| 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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| 06/05/2013 | CN103133055A High-hardness high-temperature-resistant intensified steel turbine blade |
| 06/05/2013 | CN103133054A High-hardness high-temperature-resistant stable turbine blade |
| 06/05/2013 | CN103133053A Fast-forming corrosion resistant reinforced steel turbine blade |
| 06/05/2013 | CN103133052A Heat-resistant and anti-oxidation reinforced steel turbine blade |
| 06/05/2013 | CN103133051A High-strength high-thermal-conductivity intensified steel turbine blade |
| 06/05/2013 | CN103133050A Anti-oxidation strengthened steel turbine blade |
| 06/05/2013 | CN103133049A High-heat-resistance intensified steel turbine blade |
| 06/05/2013 | CN103133048A High-heat-resistance stable intensified steel turbine blade |
| 06/05/2013 | CN103133047A High-hardness wear-resistant intensified steel turbine blade |
| 06/05/2013 | CN103133046A High-hardness wear-resistant stable turbine blade |
| 06/05/2013 | CN103133045A Turbine blade made of corrosion-resistant and high-temperature-resistant intensified steel |
| 06/05/2013 | CN103133044A High-hardness strengthened steel steam turbine vane |
| 06/05/2013 | CN103133043A Blade skirt |
| 06/05/2013 | CN103133042A High-hardness high-thermal-conductivity stable turbine blade |
| 06/05/2013 | CN103133041A Corrosion resistant high-temperature resistant stable type turbine blade |
| 06/05/2013 | CN103133040A Cooled turbine blade and corresponding method for cooling a turbine blade |
| 06/05/2013 | CN102485934B Method for preparing hollow blade inner chamber diffusion layer with high temperature resistance, oxidation resistance and corrosion resistance |
| 06/05/2013 | CN102321887B 38CrMoAl compressor blade subjected to composite surface modification and preparation process thereof |
| 06/04/2013 | US8455103 Composite material component with silicon-containing ceramic matrix, protected against corrosion |
| 06/04/2013 | US8454318 Reinforced aerodynamic profile |
| 06/04/2013 | US8454317 Radial or diagonal fan wheel |
| 06/04/2013 | US8454310 Compressor blade with tip sealing |
| 06/04/2013 | US8454306 Steam turbine |
| 05/30/2013 | WO2013078159A1 Rotary energy generating system and corresponding device |
| 05/30/2013 | WO2013077761A1 Airfoil with cooling passages |
| 05/30/2013 | WO2013076417A1 Mechanical system for a turbine engine, turbine engine, and method for attaching a mechanical system within a turbine engine |
| 05/30/2013 | WO2013076110A1 Cooling rib system for a cooling passage of a turbine blade |
| 05/30/2013 | WO2013076109A1 Coolable hot-gas component for a gas turbine |
| 05/30/2013 | WO2013075858A1 Modified interface around a hole |
| 05/30/2013 | WO2013075835A1 Method for deposition welding |
| 05/30/2013 | WO2013075815A1 Method for repairing a gas turbine component |
| 05/30/2013 | WO2013075688A1 Method for hardfacing the z-notch of tial blades |
| 05/30/2013 | US20130136621 Blading |
| 05/30/2013 | US20130136620 Water Impeller |
| 05/30/2013 | US20130136619 Blading |
| 05/30/2013 | US20130136618 Blade Skirt |
| 05/30/2013 | US20130136616 Propeller blade having a honeycomb spar core |
| 05/30/2013 | US20130136615 Propeller blade with lightweight insert |
| 05/30/2013 | US20130136614 Propeller blade having compliant adhesive at spar interface |
| 05/30/2013 | US20130136613 Propeller/impeller blade apparatus |
| 05/30/2013 | US20130136612 Fluid driven turbine blade, and turbine using same |
| 05/30/2013 | US20130136611 Turbine bucket airfoil profile |
| 05/30/2013 | US20130136610 Turbine bucket airfoil profile |
| 05/30/2013 | US20130136609 Turbine nozzle airfoil profile |
| 05/30/2013 | US20130136608 Turbine bucket airfoil profile |
| 05/30/2013 | US20130136607 Turbine nozzle airfoil profile |
| 05/30/2013 | US20130136606 Turbine bucket airfoil profile |
| 05/30/2013 | US20130136605 Device for locking a root of a rotor blade |
| 05/29/2013 | EP2597266A1 Rotor blade and flow machine |
| 05/29/2013 | EP2597265A1 Rotor blade for an axial throughflow turbo engine |
| 05/29/2013 | EP2597264A2 Aerofoil cooling arrangement |
| 05/29/2013 | EP2597263A1 Bucket assembly for turbine system |
| 05/29/2013 | EP2597262A1 Bucket assembly for turbine system |
| 05/29/2013 | EP2597261A1 Bucket Assembly for Turbine System |
| 05/29/2013 | EP2597260A1 Bucket assembly for turbine system |
| 05/29/2013 | EP2597259A1 Modified surface around a hole |
| 05/29/2013 | EP2597258A2 System and method of monitoring turbine engines |
| 05/29/2013 | EP2597257A1 Blades |
| 05/29/2013 | EP2597256A1 Radial turbine |
| 05/29/2013 | EP2597170A1 Process for repairing a cylinder running surface by means of plasma spraying processes |
| 05/29/2013 | EP2596902A1 Method for decarburization of a rotor forging |
| 05/29/2013 | EP2596214A1 Method for repairing gas turbine components of ceramic composite materials and device for carrying out the method |
| 05/29/2013 | DE102010018284B4 Turbinenschaufelrohling sowie Verfahren und Vorrichtung zum Bearbeiten eines Turbinenschaufelrohlings Turbine blade blank and method and apparatus for processing a turbine blade blank |
| 05/29/2013 | CN1944959B Dust resistant platform blade |
| 05/29/2013 | CN103122774A Turbine high-pressure cylinder first-five-level vane |
| 05/29/2013 | CN101678515B Method of manufacture using same datum features on different workpieces |
| 05/29/2013 | CN101315033B Shroud configuration having sloped seal |
| 05/29/2013 | CN101125753B Dysprosium oxide stabilized zirconia abradable |
| 05/29/2013 | CA2795653A1 Blade skirt |
| 05/28/2013 | US8452516 Variable vane scheduling based on flight conditions for inclement weather |
| 05/28/2013 | US8449994 Turbine engine components |
| 05/28/2013 | US8449784 Method for securing a sheath to a blade |
| 05/28/2013 | US8449262 Nickel-based superalloys, turbine blades, and methods of improving or repairing turbine engine components |
| 05/28/2013 | US8449260 Composite load-bearing rotating ring and process therefor |
| 05/28/2013 | US8449257 Wind generator with folding mast |
| 05/28/2013 | US8449254 Branched airfoil core cooling arrangement |
| 05/28/2013 | US8449246 BOAS with micro serpentine cooling |
| 05/28/2013 | US8449243 Device and method for axially displacing a turbine rotor |
| 05/28/2013 | CA2513045C Internally cooled gas turbine airfoil and method |
| 05/23/2013 | WO2013074393A1 Flow rotor, in particular turbine wheel |
| 05/23/2013 | WO2013072610A1 Gas turbine vane offset towards the lower surface of the head sections and with cooling channels |
| 05/23/2013 | WO2013072605A1 Impeller for a turbomachine |
| 05/23/2013 | WO2013071909A1 Armoring sealing fins of tial vanes by induction brazing hard-material particles |
| 05/23/2013 | US20130130052 Method for manufacturing a thermal-barrier protection and multilayer coating suitable for forming a thermal barrier |
| 05/23/2013 | US20130129978 Articles and Methods Providing Supermetalophobic/philic Surfaces and Superceramophobic/philic Surfaces |
| 05/23/2013 | US20130129524 Centrifugal impeller |
| 05/23/2013 | US20130129523 Bimetallic Compressor Wheel and a Method of Manufacture Thereof |
| 05/23/2013 | US20130129522 Rhenium-free single crystal superalloy for turbine blades and vane applications |
| 05/23/2013 | US20130129521 Turbine blade skirt |
| 05/23/2013 | US20130129516 Aerofoils |
| 05/23/2013 | US20130129515 Cross flow fan and air conditioner |
| 05/23/2013 | US20130129514 Propeller arrangement, in particular for watercraft |
| 05/23/2013 | US20130129513 Centrifugal fan impeller structure |
| 05/23/2013 | US20130129507 Composite Propeller Spar |
| 05/23/2013 | US20130129493 Turbine |
| 05/23/2013 | US20130129478 Gas turbine rotor comprising an axially displaceable turbine rotor shaft |
| 05/23/2013 | US20130129473 Avoidance of torsional excitations in converter-controlled compressor runs |
| 05/23/2013 | DE102012111154A1 Bimetallisches Verdichterrad und Verfahren zu dessen Herstellung Bimetallic compressor wheel and process for its preparation |
| 05/23/2013 | DE102011086770A1 Friction welding of component of continuous-flow machine, comprises moving components to be welded relative to each other or to tool to generate heat, and maintaining heated components with component regions to be welded against each other |
| 05/23/2013 | DE102011086574A1 Turbocharger shaft for use with impeller, comprises cylindrical guide section, knurled section conically extending to cylindrical guide section, and cylindrical knurled section, which are arranged one behind other in axial direction |