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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03/05/2014 | EP2703507A1 Ni base alloy and gas turbine blade and gas turbine utilizing the same |
03/05/2014 | EP2703111A1 Friction bonding method and bonding structure |
03/05/2014 | EP2702249A2 Tertiary lock system for thrust reversing mechanism |
03/05/2014 | CN103620164A Turbine engine part forming a compressor stator or turbine nozzle, and method for manufacturing same |
03/05/2014 | CN103615410A Rotor set |
03/05/2014 | CN102203389B Gas turbine having sealing plates on turbine disc |
03/05/2014 | CN102177012B Method of manufacturing polymer composite member by use of two or more resins |
03/05/2014 | CN101842582B Wind turbine blade with submerged boundary layer control means |
03/04/2014 | US8662855 Integrally woven composite fan blade using progressively larger weft yarns |
03/04/2014 | US8662849 Component of a turbine bucket platform |
03/04/2014 | US8662848 Water impeller |
03/04/2014 | US8662845 Multi-function heat shield for a gas turbine engine |
03/04/2014 | US8662844 Turbine vane and gas turbine |
03/04/2014 | US8662826 Cooling circuit for a drum rotor |
03/04/2014 | US8662825 Cooled aerofoil blade or vane |
03/04/2014 | US8661669 Method of making and joining an aerofoil and root |
03/04/2014 | CA2583847C Axial retaining device for turbomachine rotor disk flange |
02/27/2014 | WO2014031275A1 Gas turbine engine airfoil internal cooling features |
02/27/2014 | WO2014031203A2 Airfoil cover system |
02/27/2014 | WO2014031202A2 Assembled blade platform |
02/27/2014 | WO2014031195A2 Gas turbine engine fan blade tip treatment |
02/27/2014 | WO2014031189A1 Asymmetrically shaped trailing edge cooling holes |
02/27/2014 | WO2014031160A1 Compliant cantilevered airfoil |
02/27/2014 | WO2014029728A1 Internally cooled airfoil for a rotary machine |
02/27/2014 | WO2014007893A3 Geared turbofan with three turbines with first two counter-rotating, and third co-rotating with the second turbine |
02/27/2014 | WO2013172893A3 Composite airfoil with local tailoring of material properties |
02/27/2014 | WO2013162672A3 Gas turbine engine sump pressurization system |
02/27/2014 | US20140056719 Gas Turbine, Gas Turbine Blade, and Manufacturing Method of Gas Turbine Blade |
02/27/2014 | US20140056718 Inlet shroud assembly |
02/27/2014 | US20140056717 Gas turbine engine airfoil internal cooling features |
02/27/2014 | US20140056716 Bicast turbine engine components |
02/27/2014 | US20140056714 Turbomachine rotor having dovetail slot and method of machining |
02/27/2014 | US20140056713 Turbine engine rotor assembly |
02/27/2014 | US20140056712 Turbine bucket including an integral rotation controlling feature |
02/27/2014 | US20140056711 Aircraft engine annular shroud comprising an opening for the insertion of blades |
02/27/2014 | US20140056578 Heating Fan |
02/27/2014 | DE102013108860A1 Turbinenschaufel mit integraler Drehkontrolleinrichtung Turbine blade with integral rotary control device |
02/26/2014 | EP2700788A1 Vane or blade with tip cap |
02/26/2014 | EP2700787A1 Vane member and rotary machine |
02/26/2014 | EP2699764A1 Blade for a thermal turbomachine |
02/26/2014 | EP2699763A1 Cooled airfoil in a turbine engine |
02/26/2014 | EP2699713A1 Layer system having a two-ply metal layer |
02/26/2014 | CN203452854U First-stage moving blade suitable for 20-30WM grade combustion engine turbine |
02/26/2014 | CN103608641A Method and device for measuring a part in a turbine engine |
02/26/2014 | CN103608593A Turbomachine element |
02/26/2014 | CN103608546A Impingement cooling of turbine blades or vanes |
02/26/2014 | CN103603695A Blade alloy groove and processing method thereof |
02/26/2014 | CN103603694A Structure used for lowering work temperature of steam turbine main shaft bearing portion |
02/26/2014 | CN103603693A Hollow-shaft new power engine |
02/26/2014 | CN102359397B 1300mm moving blade of final stage for full-rotary-speed steam turbine |
02/26/2014 | CN102213115B Device and method for monitoring and controlling security risk of turbine movable blade on line |
02/25/2014 | US8657581 Thermoplastic rotor blade |
02/25/2014 | US8657579 Blade for use with a rotary machine and method of assembling same rotary machine |
02/25/2014 | US8657577 Gas turbine with securing plate between blade base and disk |
02/25/2014 | US8657576 Rotor blade |
02/25/2014 | US8657574 System and method for cooling a turbine bucket |
02/25/2014 | US8657561 Variable shape rotor blade |
02/25/2014 | US8656589 Aerofoil assembly and a method of manufacturing an aerofoil assembly |
02/25/2014 | CA2610278C Turbojet arrow blade |
02/25/2014 | CA2587096C Aircraft engine compressor assembly comprising hammer attachment blades with inclined roots |
02/25/2014 | CA2585875C Rotor blade retention system |
02/25/2014 | CA2573034C Balance weight, rotor disk thus equipped, rotor and aircraft engine comprising them |
02/25/2014 | CA2571900C Method for repairing a turbine engine vane assembly and repaired assembly |
02/20/2014 | WO2014028421A1 Gas turbine engine airfoil profile |
02/20/2014 | WO2014028419A1 Thermal barrier coating having outer layer |
02/20/2014 | WO2014028214A1 Compressor wheel of the compressor of an exhaust-gas turbocharger |
02/20/2014 | WO2014028138A1 Trailing edge cooling configuration for a gas turbine engine airfoil |
02/20/2014 | WO2014028077A1 Embedded actuators in composite airfoils |
02/20/2014 | WO2014028056A1 Contoured flowpath surface |
02/20/2014 | WO2014027162A1 Method for measuring the temperature reached by a part, in particular of a turbomachine |
02/20/2014 | WO2013191771A3 Process for producing ceramic composite components |
02/20/2014 | WO2013104852A3 Fibrous preform of a turbomachine blade made of composite material with in-built platform, and method of producing same |
02/20/2014 | WO2013088039A3 Fiber structure having variable-count threads |
02/20/2014 | US20140050893 Airfoil components containing ceramic-based materials and processes therefor |
02/20/2014 | US20140050590 Intentionally frequency mistuned turbine blades |
02/20/2014 | US20140050589 Hybrid structure airfoil |
02/20/2014 | US20140050581 Erosion protection system and method |
02/20/2014 | US20140050563 Stacked wheel assembly for a turbine system and method of assembling |
02/20/2014 | US20140047842 Suction side turbine blade tip cooling |
02/20/2014 | DE102012212896A1 Laufrad eines Abgasturboladers Impeller of an exhaust turbocharger |
02/19/2014 | EP2698501A1 Gas turbine rotor blade and gas turbine |
02/19/2014 | EP2698452A2 Creep-resistant environmental barrier coatings |
02/19/2014 | EP2698451A2 Cavitation-resistant environmental barrier coating |
02/19/2014 | EP2698223A2 A process of welding to repair thick sections using two arcwelding devices and a laser device; corresponding welding apparatus |
02/19/2014 | EP2697483A2 A wind turbine blade comprising metal fibres and a transition region |
02/19/2014 | EP2697482A1 Low pressure cooling seal system for a gas turbine engine |
02/19/2014 | EP2697048A2 Wind turbine blade with elongated fastening members in the root region thereof |
02/19/2014 | EP2697047A2 Wind turbine blade comprising cylindrical metal inserts in a root region thereof |
02/19/2014 | EP2697046A2 Wind turbine blade with tapering root bushings |
02/19/2014 | EP2697045A2 Wind turbine blade having a root region with elongated fastening members provided with metal fibres |
02/19/2014 | CN203441545U Bolt shaft tightening impeller and connection structure of impeller and turbine shaft |
02/19/2014 | CN103597169A Device and method for driving out blades retained in a form-fit manner in a rotor disk |
02/19/2014 | CN102766837B Novel thermal barrier coating |
02/18/2014 | US8651820 Dovetail connection for turbine rotating blade and rotor wheel |
02/18/2014 | US8651814 Axial flow fan with hub isolation slots |
02/18/2014 | US8651813 Fluid dynamic body having escapelet openings for reducing induced and interference drag, and energizing stagnant flow |
02/18/2014 | US8651799 Turbine nozzle slashface cooling holes |
02/18/2014 | CA2693046C Fan blade platform |
02/18/2014 | CA2567888C Method for producing a leak prevention unit for a sealing labyrinth, thermomechanical part and turbine engine comprising such a leak prevention unit |
02/13/2014 | WO2014025758A1 Turbine blade staking pin |