Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2013
05/01/2013EP2586982A2 Method and apparatus for cooling gas turbine rotor blades
05/01/2013EP2586981A2 Gas turbine engine component having wavy cooling channels with pedestals
05/01/2013EP2586980A2 Turbine blade rail damper
05/01/2013EP2586979A1 Turbomachine blade with tip flare
05/01/2013EP2586978A2 Turbine of a turbomachine
05/01/2013EP2586977A2 Turbine of a turbomachine
05/01/2013EP2586976A2 Turbine for a turbomachine
05/01/2013EP2586975A2 Turbine bucket with platform shaped for gas temperature control, corresponding turbine wheel and method of controlling purge air flow
05/01/2013EP2586974A2 Turbine bucket with platform leading edge scallop for performance and secondary flow, corresponding turbine wheel and method of controlling secondary purge air flow
05/01/2013EP2586973A1 Blade for a gas turbine engine
05/01/2013EP2586972A2 Airfoil devices, leading edge components, and methods of making such components
05/01/2013EP2586971A2 A spacer, a rotor, a spool and a method of orienting a rotor stack load path
05/01/2013EP2586970A2 Spoked spacer for a gas turbine engine
05/01/2013EP2586969A2 Spoked Rotor for a Gas Turbine Engine
05/01/2013EP2586968A2 Secondary flow arrangement for slotted rotor
05/01/2013EP2586967A2 Thermal plug for turbine bucket shank cavity and related method
05/01/2013EP2586562A2 Methods for repairing turbine blade tips
05/01/2013EP2586561A1 Movement strategy for producing a single crystal structure by build-up welding
05/01/2013EP2585721A1 Method for producing a metal reinforcement for a turbomachine blade
05/01/2013EP2585281A1 Turbomachine blade having an even/odd complementary geometry and its manufacturing process
05/01/2013EP2585280A1 Turbomachine blade with complementary asymetric geometry
05/01/2013EP2471965B1 Ni-based superalloy, and turbine rotor and stator blades for gas turbine using the same
05/01/2013CN202914142U Circumferential unload groove structure of installation edge of rotor part of gas turbine
05/01/2013CN1896463B Niobium silicide-based turbine components and related laser deposition method
05/01/2013CN103080479A Device for locking a root of a rotor blade
05/01/2013CN103080478A Turbine blade for a gas turbine
05/01/2013CN103080477A 燃气涡轮叶片 A gas turbine blade
05/01/2013CN103080476A Turbojet engine blade, in particular a guide blade, and turbojet engine receiving such blades
05/01/2013CN103079754A Method for recontouring a compressor or turbine blade or vane for a gas turbine
05/01/2013CN103079753A Method of servicing an airfoil assembly for use in a gas turbine engine
05/01/2013CN103075256A Turbomachine configured to burn ash-bearing fuel oils and method thereof
05/01/2013CN103075202A Impingement cooling structure with grid turbulence effect in turbine blade
05/01/2013CN103075201A Turbine cover plate assembly
05/01/2013CN103075200A Turbine bucket angel wing features for forward cavity flow control and related method
05/01/2013CN103075199A Turbine bucket and related method
05/01/2013CN103075198A Turbine bucket platform leading edge and related method
05/01/2013CN103075197A Turbine bucket platform shaping for gas temperature control and related method
05/01/2013CN103074550A Turbine rotor steel material resisting high temperature of 620 DEG C
05/01/2013CN102667063B Radial turbine
05/01/2013CN101796266B Seal coating between rotor blade and rotor disk slot in gas turbine engine
05/01/2013CN101294501B Turbomachine vane damper
05/01/2013CN101235728B Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method
04/2013
04/30/2013US8430636 Wind turbine rotor assembly
04/30/2013US8430623 Blade
04/30/2013CA2793459A1 Airfoil and method of fabricating the same
04/30/2013CA2793232A1 Component and method of fabricating the same
04/30/2013CA2776536A1 Blade for a gas turbine engine
04/30/2013CA2701312C Centrifugal compressor vane diffuser wall contouring
04/30/2013CA2699124C Hp turbine vane airfoil profile
04/30/2013CA2622020C Vane assembly with outer grommets
04/30/2013CA2497735C Rotor for a turbomachine
04/30/2013CA2427384C Ni-base sintered alloy
04/25/2013WO2013058220A1 Rotor blade support structure
04/25/2013WO2013056975A1 A cooled turbine guide vane or blade for a turbomachine
04/25/2013US20130101436 Fan rotor with cooling holes
04/25/2013US20130101432 Erosion Resistant Helicopter Blade
04/25/2013US20130101431 Rotor, a steam turbine and a method for producing a rotor
04/25/2013US20130101429 Turbomachine blade or vane having complementary asymmetrical geometry
04/25/2013US20130101424 Overflow vortex transfer system
04/25/2013US20130101422 Fastening assembly for blades of turbomachines having axial flow and method for producing such an assembly
04/25/2013US20130101421 Wear-resistant part for the support of a blade of a turbojet fan
04/25/2013US20130101400 Ram air fan inner housing
04/25/2013US20130101394 Free-surface liquid transfer device for rotating machinery
04/25/2013US20130098062 Compressor bleed cooling fluid feed system
04/25/2013DE102012109746A1 Rotor, Dampfturbine und Verfahren zur Herstellung eines Rotors Rotor, the steam turbine and method for manufacturing a rotor
04/25/2013DE102012109719A1 Zweiflutige Dampfturbine mit Dampfkühlung Double-flow steam turbine with steam cooling
04/25/2013DE102011085143A1 K3-Beschichtungsverfahren zur Bildung gut haftender und rissfester Beschichtungen sowie entsprechend beschichtendes Bauteil K3 coating process for forming good adhesion and crack-resistant coatings and coated in accordance with component
04/25/2013DE102011085105A1 Rotor shaft of a turbomachine, includes two shaft sections, where first shaft section comprises hollow plug receptacle, and second shaft section comprises plug-in projection for intervening the plug receptacle of the first shaft section
04/25/2013DE102010050185B4 Axialturbomaschine Axial turbomachine
04/25/2013DE102004036389B4 Turbinenschaufelfuß mit Mehrfachradiusnut für eine axiale Schaufelbefestigung Turbine blade with Mehrfachradiusnut for axial blade attachment
04/25/2013CA2792750A1 A support ring for a rotary assembly
04/25/2013CA2759642A1 Airfoil devices, leading edge components, and methods of making
04/24/2013EP2584191A1 Improved centre rest for rotary seat of wind-turbine blades
04/24/2013EP2584150A2 Components with laser cladding and methods of manufacture
04/24/2013EP2584149A2 Turbine blade with erosion shield plate
04/24/2013EP2584148A1 Film-cooled turbine blade for a turbomachine
04/24/2013EP2584147A1 Film-cooled turbine blade for a turbomachine
04/24/2013EP2584146A1 Method for producing a rotor blade for a fluid flow engine and corresponding rotor blade
04/24/2013EP2584145A1 A cooled turbine guide vane or blade for a turbomachine
04/24/2013EP2584144A2 Transition nozzle
04/24/2013EP2584143A2 Gas turbine engine component
04/24/2013EP2584142A2 Gas turbine engine cooling systems having hub-bleed impellers and methods for the production thereof
04/24/2013EP2584067A1 Component with graphene and method for producing components with graphene
04/24/2013EP2584060A1 Method for adhering a coating to a substrate structure
04/24/2013EP2584056A1 Titanium aluminide application process and article with titanium aluminide surface
04/24/2013EP2583784A1 Preparation of a welding point before welding and component
04/24/2013EP2583782A2 A method of brazing a component, a brazed power generation system component, and a braze
04/24/2013EP2583781A1 Combined welding-soldering process for joining two workpieces
04/24/2013EP2582986A1 Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine
04/24/2013EP2582985A1 Compressor and turbomachine with optimized efficiency
04/24/2013EP2582920A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector
04/24/2013EP2582919A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector
04/24/2013EP2582918A1 Gas turbine annular diffusor
04/24/2013EP2582580A1 Airflow-straightening structure for the nacelle of an aircraft engine
04/24/2013EP2582487A1 Method of servicing an airfoil assembly for use in a gas turbine engine
04/24/2013EP2582486A1 Method for repairing rotor blades
04/24/2013CN202900329U Combustion turbine moving blade
04/24/2013CN103069112A Film cooled component wall in a turbine engine
04/24/2013CN103069028A Co-based alloy
04/24/2013CN103061889A Thermal insulating structure
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