Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
11/2013
11/20/2013CN103403298A A turbine wheel, a turbine and use thereof
11/20/2013CN103403297A Horizontal axis airfoil turbine
11/20/2013CN103402691A Method for producing a metal component such as a turbomachine blade reinforcement
11/20/2013CN103402687A Gas tungsten arc welding using flux coated electrodes
11/20/2013CN103397912A Turbine engine rotor blade, turbine and turbine engine
11/20/2013CN103397911A Compound nozzle cooled engine
11/20/2013CN101446210B Shank shape for a turbine blade and turbine incorporating the same
11/19/2013US8585370 Rotor blade, rotor blade element and production process
11/19/2013US8585369 Device for axial retention of mobile vanes mounted on a rotor disc
11/19/2013US8585365 Turbine blade with triple pass serpentine cooling
11/19/2013US8585360 Turbine vane nominal airfoil profile
11/19/2013US8585358 Wind turbine generator including air-cooled heat exchanger
11/19/2013US8585351 Gas turbine blade
11/19/2013CA2758468C Improvements in or relating to composite structures
11/19/2013CA2682570C Gas turbine engine
11/19/2013CA2535205C Crescentic ramp turbine stage
11/19/2013CA2478750C Thermal barrier compound, superalloy mechanical part coated with such a compound, ceramic coating, and process for manufacturing the said coating
11/14/2013WO2013170157A1 Repair of directionally solidified alloys
11/14/2013WO2013169754A1 Repair method of a turbine blade tip
11/14/2013WO2013169747A1 Turbine blade with chamfered squealer tip formed from multiple components and convective cooling holes
11/14/2013WO2013169604A1 Blade tip having a recessed area
11/14/2013WO2013169471A1 Turbine airfoil trailing edge cooling slot
11/14/2013WO2013169435A1 Turbine airfoil trailing edge cooling hole plug and slot
11/14/2013WO2013169322A1 Convective shielding cooling hole pattern
11/14/2013WO2013169272A1 Wear resistant article
11/14/2013WO2013169271A1 Wear resistant turbine fan blade
11/14/2013WO2013169270A1 Rotor disk with a composite lubricating sheet
11/14/2013WO2013167847A2 Tool for manufacturing a foundry core for a turbine engine blade
11/14/2013WO2013167513A1 Method for manufacturing of components made of single crystal (sx) or directionally solidified (ds) superalloys
11/14/2013WO2013167346A1 Turbine rotor blade and axial rotor blade section for a gas turbine
11/14/2013WO2013167313A1 Airfoil with mcraly coating, corresponding airfoil arrangement and manufacturing method
11/14/2013WO2013167312A1 Airfoil arrangement with ptal bond coating and thermal barrier coating, and corresponding manufacturing method
11/14/2013WO2013166627A1 Double-area turbine of turbine boosting
11/14/2013WO2013141939A3 Method of manufacturing a turbomachine component, an airfoil and a gas turbine engine
11/14/2013WO2013122635A3 Gas turbine fan composite containment case and methods of manufacture
11/14/2013US20130302179 Turbine airfoil trailing edge cooling hole plug and slot
11/14/2013US20130302178 Asymmetrically shaped trailing edge cooling holes
11/14/2013US20130302177 Turbine airfoil trailing edge bifurcated cooling holes
11/14/2013US20130302176 Turbine airfoil trailing edge cooling slot
11/14/2013US20130302174 Archimdean screw apparatus
11/14/2013US20130302173 Wear resistant turbine fan blade
11/14/2013US20130302172 Space frame structure
11/14/2013US20130302171 Device for attaching blades to a turbine engine rotor disk
11/14/2013US20130302170 Rotor disk and rotor assembly
11/14/2013US20130302169 Rotor assembly for an axial turbine
11/14/2013US20130302166 Turbine blade with chamfered squealer tip formed from multiple components and convective cooling holes
11/14/2013US20130302163 Method and apparatus for connecting turbine rotors
11/14/2013US20130302162 Blade tip having a recessed area
11/14/2013US20130302145 Wind turbine
11/14/2013US20130302141 Convective Shielding Cooling Hole Pattern
11/14/2013DE102012207735A1 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
11/13/2013EP2662533A2 Cover segment for blade mounting region, corresponding system and method of mounting
11/13/2013EP2662531A1 Steam turbine stator blade and steam turbine
11/13/2013EP2662530A1 Airfoil with MCrAlY coating, corresponding airfoil arrangement and manufacturing method
11/13/2013EP2662529A1 Airfoil with PtAl bond coating and TBC, corresponding airfoil arrangement and manufacturing method
11/13/2013EP2662528A2 Gas turbine engine component with cooling holes having a multi-lobe configuration
11/13/2013EP2661542A1 Method for damping a gas-turbine blade, and vibration damper for implementing same
11/13/2013EP2661541A1 Method for producing a protective layer for a rotor blade
11/13/2013EP2661461A1 Resins or resin systems, and fibre composites
11/13/2013EP2661370A1 Alloy, protective layer and component
11/13/2013CN103388492A System and method for covering blade mounting region of turbine blade
11/12/2013US8579594 Wind turbine blade with submerged boundary layer control means
11/12/2013US8579593 Damping element for reducing the vibration of an airfoil
11/12/2013US8579591 Centrifugal compressor impeller
11/12/2013US8579590 Turbomachinery blade having a platform relief hole, platform cooling holes, and trailing edge cutback
11/12/2013CA2729130C Double flow compressor
11/12/2013CA2663076C Method and apparatus for production of a cast component
11/12/2013CA2517202C Offset coriolis turbulator blade
11/07/2013WO2013166284A1 Shaped rim cavity wing surface
11/07/2013WO2013165865A1 Hollow fan blade with braided fabric tubes
11/07/2013WO2013165840A1 A low stress turbocharger turbine wheel having a threaded through bore mount
11/07/2013WO2013165716A1 Reduced stress superback wheel
11/07/2013WO2013165527A2 High order shaped curve region for an airfoil
11/07/2013WO2013165521A2 Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections
11/07/2013WO2013165518A2 Gas turbine engine component with cusped, lobed cooling hole
11/07/2013WO2013165517A2 Gas turbine engine component with diffusive cooling hole
11/07/2013WO2013165515A2 Gas turbine engine with fan-tied inducer section
11/07/2013WO2013165511A2 Edm method for multi-lobed cooling hole
11/07/2013WO2013165510A2 Multi-lobed cooling hole and method of manufacture
11/07/2013WO2013165509A2 Multi-lobed cooling hole
11/07/2013WO2013165508A2 Multi-lobed cooling hole array
11/07/2013WO2013165507A2 Cooling hole with asymmetric diffuser
11/07/2013WO2013165506A2 Cooling hole with crenellation features
11/07/2013WO2013165504A2 Manufacturing methods for multi-lobed cooling holes
11/07/2013WO2013165503A2 Cooling hole with enhanced flow attachment
11/07/2013WO2013165502A2 Cooling hole with thermo-mechanical fatigue resistance
11/07/2013WO2013165495A2 Apparatus and method for optically measuring creep
11/07/2013WO2013133875A3 Composite rotor and vane assemblies with integral airfoils
11/07/2013WO2013065023A8 Method for making a shaped turbine aerofoil
11/07/2013US20130294927 System and method for covering a blade mounting region of turbine blades
11/07/2013US20130294926 Antifouling film, air blower blade provided with same, air blower, and antifouling coating material
11/07/2013US20130294925 Core for a composite structure and method of fabrication thereof
11/07/2013US20130294924 Method for manufacturing a turbine engine part by injection of resin under pressure
11/07/2013US20130294923 Wind turbine rotor blade and wind turbine for wind power generation
11/07/2013US20130294920 Method of making a metal reinforcing piece
11/07/2013US20130294913 Turbine blade with tuned damping structure
11/06/2013EP2660426A2 Turbine assembly
11/06/2013EP2660425A2 Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same
11/06/2013EP2660424A1 Inter-turbine ducts with variable area ratios
11/06/2013EP2660423A1 Blade body and rotary machine
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