| 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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| 06/18/2013 | US8465255 Gas turbine blade and gas turbine having the same |
| 06/18/2013 | CA2768660C Rotor assembly with cooling air deflectors and method |
| 06/18/2013 | CA2642505C Cooling structure |
| 06/18/2013 | CA2537435C Device for adjusting the centring of a synchronization ring for the control of turning vanes in a turbine engine |
| 06/13/2013 | WO2013085878A1 Turbine blade incorporating trailing edge cooling design |
| 06/13/2013 | WO2013084777A1 Back-shielded welding method and welded structure using same |
| 06/13/2013 | WO2013084260A1 Turbine rotor blade |
| 06/13/2013 | WO2013083937A1 Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element |
| 06/13/2013 | WO2013083918A1 Method for reshaping a turbomachine blade that has at least one zone that has become deformed using peening |
| 06/13/2013 | WO2013083304A1 Component having a film cooling hole |
| 06/13/2013 | US20130149169 Component having cooling channel with hourglass cross section |
| 06/13/2013 | US20130149165 Rotating blade having a rib arrangement with a coating |
| 06/13/2013 | US20130149164 Method and Apparatus for Fabricating Large Scale Integrated Airfoils |
| 06/13/2013 | US20130149163 Method for Reducing Stress on Blade Tips |
| 06/13/2013 | US20130149159 Gas turbine engine part retention |
| 06/13/2013 | US20130149158 Rotor with relief features and one-sided load slots |
| 06/13/2013 | US20130149157 Boundary layer controlled logarithmic spiral blade |
| 06/13/2013 | US20130149125 Turbine and method for manufacturing turbine |
| 06/13/2013 | US20130149108 Blade |
| 06/13/2013 | DE102011120682A1 Verfahren zur Auswahl einer Schaufelgeometrie Method for selecting a blade geometry |
| 06/13/2013 | DE102011088206A1 Rotary machine for use as flow machine, particularly turbo-machine such as turbine, has stator and rotor which is mounted at stator over rotational bearing unit in rotating manner |
| 06/13/2013 | CA2855172A1 Method for reshaping a turbomachine blade that has at least one zone that has become deformed using peening |
| 06/12/2013 | EP2602439A1 Coolable hot gas component for a gas turbine |
| 06/12/2013 | EP2602435A2 Turbomachine rotor and corresponding assembly method |
| 06/12/2013 | EP2602434A2 Dynamic load reduction system |
| 06/12/2013 | EP2602433A1 Method to produce a coated gas turbine component having opening holes, apparatus to perform the method and coated turbine blade having cooling holes |
| 06/12/2013 | EP2602432A1 Apparatus and method for the forming of turbine vane cover plates |
| 06/12/2013 | EP2602431A1 Device and method for the forming of a cover plate of a vane |
| 06/12/2013 | EP2602352A1 Component with film cooling holes |
| 06/12/2013 | EP2602050A1 Method for selecting a blade geometry |
| 06/12/2013 | EP2601407A1 Screw turbine and method of power generation |
| 06/12/2013 | EP2601385A1 Turbomachine rotor with blade roots with adjusting protrusions |
| 06/12/2013 | EP2601384A1 Gas turbine engine comprising a tension stud |
| 06/12/2013 | EP2601383A1 Gas turbine rotor comprising an axially displaceable turbine rotor shaft |
| 06/12/2013 | EP2601010A1 Production of blades of a turbomachine from cold-formed base material |
| 06/12/2013 | EP2601009A1 Process for manufacturing a turbomachine drum |
| 06/12/2013 | CN103154489A Aircraft propulsion assembly |
| 06/12/2013 | CN103154437A Gas turbine annular diffusor |
| 06/12/2013 | CN103154436A Rotor blade having a cover plate for a steam turbine |
| 06/12/2013 | CN103154435A 推力反向器 Thrust reverser |
| 06/12/2013 | CN103153505A Method for producing a solid part |
| 06/11/2013 | US8459956 Curved platform turbine blade |
| 06/11/2013 | US8459955 Aerofoil |
| 06/11/2013 | US8459954 Torsional flexing energy absorbing blade lock |
| 06/11/2013 | US8459953 Seal plate and bucket retention pin assembly |
| 06/11/2013 | US8459952 Device and method for connecting a blade to a rotor shaft of a continuous flow machine |
| 06/11/2013 | US8459951 Rotor for an axial flow turbomachine |
| 06/11/2013 | US8459947 Winglet for a blade of a wind turbine |
| 06/11/2013 | US8459943 Gas turbine engine rotor sections held together by tie shaft, and with blade rim undercut |
| 06/11/2013 | US8459935 Turbine vane with endwall cooling |
| 06/11/2013 | US8459934 Varying cross-sectional area guide blade |
| 06/11/2013 | US8459933 Turbine vane with endwall cooling |
| 06/11/2013 | CA2734605C Erosion- and impact-resistant coatings |
| 06/11/2013 | CA2627788C Method for determining blade mistuning on integrally manufactured rotor wheels |
| 06/06/2013 | WO2013081714A2 Guide vane assembly for a gas turbine engine |
| 06/06/2013 | WO2013081142A1 Turbine blade |
| 06/06/2013 | WO2013080828A1 Bonded component |
| 06/06/2013 | WO2013079860A1 Method for producing a turbomachine vane made from composite material and including integrated platforms |
| 06/06/2013 | WO2013079859A1 Hollow-blade turbine vane made from composite material, turbine or compressor including a nozzle or guide vane assembly formed by such blades, and turbomachine comprising same |
| 06/06/2013 | WO2013079851A1 Turbine engine vane, in particular for a one-piece bladed disk |
| 06/06/2013 | WO2013079246A1 Laser drilling through-bores without protection in the interior |
| 06/06/2013 | WO2013079193A1 Method for repairing a variable guide vane and correspondingly repaired guide vane |
| 06/06/2013 | WO2013001185A3 Tertiary locking assembly for a thrust reverser |
| 06/06/2013 | US20130142668 Cooled turbine blade for gas turbine engine |
| 06/06/2013 | US20130142666 Turbine blade incorporating trailing edge cooling design |
| 06/06/2013 | US20130142665 Hybrid vapor and film cooled turbine blade |
| 06/06/2013 | US20130142662 Exhaust-gas turbocharger component |
| 06/06/2013 | US20130142661 Nickel-based alloy |
| 06/06/2013 | US20130142660 Ceramic matrix composite airfoil structure with trailing edge support for a gas turbine engine |
| 06/06/2013 | US20130142659 Detuned vane airfoil assembly |
| 06/06/2013 | US20130142658 Rotor blade |
| 06/06/2013 | US20130142655 Multilayer-type fan device |
| 06/06/2013 | US20130142651 Turbine impeller comprising blade with squealer tip |
| 06/06/2013 | US20130142649 Cooled turbine blade and method for cooling a turbine blade |
| 06/06/2013 | US20130142637 Low rhenium single crystal superalloy for turbine blades and vane applications |
| 06/06/2013 | US20130142635 Rotary energy generating system and corresponding device |
| 06/06/2013 | US20130142626 Tank sloshing energy recovery system |
| 06/06/2013 | DE102012002283B3 Verfahren zum Herstellen eines Turbinenrotors A method of manufacturing a turbine rotor |
| 06/06/2013 | DE102011119910A1 Paddle wheel useful e.g. for a compressor, comprises disc body, which is peripherally connected with rotor blade that is connected to disk body, and the rotor blade has blade base and a connection is formed between blade base and disk body |
| 06/06/2013 | DE102011119881A1 Aufladeeinrichtung für eine Brennstoffzelle, insbesondere eines Kraftwagens Charging means for a fuel cell, in particular a motor vehicle |
| 06/06/2013 | DE102011087665A1 Verfahren zur Reparatur einer variablen Leitschaufel und entsprechend reparierte Leitschaufel Method of repairing a variable vane and vane according repaired |
| 06/06/2013 | CA2857453A1 A method of fabricating a composite material turbine engine vane with incorporated platforms |
| 06/06/2013 | CA2857452A1 Hollow-blade turbine vane made from composite material, turbine or compressor including a nozzle or guide vane assembly formed by such blades, and turbomachine comprising same |
| 06/06/2013 | CA2855956A1 Turbine engine vane, in particular for a one-piece bladed disk |
| 06/06/2013 | CA2847566A1 Guide vane assembly for a gas turbine engine |
| 06/05/2013 | EP2600142A1 Component aperture location using computer tomography |
| 06/05/2013 | EP2599966A2 Blade skirt |
| 06/05/2013 | EP2599961A2 Segmented thermally insulating coating |
| 06/05/2013 | EP2599960A1 Turbomachine component machining method |
| 06/05/2013 | EP2599959A2 Ceramic matrix composite airfoil structure with trailing edge support for a gas turbine engine |
| 06/05/2013 | EP2599958A2 Cooled turbine blade and corresponding method for cooling a turbine blade |
| 06/05/2013 | EP2599957A1 Cooling fin system for a cooling channel and turbine blade |
| 06/05/2013 | EP2599890A1 Non-flaking ceramic coat and coating system |
| 06/05/2013 | EP2599714A1 Propeller blade having compliant adhesive at spar interface |
| 06/05/2013 | EP2599575A1 Laser drilling of through boreholes without internal protection |
| 06/05/2013 | EP2598835A1 Method for treating turbine blades and device therefor |
| 06/05/2013 | EP2598721A1 Inter-vane seal for a wheel of a turbine or a turbomachine compressor |
| 06/05/2013 | EP2598720A2 Axial locking seals for aft removable turbine blade |
| 06/05/2013 | CN202970802U Hollow outer rotor pneumatic motor |
| 06/05/2013 | CN103133056A High-hardness high-corrosion-resistance intensified steel turbine blade |