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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11/20/2013 | CN103403298A A turbine wheel, a turbine and use thereof |
11/20/2013 | CN103403297A Horizontal axis airfoil turbine |
11/20/2013 | CN103402691A Method for producing a metal component such as a turbomachine blade reinforcement |
11/20/2013 | CN103402687A Gas tungsten arc welding using flux coated electrodes |
11/20/2013 | CN103397912A Turbine engine rotor blade, turbine and turbine engine |
11/20/2013 | CN103397911A Compound nozzle cooled engine |
11/20/2013 | CN101446210B Shank shape for a turbine blade and turbine incorporating the same |
11/19/2013 | US8585370 Rotor blade, rotor blade element and production process |
11/19/2013 | US8585369 Device for axial retention of mobile vanes mounted on a rotor disc |
11/19/2013 | US8585365 Turbine blade with triple pass serpentine cooling |
11/19/2013 | US8585360 Turbine vane nominal airfoil profile |
11/19/2013 | US8585358 Wind turbine generator including air-cooled heat exchanger |
11/19/2013 | US8585351 Gas turbine blade |
11/19/2013 | CA2758468C Improvements in or relating to composite structures |
11/19/2013 | CA2682570C Gas turbine engine |
11/19/2013 | CA2535205C Crescentic ramp turbine stage |
11/19/2013 | CA2478750C Thermal barrier compound, superalloy mechanical part coated with such a compound, ceramic coating, and process for manufacturing the said coating |
11/14/2013 | WO2013170157A1 Repair of directionally solidified alloys |
11/14/2013 | WO2013169754A1 Repair method of a turbine blade tip |
11/14/2013 | WO2013169747A1 Turbine blade with chamfered squealer tip formed from multiple components and convective cooling holes |
11/14/2013 | WO2013169604A1 Blade tip having a recessed area |
11/14/2013 | WO2013169471A1 Turbine airfoil trailing edge cooling slot |
11/14/2013 | WO2013169435A1 Turbine airfoil trailing edge cooling hole plug and slot |
11/14/2013 | WO2013169322A1 Convective shielding cooling hole pattern |
11/14/2013 | WO2013169272A1 Wear resistant article |
11/14/2013 | WO2013169271A1 Wear resistant turbine fan blade |
11/14/2013 | WO2013169270A1 Rotor disk with a composite lubricating sheet |
11/14/2013 | WO2013167847A2 Tool for manufacturing a foundry core for a turbine engine blade |
11/14/2013 | WO2013167513A1 Method for manufacturing of components made of single crystal (sx) or directionally solidified (ds) superalloys |
11/14/2013 | WO2013167346A1 Turbine rotor blade and axial rotor blade section for a gas turbine |
11/14/2013 | WO2013167313A1 Airfoil with mcraly coating, corresponding airfoil arrangement and manufacturing method |
11/14/2013 | WO2013167312A1 Airfoil arrangement with ptal bond coating and thermal barrier coating, and corresponding manufacturing method |
11/14/2013 | WO2013166627A1 Double-area turbine of turbine boosting |
11/14/2013 | WO2013141939A3 Method of manufacturing a turbomachine component, an airfoil and a gas turbine engine |
11/14/2013 | WO2013122635A3 Gas turbine fan composite containment case and methods of manufacture |
11/14/2013 | US20130302179 Turbine airfoil trailing edge cooling hole plug and slot |
11/14/2013 | US20130302178 Asymmetrically shaped trailing edge cooling holes |
11/14/2013 | US20130302177 Turbine airfoil trailing edge bifurcated cooling holes |
11/14/2013 | US20130302176 Turbine airfoil trailing edge cooling slot |
11/14/2013 | US20130302174 Archimdean screw apparatus |
11/14/2013 | US20130302173 Wear resistant turbine fan blade |
11/14/2013 | US20130302172 Space frame structure |
11/14/2013 | US20130302171 Device for attaching blades to a turbine engine rotor disk |
11/14/2013 | US20130302170 Rotor disk and rotor assembly |
11/14/2013 | US20130302169 Rotor assembly for an axial turbine |
11/14/2013 | US20130302166 Turbine blade with chamfered squealer tip formed from multiple components and convective cooling holes |
11/14/2013 | US20130302163 Method and apparatus for connecting turbine rotors |
11/14/2013 | US20130302162 Blade tip having a recessed area |
11/14/2013 | US20130302145 Wind turbine |
11/14/2013 | US20130302141 Convective Shielding Cooling Hole Pattern |
11/14/2013 | DE102012207735A1 Vane cascade e.g. rotor-side moving vane cascade, for e.g. turbine, has front edge fillets formed in region of vane edges, where fillet height is larger or equal to thickness and fillet length is larger or equal to reverse flow section |
11/13/2013 | EP2662533A2 Cover segment for blade mounting region, corresponding system and method of mounting |
11/13/2013 | EP2662531A1 Steam turbine stator blade and steam turbine |
11/13/2013 | EP2662530A1 Airfoil with MCrAlY coating, corresponding airfoil arrangement and manufacturing method |
11/13/2013 | EP2662529A1 Airfoil with PtAl bond coating and TBC, corresponding airfoil arrangement and manufacturing method |
11/13/2013 | EP2662528A2 Gas turbine engine component with cooling holes having a multi-lobe configuration |
11/13/2013 | EP2661542A1 Method for damping a gas-turbine blade, and vibration damper for implementing same |
11/13/2013 | EP2661541A1 Method for producing a protective layer for a rotor blade |
11/13/2013 | EP2661461A1 Resins or resin systems, and fibre composites |
11/13/2013 | EP2661370A1 Alloy, protective layer and component |
11/13/2013 | CN103388492A System and method for covering blade mounting region of turbine blade |
11/12/2013 | US8579594 Wind turbine blade with submerged boundary layer control means |
11/12/2013 | US8579593 Damping element for reducing the vibration of an airfoil |
11/12/2013 | US8579591 Centrifugal compressor impeller |
11/12/2013 | US8579590 Turbomachinery blade having a platform relief hole, platform cooling holes, and trailing edge cutback |
11/12/2013 | CA2729130C Double flow compressor |
11/12/2013 | CA2663076C Method and apparatus for production of a cast component |
11/12/2013 | CA2517202C Offset coriolis turbulator blade |
11/07/2013 | WO2013166284A1 Shaped rim cavity wing surface |
11/07/2013 | WO2013165865A1 Hollow fan blade with braided fabric tubes |
11/07/2013 | WO2013165840A1 A low stress turbocharger turbine wheel having a threaded through bore mount |
11/07/2013 | WO2013165716A1 Reduced stress superback wheel |
11/07/2013 | WO2013165527A2 High order shaped curve region for an airfoil |
11/07/2013 | WO2013165521A2 Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections |
11/07/2013 | WO2013165518A2 Gas turbine engine component with cusped, lobed cooling hole |
11/07/2013 | WO2013165517A2 Gas turbine engine component with diffusive cooling hole |
11/07/2013 | WO2013165515A2 Gas turbine engine with fan-tied inducer section |
11/07/2013 | WO2013165511A2 Edm method for multi-lobed cooling hole |
11/07/2013 | WO2013165510A2 Multi-lobed cooling hole and method of manufacture |
11/07/2013 | WO2013165509A2 Multi-lobed cooling hole |
11/07/2013 | WO2013165508A2 Multi-lobed cooling hole array |
11/07/2013 | WO2013165507A2 Cooling hole with asymmetric diffuser |
11/07/2013 | WO2013165506A2 Cooling hole with crenellation features |
11/07/2013 | WO2013165504A2 Manufacturing methods for multi-lobed cooling holes |
11/07/2013 | WO2013165503A2 Cooling hole with enhanced flow attachment |
11/07/2013 | WO2013165502A2 Cooling hole with thermo-mechanical fatigue resistance |
11/07/2013 | WO2013165495A2 Apparatus and method for optically measuring creep |
11/07/2013 | WO2013133875A3 Composite rotor and vane assemblies with integral airfoils |
11/07/2013 | WO2013065023A8 Method for making a shaped turbine aerofoil |
11/07/2013 | US20130294927 System and method for covering a blade mounting region of turbine blades |
11/07/2013 | US20130294926 Antifouling film, air blower blade provided with same, air blower, and antifouling coating material |
11/07/2013 | US20130294925 Core for a composite structure and method of fabrication thereof |
11/07/2013 | US20130294924 Method for manufacturing a turbine engine part by injection of resin under pressure |
11/07/2013 | US20130294923 Wind turbine rotor blade and wind turbine for wind power generation |
11/07/2013 | US20130294920 Method of making a metal reinforcing piece |
11/07/2013 | US20130294913 Turbine blade with tuned damping structure |
11/06/2013 | EP2660426A2 Turbine assembly |
11/06/2013 | EP2660425A2 Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same |
11/06/2013 | EP2660424A1 Inter-turbine ducts with variable area ratios |
11/06/2013 | EP2660423A1 Blade body and rotary machine |