| 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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| 02/05/2014 | CN203420740U Low pressure intergrade guide vane of gas turbine used compressor |
| 02/05/2014 | CN103561890A Process for manufacturing single part for turbomachine by diffusion welding |
| 02/05/2014 | CN103557034A Second stage guide vane applicable to turbine of heavy low calorific value fuel machine |
| 02/05/2014 | CN103556098A Trass volcanic ash erosion resistance multi-layer thermal barrier coating |
| 02/05/2014 | CN103551444A Method for manufacturing hollow structure |
| 02/05/2014 | CN101946062B Turbomachine rotor comprising pretensioning device for pretensioning guide vane |
| 02/04/2014 | US8641382 Turbocharger |
| 02/04/2014 | US8641381 System and method for reducing grain boundaries in shrouded airfoils |
| 02/04/2014 | US8641380 Compressor wheel |
| 02/04/2014 | US8641377 Industrial turbine blade with platform cooling |
| 02/04/2014 | US8641368 Industrial turbine blade with platform cooling |
| 02/04/2014 | US8641365 Rotor of a gas turbine |
| 02/04/2014 | US8641364 Blade for an impeller wheel |
| 01/30/2014 | WO2014018192A1 Turbine component and a process of fabricating a turbine component |
| 01/30/2014 | WO2014018138A2 Airfoil cooling circuits |
| 01/30/2014 | WO2014016515A1 Part to modify the profile of an aerodynamic jet |
| 01/30/2014 | WO2014016431A1 Blade ring for a turbomachine |
| 01/30/2014 | WO2014016149A1 Method for producing a guide vane and guide vane |
| 01/30/2014 | WO2014016084A1 Rotor of an exhaust gas turbocharger |
| 01/30/2014 | WO2014016016A1 Device and method for joining a shaft-hub connection of a rotor |
| 01/30/2014 | WO2014015959A1 Impeller for a fluid energy machine |
| 01/30/2014 | US20140030109 low-Modulus Gas-Turbine Compressor Blade |
| 01/30/2014 | US20140030107 Decoupled compressor blade of a gas turbine |
| 01/30/2014 | US20140030106 Compressor blade of a gas turbine as well as method for manufacturing said blade |
| 01/30/2014 | US20140030105 Composite turbine engine blade with structural reinforcement |
| 01/30/2014 | US20140030098 Article of manufacture |
| 01/30/2014 | US20140030093 Wind turbine blade comprising resistive heating means |
| 01/30/2014 | US20140030077 Stationary gas turbine arrangement and method for performing maintenance work |
| 01/30/2014 | US20140030076 Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same |
| 01/30/2014 | US20140030065 Steam Turbine, and Steam Turbine Stationary Blade |
| 01/30/2014 | DE10305912B4 Hybrid- Schaufel für thermische Turbomaschinen Hybrid bucket of thermal turbomachinery |
| 01/30/2014 | DE102012213017A1 Verfahren zur Herstellung einer Turbinenschaufel Process for producing a turbine blade |
| 01/30/2014 | DE102012212990A1 Welle-Nabeverbindung eines Läufers Shaft connection of a runner |
| 01/30/2014 | DE102012106810A1 Laufrad für eine Fluidenergiemaschine Impeller for a fluid energy machine |
| 01/30/2014 | DE102012013949A1 Repairing damaged portion of blade of gas turbine engine of aircraft, by digitizing blade damaged portion, comparing digitized data with predetermined data, inserting replacement parts and connecting replacement part with damaged portion |
| 01/29/2014 | EP2690259A1 Turbine rotor and method for producing turbine rotor |
| 01/29/2014 | EP2690254A1 Turbine rotor blade root attachments |
| 01/29/2014 | EP2690197A1 Turbine blade for industrial gas turbine and industrial gas turbine |
| 01/29/2014 | EP2689138A2 High camber compressor rotor blade |
| 01/29/2014 | EP2689108A1 Compressor airfoil with tip dihedral |
| 01/29/2014 | EP2689107A1 High camber stator vane |
| 01/29/2014 | EP2689106A1 Device and method for driving out blades retained in a form-fit manner in a rotor disk |
| 01/29/2014 | EP2688858A1 Bond layers for ceramic or ceramic matrix composite substrates |
| 01/29/2014 | EP2236748B1 A rotor arrangement for a gas turbine |
| 01/29/2014 | EP1825149B1 Multi-stage compressor and housing therefor |
| 01/29/2014 | CN103547402A Friction bonding method and bonding structure |
| 01/29/2014 | CN103541774A Method for designing turbine blades |
| 01/29/2014 | CN103541773A Filiform turbine |
| 01/29/2014 | CN101832181B Novel film cooling hole with anti-whorl hole branch structure |
| 01/29/2014 | CN101550844B Inner turbine shell support configuration and methods |
| 01/29/2014 | CN101482030B Turbine blade tip shroud |
| 01/28/2014 | US8637161 Coated article and method for manufacturing the coated article |
| 01/28/2014 | US8636890 Method for refurbishing PtAl coating to turbine hardware removed from service |
| 01/28/2014 | US8636475 Turbomachine, especially steam turbine |
| 01/28/2014 | US8636474 Rotor assembly for a gas turbine |
| 01/28/2014 | US8636471 Apparatus and methods for cooling platform regions of turbine rotor blades |
| 01/28/2014 | US8636470 Turbine blades and turbine rotor assemblies |
| 01/28/2014 | US8636463 Interior cooling channels |
| 01/28/2014 | CA2569563C Turbine blade with improved cooling characteristics and useful life |
| 01/26/2014 | CA2821057A1 Axial retention for fasteners in fan joint |
| 01/23/2014 | WO2014014750A1 Joint between airfoil and shroud |
| 01/23/2014 | WO2014014616A1 Damper system and corresponding turbine |
| 01/23/2014 | WO2014014550A1 Pmc laminate embedded hypotube lattice |
| 01/23/2014 | WO2014014539A2 Blade dovetail bottom |
| 01/23/2014 | WO2014013157A1 Method and system for cutting a preform intended for the production of a turbomachine part |
| 01/23/2014 | WO2014013020A1 A rotor for a radial compressor and a method for construction thereof |
| 01/23/2014 | WO2013180797A3 Shark-bite tip shelf cooling configuration |
| 01/23/2014 | WO2013180795A3 Turbine airfoil trailing edge cooling slots |
| 01/23/2014 | WO2013165515A3 Gas turbine engine with fan-tied inducer section |
| 01/23/2014 | WO2013165495A3 Apparatus and method for optically measuring creep |
| 01/23/2014 | WO2013088040A3 Fiber structure woven into a single part by means of 3d weaving, and use in the manufacture of a composite material part |
| 01/23/2014 | US20140023517 Nozzle for turbine system |
| 01/23/2014 | US20140023515 Fibre-reinforced composite moulding and manufacture thereof |
| 01/23/2014 | US20140023512 Thermoplastic rotor blade |
| 01/23/2014 | US20140023510 Diagonal impeller for a diagonal fan, and diagonal fan |
| 01/23/2014 | US20140023509 Bayoneted anti-rotation turbine seals |
| 01/23/2014 | US20140023508 Rotor assembly |
| 01/23/2014 | US20140023506 Damper system and a turbine |
| 01/23/2014 | US20140023504 First stage compressor disk configured for balancing the compressor rotor assembly |
| 01/23/2014 | US20140023502 Variable vane assembly for turbine system |
| 01/23/2014 | US20140023501 Turbofan, and air-conditioning apparatus |
| 01/23/2014 | US20140023498 Rotating stall detection using optical measurement of blade untwist |
| 01/23/2014 | US20140023497 Cooled turbine blade tip shroud with film/purge holes |
| 01/23/2014 | US20140023483 Airfoil assembly including vortex reducing at an airfoil leading edge |
| 01/23/2014 | DE102011102359B4 Fluggasturbine mit justierbarem Fan Aircraft gas turbine with adjustable fan |
| 01/22/2014 | EP2687729A1 Rotor structure |
| 01/22/2014 | EP2687683A2 Sealing device, axial turbine and power plant |
| 01/22/2014 | EP2687682A2 Gas turbine |
| 01/22/2014 | EP2687680A2 Axial turbine and power plant |
| 01/22/2014 | EP2687679A1 Trailing edge attachment for composite airfoil |
| 01/22/2014 | EP2687678A1 A rotor for a radial compressor and a method for construction thereof |
| 01/22/2014 | EP2686521A1 Method for retrofitting a double flow steam turbine |
| 01/22/2014 | CN203403911U Ultra-fine grain titanium alloy TC4 blade |
| 01/22/2014 | CN203403910U 涡轮增压器涡轮 Turbocharger turbine |
| 01/22/2014 | CN203403909U Turbine body of gas turbine |
| 01/22/2014 | CN103534443A Turbine engine impeller |
| 01/22/2014 | CN103534442A Random propylene copolymer with high stiffness and low haze |
| 01/22/2014 | CN103527262A Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same |
| 01/22/2014 | CN103527261A Cooled blade for a gas turbine |
| 01/22/2014 | CN103527260A Airfoil |