| 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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| 04/05/2006 | EP1642005A1 Turbine blade |
| 04/05/2006 | EP1641959A1 Layer structure and method for producing such a layer structure |
| 04/04/2006 | US7021899 Lightened turbomachine blade and its manufacturing process |
| 04/04/2006 | US7021898 Damper seal |
| 04/04/2006 | US7021896 Turbine blade |
| 04/04/2006 | US7021893 Fanned trailing edge teardrop array |
| 04/04/2006 | US7021892 Method for assembling gas turbine engine components |
| 04/04/2006 | US7021043 Jet engine using exhaust gas |
| 03/30/2006 | WO2006033407A1 Wall shape of axial flow machine and gas turbine engine |
| 03/30/2006 | US20060067832 Tri-property rotor assembly of a turbine engine, and method for its preparation |
| 03/30/2006 | US20060067821 Methods and apparatus for aerodynamically self-enhancing rotor blades |
| 03/30/2006 | DE10319019B4 Verfahren zur Wartung, insbesondere Reparatur, von Gasturbinen Procedures for maintenance, in particular repair of gas turbines |
| 03/30/2006 | DE102005042621A1 Vorrichtung und Verfahren zum Kühlen der Plattformen von Turbinenlaufschaufeln Apparatus and method for cooling the platforms of turbine blades |
| 03/30/2006 | DE102005007404B3 Production of a welding joint of a shaft with a turbine wheel of an exhaust gas turbocharger comprises joining the shaft with the turbine wheel and surface treating the sealed region of the shaft in the same step |
| 03/29/2006 | EP1640587A1 Cooling system for gas turbine, compressor stator vane and method for cooling a gas turbine |
| 03/29/2006 | EP1640563A2 Heat transfer augmentation in a compact heat exchanger pedestral array |
| 03/29/2006 | EP1640562A1 Frequency tuning method of a turbine blade and turbine blade |
| 03/29/2006 | EP1640477A2 High temperature component with thermal barrier coating and gas turbine using the same |
| 03/29/2006 | EP1640473A1 Thermal barrier coating with modulated grain structure and method therefor |
| 03/29/2006 | EP1639152A1 Method for producing a protective layer, protective layer, use thereof, and part provided with a protective layer |
| 03/29/2006 | EP1153157B1 Thermal barrier coating resistant to sintering |
| 03/29/2006 | CN1752415A Heat transfer augmentation in a compact heat exchanger pedestal array |
| 03/28/2006 | US7018176 Cooled turbine airfoil |
| 03/28/2006 | US7018174 Turbine blade |
| 03/28/2006 | US7018172 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 03/28/2006 | US7018170 Ribbon drive pumping apparatus and method with added fluid |
| 03/28/2006 | US7018167 Fluid machinery |
| 03/28/2006 | US7017793 Repair process |
| 03/28/2006 | US7017349 Gas turbine and bleeding method thereof |
| 03/23/2006 | WO2006029983A1 Turbine engine vane with fluid cooled shroud |
| 03/23/2006 | US20060062674 Axial-flow thermal turbomachine |
| 03/23/2006 | US20060062673 Mechanical solution for rail retention of turbine nozzles |
| 03/23/2006 | US20060062671 Common tip chamber blade |
| 03/23/2006 | US20060062664 Thermal turbomachine |
| 03/23/2006 | US20060059890 Rotor blade for a first phase of a gas turbine |
| 03/23/2006 | DE102004037331A1 Gasturbinenrotor Gas turbine rotor |
| 03/23/2006 | DE102004036598A1 Verfahren zum Herstellen aerodynamischer Strukturen bei der Fertigung von integral beschaufelten Gasturbinenrotoren A method for producing aerodynamic structures in the manufacture of integrally bladed gas turbine rotors |
| 03/23/2006 | DE102004036389A1 Method for fitting turbine blade into mounting with a securing element located into a profiled groove having at least two cross sectional curvatures for a strain free fitting |
| 03/22/2006 | EP1637702A1 Turbine module for gas turbine engine |
| 03/22/2006 | EP1637701A1 A monoblock body for a rotor of a gas turbine engine |
| 03/22/2006 | EP1637699A2 Offset coriolis turbulator blade |
| 03/22/2006 | EP1637698A1 Rotor blade for a first phase of a gas turbine |
| 03/22/2006 | EP1637697A2 Fluid machine flow path with axial gap concentration smaller than 1 |
| 03/22/2006 | EP1637696A2 Apparatus for balancing gas turbine engines |
| 03/22/2006 | EP1637253A1 Process of fabricating a turbine blade and core assembly to be used in the process |
| 03/22/2006 | EP1636462A1 Blade and gas turbine |
| 03/22/2006 | EP1636461A1 Turbomachine, in particular gas turbine |
| 03/22/2006 | EP1341639B1 Nickel diffusion braze alloy and method for repair of superalloys |
| 03/22/2006 | EP1200713B1 Turbine guide vane for exhaust gas turbocharger |
| 03/22/2006 | CN1749535A Turbine blade and turbine device |
| 03/22/2006 | CN1749534A Cooling system for the trailing edges of turbine bucket airfoils |
| 03/22/2006 | CN1749533A Apparatus and methods for cooling turbine bucket platforms |
| 03/22/2006 | CN1749532A Apparatus and methods for cooling turbine bucket platforms |
| 03/22/2006 | CN1749531A Turbine blade nested seal damper assembly |
| 03/22/2006 | CN1246570C Turbine rotor vane |
| 03/21/2006 | US7014533 Method for smoothing the surface of a gas turbine blade |
| 03/21/2006 | US7014424 Turbine element |
| 03/21/2006 | CA2520282A1 Turbine module for gas turbine engine |
| 03/21/2006 | CA2520069A1 Turbine module for gas turbine engine with rotor that includes a monobloc body |
| 03/21/2006 | CA2518558A1 Rotor blade for a first phase of a gas turbine |
| 03/21/2006 | CA2393282C Turbine blade and method of repair |
| 03/20/2006 | CA2510810A1 Heat transfer augmentation in a compact heat exchanger pedestal array |
| 03/16/2006 | WO2006028941A2 Fretting wear protection for spline couplings |
| 03/16/2006 | WO2006028482A1 Platinum aluminide coating and method thereof |
| 03/16/2006 | WO2006026962A1 Method for producing a gas turbine rotor comprising integral hollow blades |
| 03/16/2006 | US20060057414 Steel tube excellent in exfoliation resistance of scale on inner surface |
| 03/16/2006 | US20060057305 Method for treating organs subject to erosion by liquids and anti-erosion coating alloy |
| 03/16/2006 | US20060057018 Composition of matter |
| 03/16/2006 | US20060056975 Methods and apparatus for assembling gas turbine engine rotor assemblies |
| 03/16/2006 | US20060056974 Turbine blade nested seal damper assembly |
| 03/16/2006 | US20060056970 Apparatus and methods for cooling turbine bucket platforms |
| 03/16/2006 | US20060056969 Cooling system for the trailing edges of turbine bucket airfoils |
| 03/16/2006 | US20060056968 Apparatus and methods for cooling turbine bucket platforms |
| 03/16/2006 | US20060056967 Vortex cooling system for a turbine blade |
| 03/16/2006 | US20060056961 Turbine assembly and turbine shroud therefor |
| 03/16/2006 | DE102005044183A1 Vorrichtung und Verfahren zur Kühlung von Turbinenschaufelplattformen Apparatus and method for cooling turbine blade platforms |
| 03/16/2006 | DE102005044182A1 Kühlsystem für die Hinterkanten von Turbinenschaufelblättern Cooling system for the rear edges of airfoils |
| 03/16/2006 | DE102004045049A1 Protection layer application, involves applying undercoating with heat insulating layer, and subjecting diffusion layer to abrasive treatment, so that outer structure layer of diffusion layer is removed by abrasive treatment |
| 03/16/2006 | DE102004044324A1 Abgasturbolader Exhaust gas turbocharger |
| 03/15/2006 | EP1635041A1 Variable stator vanes for a turbocharger |
| 03/15/2006 | EP1635038A1 Exhaust turbocharger |
| 03/15/2006 | EP1635037A2 Turbine blade nested seal damper assembly |
| 03/15/2006 | EP1634977A1 Process for inhibiting the formation of a secondary reaction zone (SRZ) and coating system therefor |
| 03/15/2006 | EP1634971A2 Application of high strength titanium alloys in last stage turbine buckets having longer vane lengths |
| 03/15/2006 | CN1746338A Methods and apparatus for fabricating gas turbine engines |
| 03/14/2006 | US7011894 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby |
| 03/14/2006 | US7011721 Provides improved casting/coating performance, stress-/creep-rupture properties, and an increased tolerance for grain defects; oxidation resistance |
| 03/14/2006 | US7011502 Thermal shield turbine airfoil |
| 03/14/2006 | US7011496 Ring unit for decreasing eddy flow area of a fan module |
| 03/14/2006 | US7011495 Fluid flow machine (turbomachine) with increased rotor-stator ratio |
| 03/14/2006 | US7011494 Dual retention vane arm |
| 03/14/2006 | US7011492 Turbine vane cooled by a reduced cooling air leak |
| 03/14/2006 | US7010916 Exhaust-gas turbocharger |
| 03/13/2006 | CA2507086A1 Turbine blade nested seal damper assembly |
| 03/09/2006 | WO2006026695A2 Welding shield for automated welding of impellers and blisks, sized to match within vallexs of a particular designed impeller ; method to provide protection from welding related damage in an impeller |
| 03/09/2006 | WO2006025847A2 Fanned trailing edge teardrop array |
| 03/09/2006 | WO2006024273A1 Rotor for a power plant |
| 03/09/2006 | US20060051608 Layer system |
| 03/09/2006 | US20060051211 Method of assembling one-piece bladed disks, and a device for damping vibration of the blades of such disks |
| 03/09/2006 | US20060051209 Fluted tip turbine blade |