| 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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| 12/26/2013 | US20130343899 Turbine Rotor, Manufacturing Method Thereof and Steam Turbine Using Turbine Rotor |
| 12/26/2013 | US20130343898 Propeller blade with carbon foam spar core |
| 12/26/2013 | US20130343897 Helix Type Vertical Axis Turbine Blades and Method for Continuously Making Same |
| 12/26/2013 | US20130343895 System having blade segment with curved mounting geometry |
| 12/26/2013 | US20130343894 Turbine wheel in a turbine engine |
| 12/26/2013 | US20130343893 Turbine rotor and production method thereof |
| 12/26/2013 | US20130343892 Propfan engine |
| 12/26/2013 | US20130343891 Spiral screw fluid turbine having axial void |
| 12/26/2013 | US20130343884 Impeller of Cooling Fan |
| 12/26/2013 | US20130343872 Cooled component for the turbine of a gas turbine engine |
| 12/25/2013 | EP2677121A2 A catcher ring arrangement |
| 12/25/2013 | EP2677120A1 Gas turbine conical flange bolted joint |
| 12/25/2013 | EP2677119A2 Rotor balancing method |
| 12/25/2013 | EP2677063A1 Erosion and corrosion resistant coatings for exhaust gas recirculation-based gas turbines |
| 12/25/2013 | EP2676759A2 Turbine rotor, manufacturing method thereof and steam turbine using turbine rotor |
| 12/25/2013 | EP2676023A1 Process for cooling the turbine stage and gas turbine having a cooled turbine stage |
| 12/25/2013 | EP2676001A1 Rotary machine |
| 12/25/2013 | EP2676000A1 Integrated axial and tangential serpentine cooling circuit in a turbine airfoil |
| 12/25/2013 | EP2531700B1 Turbine engine air blower |
| 12/25/2013 | EP2479382B1 Rotor blade |
| 12/25/2013 | EP2440367B1 Method for reducing the diameter of an opening |
| 12/25/2013 | EP2281653B1 A method of friction welding a first workpiece to a second workpiece with converging parts |
| 12/25/2013 | CN203362237U 增压器组件 Turbocharger Components |
| 12/25/2013 | CN203362236U Turbine rotor weight reduction structure |
| 12/25/2013 | CN203362235U Weight reducing structure of booster turbine rotor |
| 12/25/2013 | CN203362234U Turbine rotor |
| 12/25/2013 | CN103477031A Low pressure cooling seal system for a gas turbine engine |
| 12/25/2013 | CN103476544A Method for manufacturing a metal part |
| 12/25/2013 | CN103470316A Hybrid mini layer type turbine capable of combining impulse action with boundary layer effect |
| 12/25/2013 | CN103470314A Method and system for determining creep capability of turbine components prior to operation |
| 12/25/2013 | CN103470313A Turbine blade and turbine with same, and engine |
| 12/25/2013 | CN103470312A Gas turbine engine blade with inner meshed structure |
| 12/25/2013 | CN103470311A Turbomachine bucket assembly and method of cooling a turbomachine bucket assembly |
| 12/25/2013 | CN103470310A Low-pressure intermediate-stage guide blade of gas compressor for gas turbine |
| 12/25/2013 | CN103470309A Segmented combined type rotor |
| 12/25/2013 | CN103470308A Turbine rotor and blade assembly with multi-piece locking blade |
| 12/25/2013 | CN103470307A Turbine rotor and blade assembly with blind holes |
| 12/25/2013 | CN103469144A High-porosity thermal barrier coating with isometric crystal structure |
| 12/25/2013 | CN103469009A Method for preparing titanium alloy blade by investment casting method |
| 12/24/2013 | US8613599 Turbine blade assembly and seal strip |
| 12/24/2013 | US8613598 Wet compression apparatus and method |
| 12/24/2013 | US8613597 Turbine blade with trailing edge cooling |
| 12/24/2013 | US8613596 Vane assembly having a vane end seal |
| 12/24/2013 | CA2569566C Central cooling circuit for mobile turbine engine blade |
| 12/22/2013 | CA2818666A1 A catcher ring arrangement |
| 12/19/2013 | WO2013188869A1 Turbine airfoil with cast platform cooling circuit |
| 12/19/2013 | WO2013188778A1 Compressor blade |
| 12/19/2013 | WO2013188731A1 Rotor assembly, corresponding gas turbine engine and method of assembling |
| 12/19/2013 | WO2013188115A1 Rotor assembly with interlocking tabs |
| 12/19/2013 | WO2013187103A1 Blade root spring insertion tool and blade root spring insertion method |
| 12/19/2013 | WO2013186756A1 Aerofoil array for a gas turbine with anti fluttering means |
| 12/19/2013 | WO2013165518A3 Gas turbine engine component with cusped, lobed cooling hole |
| 12/19/2013 | WO2013165517A3 Gas turbine engine component with diffusive cooling hole |
| 12/19/2013 | US20130336811 Rotor apparatus |
| 12/19/2013 | US20130336801 Rotating airfoil component with platform having a recessed surface region therein |
| 12/19/2013 | US20130336799 Compressor blade |
| 12/19/2013 | US20130336796 Modified taper roller edge |
| 12/19/2013 | US20130336790 High Volume Low Speed Fan |
| 12/19/2013 | US20130336770 Turbine |
| 12/19/2013 | US20130336767 Cooling for a turbine airfoil trailing edge |
| 12/19/2013 | US20130333392 Turbine compressor blade tip resistant to metal transfer |
| 12/19/2013 | US20130333173 Blade root spring insertion jig and insertion method of blade root spring |
| 12/19/2013 | CA2876147A1 Aerofoil array for a gas turbine with anti fluttering means |
| 12/19/2013 | CA2875816A1 Turbine airfoil apparatus and corresponding method |
| 12/19/2013 | CA2875810A1 Rotor assembly, corresponding gas turbine engine and method of assembling |
| 12/18/2013 | EP2674577A2 Blade attachment assembly for a turbomachine and corresponding turbomachine |
| 12/18/2013 | EP2674576A1 Reinforced Coatings and Methods of Making the Same |
| 12/18/2013 | EP2674575A1 A diffuser apparatus in a turbomachine |
| 12/18/2013 | EP2674574A1 A diffuser apparatus in a turbomachine |
| 12/18/2013 | EP2674573A2 Rotating blade with platform having a recessed surface region therein |
| 12/18/2013 | EP2674572A2 Turbine exhaust diffuser |
| 12/18/2013 | EP2674510A1 Channel marker and related methods |
| 12/18/2013 | EP2673475A1 Joining mechanism and method for interlocking modular turbine engine component with a split ring |
| 12/18/2013 | EP2673473A1 Blade-platform assembly for supersonic flow |
| 12/18/2013 | EP2673472A1 Blade-platform assembly for subsonic flow |
| 12/18/2013 | EP2548686B1 Solder film for high temperature soldering and method of repairing or producing components using this solder film |
| 12/18/2013 | EP2408584B1 Method for producing an integrally bladed rotor, rotor and apparatus for carrying out the method |
| 12/18/2013 | EP1891300B1 Trailing edge attachment for composite airfoil |
| 12/18/2013 | EP1797283B1 Variable nozzle turbocharger having cambered vanes |
| 12/18/2013 | CN203347846U Turbine blade front edge structure |
| 12/18/2013 | CN203347845U Bending moment-resistant anti-corrosion wedge block-connected movable blade structure of turbine |
| 12/18/2013 | CN1987053B Apparatus and method for cooling turbine engine blade trailing edges |
| 12/18/2013 | CN103459804A Process for cooling the turbine stage and gas turbine having a cooled turbine stage |
| 12/18/2013 | CN103459779A Turbine rotor and method for producing turbine rotor |
| 12/18/2013 | CN103459777A Sealing ring for a turbine stage of an aircraft turbomachine, comprising slotted anti-rotation pegs |
| 12/18/2013 | CN103459776A Vane member and rotary machine |
| 12/18/2013 | CN103459775A Gas turbine |
| 12/18/2013 | CN103459774A Compressor airfoil with tip dihedral |
| 12/18/2013 | CN103459773A Rotor of rotating machine, and rotating machine |
| 12/18/2013 | CN103452904A S-shaped profile blade of axial turbomachine compressor, corresponding compressor and turbomachine |
| 12/18/2013 | CN103452604A Control system for axial flow turbine |
| 12/18/2013 | CN103452602A Power generation device of turbine expander |
| 12/18/2013 | CN103452599A Nozzle diaphragm inducer |
| 12/18/2013 | CN103452598A Apparatus for minimizing solid particle erosion in steam turbines |
| 12/18/2013 | CN103452597A Method of coating corner interface of turbine system |
| 12/18/2013 | CN103452596A Shroud for airfoils |
| 12/18/2013 | CN103452595A Novel air film hole with improved cooling efficiency |
| 12/18/2013 | CN103452594A Cooling assembly for a bucket of a turbine system and method of cooling |
| 12/17/2013 | US8608446 Rotor disk and blade arrangement |
| 12/17/2013 | US8608443 Film cooled component wall in a turbine engine |