diagnosis of a in use strained component |
| 10/05/2005 | EP1582838A1 Template for evaluating turbine blades |
| 10/05/2005 | EP1582700A2 Seal assembly for a turbomachine |
| 10/05/2005 | EP1582699A2 Hybrid seal for a gas turbine |
| 10/05/2005 | EP1582698A1 Integral covered nozzle with attached overcover |
| 10/05/2005 | EP1582697A1 Cavity on-board injection for leakage flows |
| 10/05/2005 | EP1582696A1 Compressor vane and method of constructing a compressor vane |
| 10/05/2005 | EP1582695A1 Turbomachine blade |
| 10/05/2005 | EP1582694A1 Method for protecting openings in a component during processing |
| 10/05/2005 | EP1582289A1 Apparatus and method for repairing tenons on turbine buckets |
| 10/05/2005 | EP1581386A1 Layer system |
| 10/05/2005 | EP1144141B1 Multipiece core assembly |
| 10/05/2005 | CN1678816A Recirculation structure for a turbocompressor |
| 10/05/2005 | CN1677045A Template for evaluating parts and method of using same |
| 10/05/2005 | CN1676976A Hybrid seal assembly and system and method incorporating the same |
| 10/05/2005 | CN1676885A Integral covered guider with attached overcover |
| 10/05/2005 | CN1676884A Erosion and wear resistant protective structures for turbine engine components |
| 10/04/2005 | US6951448 Axial retention system and components thereof for a bladed rotor |
| 10/04/2005 | US6951447 Turbine blade with trailing edge platform undercut |
| 10/04/2005 | US6951444 Turbine and a turbine vane for a turbine |
| 10/04/2005 | CA2192327C Centrifugal or mixed flow turbomachinery |
| 10/01/2005 | CA2500683A1 Template for evaluating parts and method of using same |
| 09/29/2005 | WO2005090755A1 Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine |
| 09/29/2005 | US20050214563 Modified bond coat for increasing the cyclic spallation life of thermal barrier coating |
| 09/29/2005 | US20050214505 Article having a vibration damping coating and a method of applying a vibration damping coating to an article |
| 09/29/2005 | US20050214124 Apparatus and methods for repairing tenons on turbine buckets |
| 09/29/2005 | US20050214123 Compressor wheel and shield |
| 09/29/2005 | US20050214120 High speed rotor assembly shroud |
| 09/29/2005 | US20050214118 Cooling arrangement |
| 09/29/2005 | US20050214113 Compressor for an aircraft engine |
| 09/29/2005 | US20050214111 Pressure relief of a flange connection in overflow lines between a live steam valve and a high-pressure steam turbine inlet |
| 09/29/2005 | DE102004012599A1 Druckentlastung einer Flanschverbindung in Überströmleitungen zwischen Frischdampfventil und HD-Dampfturbineneintritt Depressurization of a flange in overflow lines between steam valve and steam turbine inlet HD |
| 09/29/2005 | DE102004011508A1 Rotor-Schluss Rotor end |
| 09/28/2005 | EP1580537A1 Method and device for detecting cooling system failures of a turbine |
| 09/28/2005 | EP1580414A2 Turbomachine component with cooling arrangement |
| 09/28/2005 | EP1580401A2 Sealing for transition between cooling passages of two turbomachine components |
| 09/28/2005 | EP1580400A1 Array of flow directing elements |
| 09/28/2005 | EP1580399A1 Compressor for an aircraft engine. |
| 09/28/2005 | EP1580296A2 Reduced thermal conductivity TBC by EB-PVD process to incorporate porosity |
| 09/28/2005 | EP1580293A2 An article having a vibration damping coating and a method of applying a vibration damping coating to an article |
| 09/28/2005 | CN1673492A Gas turbine engine-driven blade with gas nozzle |
| 09/28/2005 | CN1673491A Soldering structure and soldering method for machinable seal structual parts |
| 09/27/2005 | US6948913 Turbochargers |
| 09/22/2005 | WO2005088135A1 Compressor of a gas turbine and gas turbine |
| 09/22/2005 | US20050208337 Reduced thermal conductivity TBC by EB-PVD process to incorporate porosity |
| 09/22/2005 | US20050207896 Erosion and wear resistant protective structures for turbine engine components |
| 09/22/2005 | US20050207892 Rotating blade body and rotary machine using rotating blade body |
| 09/22/2005 | US20050205644 Method and device for holding a metallic component to be connected, especially a gas turbine blade |
| 09/22/2005 | US20050205415 Multi-component deposition |
| 09/22/2005 | US20050205174 Property recovering method |
| 09/22/2005 | US20050205002 Casting method |
| 09/22/2005 | DE102005009748A1 Motorwerkzeug Engine Tools |
| 09/22/2005 | DE102005008509A1 Laufschaufelkörper und Rotationsmaschine mit einem Laufschaufelkörper Blade body and rotating machine with a blade body |
| 09/22/2005 | CA2558325A1 Compressor of a gas turbine and gas turbine |
| 09/21/2005 | EP1577503A1 Turbo machine, stator vanes and assembly ring |
| 09/21/2005 | EP1577499A2 Turbine components with thermal barrier coatings |
| 09/21/2005 | EP1577498A1 Microcircuit cooling for a turbine airfoil |
| 09/21/2005 | EP1577497A1 Internally cooled turbomachine blade |
| 09/21/2005 | EP1577496A2 Casting method for turbine blade |
| 09/21/2005 | EP1577495A1 Turbomachine rolling bearing assembly having a reduced space requirement |
| 09/21/2005 | EP1577494A1 Welded steam turbine shaft and its method of manufacture |
| 09/21/2005 | EP1577493A1 Turbomachine and rotor for a turbomachine |
| 09/21/2005 | EP1577492A1 Method and apparatus for establishing the state of the rotor of a turbomachine |
| 09/21/2005 | EP1577422A1 Erosion and wear resistant protective structures for turbine engine components |
| 09/21/2005 | EP1577417A1 Multi-component deposition |
| 09/21/2005 | EP1577415A1 Method for aluminide coating a hollow article |
| 09/21/2005 | EP1576257A1 Manufacturing method of high-temperature resistant blades in a gas turbine |
| 09/21/2005 | EP1575736A1 Spun metal form used to manufacture dual alloy turbine wheel |
| 09/21/2005 | EP1575727A1 Manufacturing method for obtaining high-performance components for gas turbines and components thus obtained |
| 09/21/2005 | CN1671948A Coolable component and method for the production of a through opening in a coolable component |
| 09/21/2005 | CN1671878A Ceramic particle-containing self-melting alloy thermal spraying material |
| 09/21/2005 | CN1670337A Turbine components with thermal barrier coatings |
| 09/21/2005 | CN1670336A Microcircuit cooling for a turbine airfoil |
| 09/21/2005 | CN1670253A Multi-component deposition |
| 09/20/2005 | US6946208 Sinter resistant abradable thermal barrier coating |
| 09/20/2005 | US6945754 Methods and apparatus for designing gas turbine engine rotor assemblies |
| 09/20/2005 | US6945750 Turbine blade |
| 09/20/2005 | US6945749 Turbine blade platform cooling system |
| 09/20/2005 | US6945124 Measurement system |
| 09/19/2005 | CA2500933A1 Multi-component deposition |
| 09/17/2005 | CA2500753A1 Turbine components with thermal barrier coatings |
| 09/16/2005 | CA2497755A1 Microcircuit cooling for a turbine airfoil |
| 09/15/2005 | WO2005085599A1 Rotor end |