Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
10/2009
10/22/2009US20090263253 Engine components and rotor groups
10/22/2009US20090263251 Reduced weight blade for a gas turbine engine
10/22/2009US20090263249 Welded Low-Pressure Turbine Shaft
10/22/2009US20090263248 Shape for a turbine bucket tip shroud
10/22/2009US20090263237 Coated turbine component and method of coating a turbine component
10/22/2009DE102008019891A1 Erosionsschutzbeschichtung Erosion protection coating
10/22/2009DE102004055199B4 Herstellungsverfahren für Gleitschichten aus Verbundmaterial Manufacturing processes for sliding layers of composite material
10/22/2009CA2724693A1 Blade for a water turbine
10/21/2009EP2110515A2 Cooling arrangement between two blade platforms for a gas turbine engine
10/21/2009EP2110514A2 Asymmetrical rotor blade fir tree attachment
10/21/2009EP2110513A2 Reduced weight blade for a gas turbine engine
10/21/2009EP2110512A1 Turbine blade twist angle correction tooling
10/21/2009EP2110457A2 Platinum-modified cathodic arc coating
10/21/2009EP2110449A1 Heat resistant member
10/21/2009EP2110193A1 Method for blisk milling
10/21/2009EP1828546B1 Stacked annular components for turbine engines
10/21/2009EP1373593B1 Method and device for gas phase diffusion coating of metal components
10/21/2009CN201330619Y Industrial exhaust heat steam and pneumatic helical engine
10/21/2009CN100552189C Heated wall surface cooling structure and gas turbine impeller vane with the same
10/20/2009US7604199 Aerofoil containment structure
10/20/2009CA2569026C Wall configuration of axial-flow machine, and gas turbine engine
10/20/2009CA2480989C Teardrop film cooled blade
10/20/2009CA2396216C Process for making a one-piece rotor blade and corresponding blade
10/15/2009WO2009126194A1 Segmented thermal barrier coating
10/15/2009WO2009126191A2 Sealing arrangement for turbine engine having ceramic components
10/15/2009WO2009124949A1 Turbomachine rotor comprising an anti-wear plug, and anti-wear plug
10/15/2009WO2009124585A1 Turbine device
10/15/2009WO2009082581A3 Main rotor blade with integral tip section
10/15/2009WO2009071521A3 Device for dynamically measuring the imbalance of the rotor of a turbocharger
10/15/2009US20090257878 Low exhaust loss turbine and method of minimizing exhaust losses
10/15/2009US20090257877 Asymmetrical rotor blade fir-tree attachment
10/15/2009US20090257876 Blower Impeller with Partial Tip Blockage
10/15/2009US20090257875 Platformless turbine blade
10/15/2009US20090255267 Comubstor seal having multiple cooling fluid pathways
10/15/2009DE102008017793A1 Vorrichtung und Verfahren zur Fixierung eines Werkstücks Apparatus and method for securing a workpiece
10/15/2009CA2720807A1 Turbomachine rotor comprising an anti-wear plug, and anti-wear plugi-usu
10/14/2009EP2108785A2 Turbine blade and vane assembly with a ceramic platform
10/14/2009EP2108784A2 Flow machine with fluid injector component group
10/14/2009EP2108715A2 Thermal barrier coating system and coating methods for gas turbine engine shroud
10/14/2009EP2108477A1 Gas turbine hot gas component repair method
10/14/2009EP1642005B1 Turbine blade
10/14/2009CN201326456Y Gas engine power generation muffler
10/14/2009CN101558235A Flow deflection devices and method for energy capture machines
10/13/2009US7600979 CMC articles having small complex features
10/13/2009US7600978 Hollow CMC airfoil with internal stitch
10/13/2009US7600977 Turbine blade tip cap
10/13/2009US7600973 Blades for gas turbine engines
10/13/2009US7600972 Methods and apparatus for cooling gas turbine engine rotor assemblies
10/13/2009US7600966 Turbine airfoil with improved cooling
10/08/2009WO2009122040A1 Method for manufacturing hollow blade
10/08/2009WO2009121768A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed after a finish-milling step
10/08/2009WO2009121767A1 Method for producing a one-piece bladed disc by abrasive water-jet cutting
10/08/2009WO2009121765A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed before a finish-milling step
10/08/2009WO2009121764A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring
10/08/2009WO2009121762A1 Improved method for making a one-piece bladed disk, with temporary retaining ring for bladed disks removed before a milling step
10/08/2009WO2009121716A1 Blade for a gas turbine
10/08/2009WO2009121715A1 Cooling duct arrangement within a hollow-cast casting
10/08/2009WO2009121465A1 Exhaust gas turbocharger for an internal combustion engine
10/08/2009US20090252615 Cooled Turbine Rotor Blade
10/08/2009US20090252613 Repair of gas turbine blade tip without recoating the repaired blade tip
10/08/2009US20090252612 Blade and gas turbine
10/08/2009US20090252611 Axial compressor blade retention
10/08/2009US20090252610 Turbine blade retention system and method
10/08/2009US20090252609 Impeller for supercharger and method of manufacturing the same
10/08/2009DE202009008513U1 Umlenkschaufeln für Gleichdruckturbinen mit Überschallströmung Turning vanes for constant-pressure turbines with supersonic flow
10/08/2009DE10350946B4 Turbinendüsenhaltevorrichtung an der horizontalen Verbindungsfläche des Trägers Turbine nozzle holder at the horizontal joint surface of the carrier
10/08/2009DE102009003714A1 Turbinenschaufelhaltesystem und -verfahren Turbine blade retention system and method
10/08/2009DE102009003712A1 Axialverdichter-Laufschaufelhalterung Axial compressor blade holder
10/08/2009DE102009003710A1 Schaufelblatt für einen Leitapparat mit einem maschinell bearbeiteten kontourierten Kanal darin Airfoil for a diffuser with a machined contoured channel therein
10/08/2009DE102008017624A1 Verfahren zur aerodynamischen Ausformung der Vorderkante von Bliskschaufeln A method for aerodynamic shaping of the front edge of the blisk blades
10/08/2009DE102008017495A1 Verfahren zur Herstellung von integral beschaufelten Rotoren A method of manufacturing integrally bladed rotors
10/08/2009DE102008017494A1 Verfahren zur Fertigung integral beschaufelter Rotoren Method for manufacturing integrally bladed rotors
10/08/2009DE102008016937A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine
10/08/2009DE102008016800A1 Gasturbinenverdichter Gas turbine compressor
10/08/2009DE102008015913A1 Vorrichtung zum Schweißen mit einer Prozesskammer und ein Schweißverfahren Apparatus for welding with a process chamber and a welding method
10/08/2009CA2719355A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed after a finish-milling step
10/08/2009CA2719354A1 Method for producing a one-piece bladed disc by abrasive water-jet cutting
10/08/2009CA2719352A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring which is removed before a finish-milling step
10/08/2009CA2719351A1 Improved method for producing a one-piece bladed disc, with temporary blade-supporting ring
10/08/2009CA2719350A1 Improved method for making a one-piece bladed disk, with temporary retaining ring for bladed disks removed before a milling step
10/08/2009CA2718801A1 Method for manufacturing hollow blade
10/07/2009EP2107215A1 Gas turbine airfoil
10/07/2009EP2107214A1 Chambered airfoil cooling
10/07/2009EP2106877A1 Method for the fabrication of integrally bladed rotors
10/07/2009EP2106876A1 Method for aerodynamically shaping the leading edge of blisk blades
10/07/2009EP2106873A1 Method of producting integrally bladed rotors using orbital friction welding
10/07/2009EP1971761B1 Method and apparatus for balancing an electrically assisted turbocharger rotor
10/07/2009EP1834066B1 Turbine blade for a gas turbine, use of a turbine blade and method for cooling a turbine blade
10/07/2009CN101550845A Turbine blade retention system and method
10/07/2009CN101550844A Inner turbine shell support configuration and methods
10/07/2009CN101550843A 燃气轮机翼型 Gas turbine airfoil
10/06/2009US7597843 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
10/06/2009US7597540 Turbine blade with showerhead film cooling holes
10/06/2009US7597539 Turbine blade with vortex cooled end tip rail
10/06/2009US7597536 Turbine airfoil with de-coupled platform
10/06/2009US7597535 Fan module and its fan casing
10/06/2009US7597533 BOAS with multi-metering diffusion cooling
10/01/2009WO2009120778A2 Subsonic and stationary ramjet engines
10/01/2009WO2009120629A1 High temperature resistant coating compositions
10/01/2009WO2009119345A1 Alloy material having high-temperature corrosion resistance, heat-shielding coating material, turbine member, and gas turbine