| 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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| 03/09/2006 | US20060051208 Offset coriolis turbulator blade |
| 03/09/2006 | US20060051200 Flow structure for a gas turbine |
| 03/09/2006 | DE102004042699A1 Strömungsstruktur für eine Gasturbine Flow structure for a gas turbine |
| 03/09/2006 | DE102004030703A1 Abgasturbolader für eine Hubkolben-Brennkraftmaschine und Hubkolben-Brennkraftmaschine Exhaust gas turbocharger for an internal combustion reciprocating piston engine and reciprocating internal combustion engine |
| 03/09/2006 | CA2518979A1 Fluted tip turbine blade |
| 03/09/2006 | CA2517202A1 Offset coriolis turbulator blade |
| 03/08/2006 | EP1632662A2 Turbomachine with bleeding |
| 03/08/2006 | EP1632648A2 Gas turbine flow path |
| 03/08/2006 | EP1631734A1 Rotor for a gas turbine and gas turbine |
| 03/08/2006 | EP1631700A2 Method for armour-plating the tips of rotating blades of a gas turbine mechanism and device for carrying out said method |
| 03/08/2006 | EP1631417A1 A turbine blade |
| 03/08/2006 | CN1743646A Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 03/07/2006 | US7009137 Laser powder fusion repair of Z-notches with nickel based superalloy powder |
| 03/07/2006 | US7008689 Pin reinforced, crack resistant fiber reinforced composite article |
| 03/07/2006 | US7008674 Thermal barrier coating protected by alumina and method for preparing same |
| 03/07/2006 | US7008553 Method for removing aluminide coating from metal substrate and turbine engine part so treated |
| 03/07/2006 | US7008190 Turbomachine rotor arrangement |
| 03/07/2006 | US7008186 Teardrop film cooled blade |
| 03/07/2006 | US7008185 Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 03/07/2006 | US7008181 Gas turbine engine air baffle for a rotating cavity |
| 03/07/2006 | US7008179 Turbine blade frequency tuned pin bank |
| 03/07/2006 | US7008178 Inboard cooled nozzle doublet |
| 03/07/2006 | US7007382 Slot machining |
| 03/03/2006 | CA2517080A1 Adjusting airflow in turbine component by depositing overlay metallic coating |
| 03/02/2006 | US20060045747 Compressor stator floating tip shroud and related method |
| 03/02/2006 | US20060045746 Multi-point seal |
| 03/02/2006 | US20060045745 Vane attachment arrangement |
| 03/02/2006 | US20060045741 Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 03/02/2006 | DE102004042295A1 Rotor für ein Triebwerk Rotor for an engine |
| 03/01/2006 | EP1630385A2 Method and apparatus for maintaining rotor assembly tip clearances |
| 03/01/2006 | EP1630362A1 Steam turbine with extraction of steam through hollow stator vanes |
| 03/01/2006 | EP1630354A2 Cooled gas turbine aerofoil |
| 03/01/2006 | EP1630353A2 Internally cooled gas turbine aerofoil |
| 03/01/2006 | EP1630352A1 Turbine component |
| 03/01/2006 | EP1630351A1 Blade for a compressor or a gas turbine |
| 03/01/2006 | EP1630350A1 Rotor blade of a compressor or a gas turbine |
| 03/01/2006 | EP1630262A1 Process for rebuilding a single crystal or directionally solidified metallic article |
| 03/01/2006 | EP1630259A2 Electroplating apparatus and method for making an electroplating anode assembly |
| 03/01/2006 | EP1630246A1 Turbine blade capable of inhibiting reaction |
| 03/01/2006 | EP1630245A1 Coating method for inhibiting reaction |
| 03/01/2006 | EP1629938A2 Turbine engine component manufacture |
| 03/01/2006 | EP1629930A1 Method of repairing cracks in a turbine component using cathodic arc and/or low pressure plasma spraying and high isostatic pressure (HIP) |
| 03/01/2006 | EP1629929A1 Method of repairing worn portions of a turbine component restoration using cathodic arc or Low Pressure Plasma Spraying (LPPS) and High Isostatic Pressing (HIP) |
| 03/01/2006 | CN1740641A Combustor member and method for making a combustor assembly |
| 03/01/2006 | CN1243937C Air-cooling apparatus |
| 02/28/2006 | US7005191 coatings that form a protective layer that prevents the substrate from oxidizing which results in a weakening of the substrate through dissolution or disintegration, particularly at high temperatures |
| 02/28/2006 | US7005015 A high-temperature component made of a nickel super-alloy consists of in wt %: 11-13% of Chromium, 3-5% of tungsten, 0.5- 2.5% of molybdenum, 3-5% aluminum, 3-5% of titanium , 3-7% of tantalum, 1-5% Re, reminder Nickel |
| 02/28/2006 | US7004725 Device for centering a tube in a turbine shaft |
| 02/28/2006 | US7004722 Axial flow compressor |
| 02/28/2006 | US7004721 Annular platform for a nozzle of a low-pressure turbine of a turbomachine |
| 02/28/2006 | US7004720 Cooled turbine vane platform |
| 02/28/2006 | US7003959 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing |
| 02/28/2006 | CA2516851A1 Foldable blades for wind turbines |
| 02/23/2006 | US20060040127 Ceramic compositions for thermal barrier coatings with improved mechanical properties |
| 02/23/2006 | US20060039792 Lightened turbomachine blade and its manufacturing process |
| 02/23/2006 | US20060039790 Device for the demounting of blades of a turbine or of a compressor |
| 02/23/2006 | US20060039789 Hub structure for a heat-dissipation fan |
| 02/23/2006 | US20060039787 Component having a cooling arrangement |
| 02/23/2006 | US20060039786 Airfoil cooling passage trailing edge flow restriction |
| 02/23/2006 | US20060037865 Methods and apparatus for fabricating gas turbine engines |
| 02/23/2006 | DE102005033362A1 Axialdampfturbinenanordnung Axialdampfturbinenanordnung |
| 02/23/2006 | DE102004038930A1 Blade for gas turbine engines of airplanes comprises a surface with dimples distributed over the blade surface |
| 02/23/2006 | DE102004038903A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
| 02/22/2006 | EP1628076A1 Cooling Channel, Combustor and Gas Turbine |
| 02/22/2006 | EP1627992A2 Methods and apparatus for fabricating gas turbine engines |
| 02/22/2006 | EP1627991A2 A component having a cooling arrangement |
| 02/22/2006 | EP1627990A2 Boundary layer control arrangement |
| 02/22/2006 | EP1627862A1 Ceramic compositions for thermal barrier coatings with improved mechanical properties |
| 02/22/2006 | CN1737378A Radial-flow turbine wheel |
| 02/22/2006 | CN1737339A Application of high strength titanium alloys in last stage turbine buckets having longer vane lengths |
| 02/22/2006 | CN1737199A Cleaning and servicing technology for turbine blade basal body surface by strong current pulsed ionizing beam |
| 02/22/2006 | CN1243119C High-strength, low-heat expansion cast steel |
| 02/21/2006 | US7001679 Protective overlayer for ceramics |
| 02/21/2006 | US7001155 Compressor impeller with stress riser |
| 02/21/2006 | US7001152 Shrouded turbine blades with locally increased contact faces |
| 02/21/2006 | US7001151 Gas turbine bucket tip cap |
| 02/21/2006 | US7001150 Hollow turbine blade stiffening |
| 02/21/2006 | US7001145 Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine |
| 02/21/2006 | US7001144 Gas turbine and method for reducing bucket tip shroud creep rate |
| 02/21/2006 | US7001143 Cambered vane for use in turbochargers |
| 02/21/2006 | US7001141 Cooled nozzled guide vane or turbine rotor blade platform |
| 02/21/2006 | US7000404 Heat exchanger on a turbine cooling circuit |
| 02/21/2006 | US7000306 Spun metal form used to manufacture dual alloy turbine wheel |
| 02/18/2006 | CA2513036A1 Airfoil cooling passage trailing edge flow restriction |
| 02/16/2006 | US20060035102 Strengthened bond coats for thermal barrier coatings |
| 02/16/2006 | US20060034695 Method of manufacture of dual titanium alloy impeller |
| 02/16/2006 | US20060034689 Turbine |
| 02/16/2006 | US20060034682 Ducted fan with containment structure |
| 02/16/2006 | US20060034681 Fan assembly and method |
| 02/16/2006 | US20060033974 Light regulator and image pickup system |
| 02/16/2006 | US20060032988 Boundary layer control arrangement |
| 02/16/2006 | DE102004034721A1 Laser process for forming a hole especially an air cooling hole in a layered workpiece especially a turbine component first removes cover layer then bores into base |
| 02/15/2006 | EP1626170A1 Turbomachine with counter-rotating fan |
| 02/15/2006 | EP1626163A2 Clip member for a stator assembly |
| 02/15/2006 | EP1626162A1 Temperature tolerant vane assembly |
| 02/15/2006 | EP1626161A1 Method of suppressing the aero-elastic response of a row of blades on a steam turbine wheel |
| 02/15/2006 | EP1626160A2 Degassing pipe for low pressure turbine shaft |
| 02/15/2006 | EP1626040A2 Coating process to enable electrophoretic deposition |
| 02/15/2006 | EP1626039A2 Non-line of-sight process for coating complexed shaped structures |
| 02/15/2006 | EP1626038A2 Thermal resistant environmental barrier coating |