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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10/22/2009 | US20090263253 Engine components and rotor groups |
10/22/2009 | US20090263251 Reduced weight blade for a gas turbine engine |
10/22/2009 | US20090263249 Welded Low-Pressure Turbine Shaft |
10/22/2009 | US20090263248 Shape for a turbine bucket tip shroud |
10/22/2009 | US20090263237 Coated turbine component and method of coating a turbine component |
10/22/2009 | DE102008019891A1 Erosionsschutzbeschichtung Erosion protection coating |
10/22/2009 | DE102004055199B4 Herstellungsverfahren für Gleitschichten aus Verbundmaterial Manufacturing processes for sliding layers of composite material |
10/22/2009 | CA2724693A1 Blade for a water turbine |
10/21/2009 | EP2110515A2 Cooling arrangement between two blade platforms for a gas turbine engine |
10/21/2009 | EP2110514A2 Asymmetrical rotor blade fir tree attachment |
10/21/2009 | EP2110513A2 Reduced weight blade for a gas turbine engine |
10/21/2009 | EP2110512A1 Turbine blade twist angle correction tooling |
10/21/2009 | EP2110457A2 Platinum-modified cathodic arc coating |
10/21/2009 | EP2110449A1 Heat resistant member |
10/21/2009 | EP2110193A1 Method for blisk milling |
10/21/2009 | EP1828546B1 Stacked annular components for turbine engines |
10/21/2009 | EP1373593B1 Method and device for gas phase diffusion coating of metal components |
10/21/2009 | CN201330619Y Industrial exhaust heat steam and pneumatic helical engine |
10/21/2009 | CN100552189C Heated wall surface cooling structure and gas turbine impeller vane with the same |
10/20/2009 | US7604199 Aerofoil containment structure |
10/20/2009 | CA2569026C Wall configuration of axial-flow machine, and gas turbine engine |
10/20/2009 | CA2480989C Teardrop film cooled blade |
10/20/2009 | CA2396216C Process for making a one-piece rotor blade and corresponding blade |
10/15/2009 | WO2009126194A1 Segmented thermal barrier coating |
10/15/2009 | WO2009126191A2 Sealing arrangement for turbine engine having ceramic components |
10/15/2009 | WO2009124949A1 Turbomachine rotor comprising an anti-wear plug, and anti-wear plug |
10/15/2009 | WO2009124585A1 Turbine device |
10/15/2009 | WO2009082581A3 Main rotor blade with integral tip section |
10/15/2009 | WO2009071521A3 Device for dynamically measuring the imbalance of the rotor of a turbocharger |
10/15/2009 | US20090257878 Low exhaust loss turbine and method of minimizing exhaust losses |
10/15/2009 | US20090257877 Asymmetrical rotor blade fir-tree attachment |
10/15/2009 | US20090257876 Blower Impeller with Partial Tip Blockage |
10/15/2009 | US20090257875 Platformless turbine blade |
10/15/2009 | US20090255267 Comubstor seal having multiple cooling fluid pathways |
10/15/2009 | DE102008017793A1 Vorrichtung und Verfahren zur Fixierung eines Werkstücks Apparatus and method for securing a workpiece |
10/15/2009 | CA2720807A1 Turbomachine rotor comprising an anti-wear plug, and anti-wear plugi-usu |
10/14/2009 | EP2108785A2 Turbine blade and vane assembly with a ceramic platform |
10/14/2009 | EP2108784A2 Flow machine with fluid injector component group |
10/14/2009 | EP2108715A2 Thermal barrier coating system and coating methods for gas turbine engine shroud |
10/14/2009 | EP2108477A1 Gas turbine hot gas component repair method |
10/14/2009 | EP1642005B1 Turbine blade |
10/14/2009 | CN201326456Y Gas engine power generation muffler |
10/14/2009 | CN101558235A Flow deflection devices and method for energy capture machines |
10/13/2009 | US7600979 CMC articles having small complex features |
10/13/2009 | US7600978 Hollow CMC airfoil with internal stitch |
10/13/2009 | US7600977 Turbine blade tip cap |
10/13/2009 | US7600973 Blades for gas turbine engines |
10/13/2009 | US7600972 Methods and apparatus for cooling gas turbine engine rotor assemblies |
10/13/2009 | US7600966 Turbine airfoil with improved cooling |
10/08/2009 | WO2009122040A1 Method for manufacturing hollow blade |
10/08/2009 | WO2009121768A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed after a finish-milling step |
10/08/2009 | WO2009121767A1 Method for producing a one-piece bladed disc by abrasive water-jet cutting |
10/08/2009 | WO2009121765A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed before a finish-milling step |
10/08/2009 | WO2009121764A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring |
10/08/2009 | WO2009121762A1 Improved method for making a one-piece bladed disk, with temporary retaining ring for bladed disks removed before a milling step |
10/08/2009 | WO2009121716A1 Blade for a gas turbine |
10/08/2009 | WO2009121715A1 Cooling duct arrangement within a hollow-cast casting |
10/08/2009 | WO2009121465A1 Exhaust gas turbocharger for an internal combustion engine |
10/08/2009 | US20090252615 Cooled Turbine Rotor Blade |
10/08/2009 | US20090252613 Repair of gas turbine blade tip without recoating the repaired blade tip |
10/08/2009 | US20090252612 Blade and gas turbine |
10/08/2009 | US20090252611 Axial compressor blade retention |
10/08/2009 | US20090252610 Turbine blade retention system and method |
10/08/2009 | US20090252609 Impeller for supercharger and method of manufacturing the same |
10/08/2009 | DE202009008513U1 Umlenkschaufeln für Gleichdruckturbinen mit Überschallströmung Turning vanes for constant-pressure turbines with supersonic flow |
10/08/2009 | DE10350946B4 Turbinendüsenhaltevorrichtung an der horizontalen Verbindungsfläche des Trägers Turbine nozzle holder at the horizontal joint surface of the carrier |
10/08/2009 | DE102009003714A1 Turbinenschaufelhaltesystem und -verfahren Turbine blade retention system and method |
10/08/2009 | DE102009003712A1 Axialverdichter-Laufschaufelhalterung Axial compressor blade holder |
10/08/2009 | DE102009003710A1 Schaufelblatt für einen Leitapparat mit einem maschinell bearbeiteten kontourierten Kanal darin Airfoil for a diffuser with a machined contoured channel therein |
10/08/2009 | DE102008017624A1 Verfahren zur aerodynamischen Ausformung der Vorderkante von Bliskschaufeln A method for aerodynamic shaping of the front edge of the blisk blades |
10/08/2009 | DE102008017495A1 Verfahren zur Herstellung von integral beschaufelten Rotoren A method of manufacturing integrally bladed rotors |
10/08/2009 | DE102008017494A1 Verfahren zur Fertigung integral beschaufelter Rotoren Method for manufacturing integrally bladed rotors |
10/08/2009 | DE102008016937A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
10/08/2009 | DE102008016800A1 Gasturbinenverdichter Gas turbine compressor |
10/08/2009 | DE102008015913A1 Vorrichtung zum Schweißen mit einer Prozesskammer und ein Schweißverfahren Apparatus for welding with a process chamber and a welding method |
10/08/2009 | CA2719355A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed after a finish-milling step |
10/08/2009 | CA2719354A1 Method for producing a one-piece bladed disc by abrasive water-jet cutting |
10/08/2009 | CA2719352A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed before a finish-milling step |
10/08/2009 | CA2719351A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring |
10/08/2009 | CA2719350A1 Improved method for making a one-piece bladed disk, with temporary retaining ring for bladed disks removed before a milling step |
10/08/2009 | CA2718801A1 Method for manufacturing hollow blade |
10/07/2009 | EP2107215A1 Gas turbine airfoil |
10/07/2009 | EP2107214A1 Chambered airfoil cooling |
10/07/2009 | EP2106877A1 Method for the fabrication of integrally bladed rotors |
10/07/2009 | EP2106876A1 Method for aerodynamically shaping the leading edge of blisk blades |
10/07/2009 | EP2106873A1 Method of producting integrally bladed rotors using orbital friction welding |
10/07/2009 | EP1971761B1 Method and apparatus for balancing an electrically assisted turbocharger rotor |
10/07/2009 | EP1834066B1 Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade |
10/07/2009 | CN101550845A Turbine blade retention system and method |
10/07/2009 | CN101550844A Inner turbine shell support configuration and methods |
10/07/2009 | CN101550843A 燃气轮机翼型 Gas turbine airfoil |
10/06/2009 | US7597843 Excellent in high temperature creep rupture strength, high temperature corrosion resistance and oxidation resistance; alloys are suitable for power plants such as jet engines, gas turbines, for high performance and high efficiency; single crystal superalloy |
10/06/2009 | US7597540 Turbine blade with showerhead film cooling holes |
10/06/2009 | US7597539 Turbine blade with vortex cooled end tip rail |
10/06/2009 | US7597536 Turbine airfoil with de-coupled platform |
10/06/2009 | US7597535 Fan module and its fan casing |
10/06/2009 | US7597533 BOAS with multi-metering diffusion cooling |
10/01/2009 | WO2009120778A2 Subsonic and stationary ramjet engines |
10/01/2009 | WO2009120629A1 High temperature resistant coating compositions |
10/01/2009 | WO2009119345A1 Alloy material having high-temperature corrosion resistance, heat-shielding coating material, turbine member, and gas turbine |