Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2013
08/29/2013US20130224024 Rotor blade for wind turbine with movable control surface
08/29/2013US20130224019 Turbine cooling system and method
08/29/2013US20130224017 Mission adaptive rotor blade
08/29/2013US20130224014 Low loss airfoil platform trailing edge
08/29/2013US20130223986 Gas turbine engine with fan-tied inducer section and multiple low pressure turbine sections
08/29/2013US20130223980 Active grill shutter vane design and vehicle system
08/29/2013DE102012203144A1 Strömungsmaschine Flow machine
08/29/2013DE102012203047A1 Lagervorrichtung und Turbomaschine mit Lagervorrichtung Storage device and turbomachinery bearing device
08/29/2013CA2807678A1 Nano-metal coated vane component for gas turbine engines and method of manufacturing same
08/28/2013EP2631491A1 Transonic blade
08/28/2013EP2631490A1 Radial-flow impeller with radially free base ring
08/28/2013EP2631435A1 Turbine engine variable stator vane
08/28/2013EP2631432A1 Steam turbine rotor
08/28/2013EP2631431A1 Aerofoil Cooling Arrangement
08/28/2013EP2631430A1 Interlaminar stress reducing configuration for composite turbine components
08/28/2013EP2631429A1 Blades
08/28/2013EP2631428A1 Turbine nozzle segment
08/28/2013EP2631427A2 Balancing of Rotors
08/28/2013EP2631324A1 Ni-based superalloy member having heat-resistant bond coat layer formed therein
08/28/2013EP2631323A1 Erosion and fatigue resistant blade and blade coating
08/28/2013EP2631321A1 Ceramic heat insulation layer system with external high aluminium layer and method
08/28/2013EP2630334A1 Repair of a turbine engine component having surface opening crevices
08/28/2013CN203161306U Multi-stage steam turbine adopting wheel disc drawbar structure
08/28/2013CN103270312A Rotor structure
08/28/2013CN103270249A Repair of a turbine engine component having surface opening crevices
08/28/2013CN103266921A External combustion ring cylinder engine
08/28/2013CN101929357B Systems, methods, and apparatus for thermally isolating a turbine rotor wheel
08/28/2013CN101852099B Film-cooling augmentation device and turbine airfoil incorporating the same
08/27/2013US8518485 Process for producing a component of a turbine, and a component of a turbine
08/27/2013US8517689 Multi-segment wind turbine rotor blade with span-wise offset joints
08/27/2013US8517688 Rotor assembly for use in turbine engines and methods for assembling same
08/27/2013US8517687 Gas turbine engine compressor and turbine section assembly utilizing tie shaft
08/27/2013US8517686 Flow passage for gas turbine engine
08/27/2013US8517684 Turbine blade with multiple impingement cooled passages
08/27/2013US8517677 Advanced booster system
08/27/2013US8517675 Blower fan for low profile environment
08/27/2013US8517667 Turbine vane with counter flow cooling passages
08/27/2013US8517666 Turbine cooling air sealing
08/22/2013WO2013123502A1 System and method for blade retention
08/22/2013WO2013123121A1 Gas turbine engine component with multi-lobed cooling hole
08/22/2013WO2013123120A1 Gas turbine engine component with impingement and lobed cooling hole
08/22/2013WO2013123115A1 Gas turbine engine component with impingement and diffusive cooling
08/22/2013WO2013123012A1 Gas turbine engine component with compound cusp cooling configuration
08/22/2013WO2013123006A1 Gas turbine engine component with cusped cooling hole
08/22/2013WO2013122913A1 Cooling hole with curved metering section
08/22/2013WO2013122910A1 Multi-lobed cooling hole
08/22/2013WO2013122908A1 Multiple diffusing cooling hole
08/22/2013WO2013122906A1 Tri-lobed cooling hole and method of manufacture
08/22/2013WO2013120999A1 Method for producing a near-surface cooling passage in a thermally highly stressed component, and component having such a passage
08/22/2013WO2013120552A1 Impingement cooling of turbine blades or vanes
08/22/2013US20130216395 Gas turbine blade
08/22/2013US20130216391 Method for the production of a one-piece rotor area and one-piece rotor area
08/22/2013US20130216389 Interlaminar stress reducing configuration for composite turbine components
08/22/2013US20130216387 System and method for blade retention
08/22/2013US20130216383 Combined sealing and balancing arrangement for a turbine disc
08/22/2013US20130216382 Hub Assembly with Centrifugal and Radial Bearings
08/22/2013US20130216381 Oscillating foil turbine
08/22/2013US20130213039 Bladeless Turbine
08/22/2013DE10361882B4 Rotor für die Hochdruckturbine eines Flugtriebwerks Rotor for the high-pressure turbine of an aircraft engine
08/22/2013DE102012202272A1 Rotor Rotor
08/22/2013CA2806398A1 Interlaminar stress reducing configuration for composite turbine components
08/21/2013EP2628905A2 Turbomachine hot-section component protrusion, corresponding component and method of augmentIng a surface area
08/21/2013EP2628903A2 Gas Turbine Engine Airfoil Cooling Circuit
08/21/2013EP2628902A2 Tip shrouded blade and corresponding turbine system
08/21/2013EP2628901A1 Turbine blade with impingement cooling
08/21/2013EP2628900A1 Turbine vane with a throttling element
08/21/2013EP2628899A2 Turbomachine flow improvement system
08/21/2013EP2628898A2 Turbomachine Including Flow Improvement System
08/21/2013EP2628897A2 Gas turbine system
08/21/2013EP2628825A1 Coated article and process of coating an article
08/21/2013EP2628816A1 Method for applying a heat insulation layer
08/21/2013EP2627909A2 Thermally insulating turbine coupling
08/21/2013EP2627868A1 A bolt retention clip
08/21/2013CN203146032U Novel bacteria type blade root
08/21/2013CN103261700A Turbine engine blade having improved stacking law
08/21/2013CN103261584A Impingement cooling of gas turbine blades or vanes
08/21/2013CN103256078A Tip shrouded blade
08/21/2013CN103256077A Multistage centripetal turbine system
08/21/2013CN102182517B Boundary layer turbine with blade plate
08/21/2013CN101852097B Systems, methods, and apparatus for passive purge flow control in a turbine
08/20/2013US8512874 Coating systems containing beta phase and gamma-prime phase nickel aluminide
08/20/2013US8512488 Ni—Fe based forging superalloy excellent in high-temperature strength and high-temperature ductility, method of manufacturing the same, and steam turbine rotor
08/20/2013US8512004 Propeller fan
08/20/2013US8512003 Tip ramp turbine blade
08/20/2013US8512002 Method of manufacturing an aerofoil
08/20/2013US8511999 Multiple piece turbine rotor blade
08/20/2013US8511998 Slurry pump impeller
08/20/2013US8511995 Turbine blade with platform cooling
08/20/2013US8511994 Serpentine cored airfoil with body microcircuits
08/20/2013US8511993 Application of dense vertically cracked and porous thermal barrier coating to a gas turbine component
08/20/2013US8511992 Minimization of fouling and fluid losses in turbine airfoils
08/20/2013US8511991 Composite turbine blade and method of manufacture thereof
08/20/2013US8511990 Cooling hole exits for a turbine bucket tip shroud
08/20/2013US8511977 Heat transfer passage
08/20/2013US8511976 Turbine seal system
08/20/2013US8511968 Turbine vane for a gas turbine engine having serpentine cooling channels with internal flow blockers
08/20/2013CA2585815C Airfoil optimized for a turbine blade
08/15/2013WO2013119652A1 Electroformed sheath
08/15/2013WO2013116927A1 Mounting in hub for blades of a hydro turbine
08/15/2013US20130209271 Gas turbine blade, manufacturing method therefor, and gas turbine using turbine blade
1 ... 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 ... 330