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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02/16/2012 | WO2012021194A2 Component wall having diffusion sections for cooling in a turbine engine |
02/16/2012 | WO2012020195A1 Device for locking a root of a rotor blade |
02/16/2012 | WO2012019975A1 Gas turbine vane |
02/16/2012 | WO2012019684A1 Method for repairing gas turbine components of ceramic composite materials and device for carrying out the method |
02/16/2012 | WO2011081768A3 Turbine blade damping device with controlled loading |
02/16/2012 | US20120039722 Geared Compressor Rotor For Cold Gas Applications |
02/16/2012 | US20120039721 Impeller for mixing slurry in metallurgical processes |
02/16/2012 | US20120039719 Rotor section for a rotor of a turbomachine, and rotor blade for a turbomachine |
02/16/2012 | US20120039718 Casting apparatus for producing a turbine rotor blade of a gas turbine and turbine rotor blade |
02/16/2012 | US20120039717 Ceiling fan |
02/16/2012 | US20120039716 Guide vane system for a turbomachine having segmented guide vane carriers |
02/16/2012 | US20120039706 Compressor having a guide vane assembly with a radially variable outflow |
02/16/2012 | DE102010036042B3 Verfahren zum Rekonturieren einer Kompressor- oder Turbinenschaufel für eine Gasturbine A method for recontouring a compressor or turbine blade for a gas turbine |
02/16/2012 | DE102010033889A1 System for influencing barrier layer in rotor blades of e.g. bypassing engines of helicopter, has set of apertures formed in location at outer skin of rotor blade, where flow medium is pumped in radial direction by hollow channel |
02/16/2012 | CA2807556A1 Device for locking a root of a rotor blade |
02/16/2012 | CA2802153A1 Component wall having diffusion sections for cooling in a turbine engine |
02/15/2012 | EP2418367A1 Cooling assembly and method for a gas-turbine electric power generating plant and gas-turbine electric power generating plant comprising said cooling assembly |
02/15/2012 | EP2418357A1 Turbine airfoil and method for thermal barrier coating |
02/15/2012 | EP2418356A1 Turbine inter-platform damper and corresponding turbine blade |
02/15/2012 | EP2418355A1 Gas turbine vane |
02/15/2012 | EP2418354A1 Method for producing an internally cooled turbine blade and gas turbine with a turbine blade produced according to the method |
02/15/2012 | EP2418353A2 An aerofoil, an aerofoil sub-assembly and a method of making the same |
02/15/2012 | EP2418352A2 Gas turbine engine and method for cooling the compressor of a gas turbine engine |
02/15/2012 | EP2418066A1 Injection moulding tool for producing a hybrid component |
02/15/2012 | EP2416950A1 A protected wind turbine blade, a method of manufacturing it and a wind turbine |
02/15/2012 | EP2416944A1 Method for producing a turbomachine blade made from a composite material |
02/15/2012 | EP2416910A1 Method for producing a turbine wheel for an exhaust gas turbocharger |
02/14/2012 | US8115329 Water turbine with bi-symmetric airfoil |
02/14/2012 | US8113802 Food centrifugal pump formed by stamping and welding having a seal arrangement between the impeller and casing |
02/14/2012 | US8113787 Turbomachine blade with erosion and corrosion protective coating and method of manufacturing |
02/14/2012 | US8113784 Coolable airfoil attachment section |
02/14/2012 | US8113783 Assembly of a fan blade and of its damper, fan blade damper and method for calibrating the damper |
02/14/2012 | US8113780 Castings, casting cores, and methods |
02/14/2012 | US8113779 Turbine blade with tip rail cooling and sealing |
02/14/2012 | US8113771 Spring system designs for active and passive retractable seals |
02/14/2012 | CA2487960C Improved low cycle fatigue life (lcf) impeller design concept |
02/09/2012 | WO2012017168A1 Process for manufacturing a turbomachine drum |
02/09/2012 | WO2012016981A1 Gas turbine engine comprising a tension stud |
02/09/2012 | WO2012016830A1 Gas turbine rotor comprising an axially displaceable turbine rotor shaft |
02/09/2012 | WO2012016789A1 Turbine airfoil and method for thermal barrier coating |
02/09/2012 | US20120034102 Bucket assembly cooling apparatus and method for forming the bucket assembly |
02/09/2012 | US20120034101 Turbine blade squealer tip |
02/09/2012 | US20120034100 Recessed metering standoffs for airfoil baffle |
02/09/2012 | US20120034099 Reinforcing Element for Use with a Ventilator Hub |
02/09/2012 | US20120034098 Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE INCORPORATING THE SAME |
02/09/2012 | US20120034097 Component with inspection-facilitating features |
02/09/2012 | US20120034092 Method for producing a plating of a vane tip and correspondingly produced vanes and gas turbines |
02/09/2012 | US20120034091 Aerofoil, an aerofoil sub-assembly and a method of making the same |
02/09/2012 | US20120034088 Method for Connecting a Tension-Torsion Strap |
02/09/2012 | US20120034087 Axial Turbomachine Rotor Having a Sealing Plate |
02/09/2012 | US20120034086 Swing axial entry dovetail for steam turbine buckets |
02/09/2012 | US20120034084 Process for producing a turbine wheel for an exhaust gas turbocharger |
02/09/2012 | US20120034083 Fan with area expansion between rotor and stator blades |
02/09/2012 | US20120034081 Compressor blade root heating system |
02/09/2012 | US20120034078 Impeller and centrifugal compressor including the same |
02/09/2012 | DE102011052307A1 Schwalbenschwanz zur schwenkenden axialen Einführung für Dampfturbinenlaufschaufeln Dovetail for pivotal axial insertion for steam turbine blades |
02/09/2012 | DE102011052033A1 Schaufelanordnungs-Kühlvorrichtung und Verfahren zum Herstellen der Schaufelanordnung Blade assembly cooling device and method of manufacturing the vane assembly |
02/09/2012 | DE102010033708A1 Turbine stage has series of adjacent profiled blades distributed in circumferential direction, where blades contain pressure surface and suction surface, and extends from end wall in radial manner |
02/09/2012 | DE102010033686A1 Gas turbine for use as turbofan engine, for aircraft in e.g. hot countries, has heat insulating layer provided on surface of blades of guide vane ring along flowing direction of working gas downstream behind profile center of gravity |
02/09/2012 | DE102010033302A1 Verfahren zum Überprüfen der Mechanischen Integrität von Stabilisierungselementen an den Laufschaufeln einer Turbine sowie Abtastvorrichtung zur Durchführung des Verfahrens Method for checking the integrity of the mechanical stabilization elements on the rotor blades of a turbine and scanning device for carrying out the method |
02/09/2012 | CA2806267A1 Process for manufacturing a turbomachine drum |
02/08/2012 | EP2416026A1 Power transmission for a gas turbine |
02/08/2012 | EP2415968A1 Method for Checking the Mechanical Integrity of Stabilizing Elements on the Rotor Blades of a Turbine and Scanning Device for Implementing the Method |
02/08/2012 | EP2415967A1 Gas turbine engine comprising a tension stud |
02/08/2012 | EP2415966A1 Power train for a gas turbine |
02/08/2012 | EP2415903A1 Thermal barrier coating material, thermal barrier coating, turbine member, and gas turbine |
02/08/2012 | EP2414641A1 Axial turbomachine rotor having sealing disc |
02/08/2012 | EP2414640A1 Blade for a gas turbine |
02/08/2012 | EP2414639A1 Cooled component for a gas turbine |
02/08/2012 | EP2414638A1 Turbine wheel with untuned blades comprising a damping device |
02/08/2012 | EP2414637A2 Rotor for a turbomachine |
02/08/2012 | EP2414305A1 Process for smoothing the surface of a part made of cmc material. |
02/08/2012 | EP2414127A2 Method for welding a recess in a component by means of sheeting for fusion welding applied outside or around the contour, and corresponding component |
02/08/2012 | EP2414125A1 Dual brazing alloy element comprising at least one first layer of an ni-based brazing alloy and also at least one second layer with active element, process for producing said element and uses thereof |
02/08/2012 | EP1989399B1 Roughened coating for gas turbine engine components |
02/08/2012 | CN102348867A Turbine vane with dusting hole at the base of the blade |
02/08/2012 | CN102345122A Multipurpose low-conductivity ceramic/noble metal lamellar composite thermal barrier coating |
02/08/2012 | CN101460706B 用于流体机械、尤其是用于蒸汽涡轮机的导向叶片 For fluid machinery, in particular, guide vanes for steam turbine |
02/08/2012 | CN101117897B 涡轮机叶片尖端罩 Turbine blade tip shroud |
02/07/2012 | US8109734 Article formed from a composite material |
02/07/2012 | US8109727 Wind turbine |
02/07/2012 | US8109726 Turbine blade with micro channel cooling system |
02/07/2012 | US8109725 Airfoil with wrapped leading edge cooling passage |
02/07/2012 | US8109722 Turbine and system for generating power from fluid flow and method therefor |
02/07/2012 | US8109712 Method of producing a turbine or compressor component, and turbine or compressor component |
02/07/2012 | CA2448465C Fabricated repair of cast nozzle |
02/07/2012 | CA2434487C Process for distributing turbomachine rotor blades |
02/05/2012 | CA2748070A1 Transverse axis turbine with controllable display |
02/02/2012 | WO2012013892A1 Inter-vane seal for a wheel of a turbine or a turbomachine compressor |
02/02/2012 | WO2011143064A3 Fan with overmolded blades |
02/02/2012 | US20120027619 Cast features for a turbine engine airfoil |
02/02/2012 | US20120027618 Angled blade root |
02/02/2012 | US20120027617 Turbine nozzle segment and method of repairing same |
02/02/2012 | US20120027616 Gas turbine blade with intra-span snubber and manufacturing method for producing the same |
02/02/2012 | US20120027615 Rotor blade |
02/02/2012 | US20120027614 Wind turbine blade multi-component shear web with intermediate connection assembly |
02/02/2012 | US20120027613 Wind turbine blade shear web connection assembly |
02/02/2012 | US20120027612 Wind turbine blade shear web connection assembly |
02/02/2012 | US20120027611 Compression member for wind turbine rotor blades |
02/02/2012 | US20120027610 Wind turbine blade shear web with spring flanges |