| 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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| 01/16/2013 | EP2546462A2 Hole for rotating component cooling system |
| 01/16/2013 | EP2546461A1 Rotor assembly and corresponding gas turbine engine |
| 01/16/2013 | EP2546460A2 Turbine engine and load reduction device thereof |
| 01/16/2013 | EP2546459A1 A rotor train for a turbine system |
| 01/16/2013 | EP2546458A2 Rotatable power-plant case section |
| 01/16/2013 | EP2546384A1 Steam turbine member |
| 01/16/2013 | EP2546007A1 Microcircuit skin core cut back to reduce microcircuit trailing edge stresses of an airfoil |
| 01/16/2013 | EP2545253A1 Mounting device and method for mounting a component on a component carrier using an adhesive |
| 01/16/2013 | EP2545252A1 Balance correction weight providing constant mass |
| 01/16/2013 | EP2545210A1 Method for electrochemically stripping coatings from gas turbine components |
| 01/16/2013 | EP2545198A1 Method for manufacturing a thermal-barrier protection and multi-layer coating suitable for forming a thermal barrier |
| 01/16/2013 | EP2544840A1 Method and device for producing a component |
| 01/16/2013 | CN202673375U Compact-type high-load power turbine generator |
| 01/16/2013 | CN202673372U Blade backside groove structure of open centripetal turbine |
| 01/16/2013 | CN202673371U Straight shrouded impeller |
| 01/16/2013 | CN102877892A Turbine rotor blade and gas turbine with same |
| 01/16/2013 | CN102877891A Rotor assembly for gas turbines |
| 01/16/2013 | CN102392217B Blade surface pitting corrosion resistant coating and preparation method thereof |
| 01/16/2013 | CN101724768B Heat barrier coating bonding layer material |
| 01/16/2013 | CN101631932B Rotor of a gas turbine |
| 01/16/2013 | CN101326138B Metal part and brazed joint of metal part produced from ceramic material |
| 01/15/2013 | US8353670 Axial balancing clip weight for rotor assembly and method for balancing a rotor assembly |
| 01/15/2013 | US8353669 Turbine vane platform leading edge cooling holes |
| 01/15/2013 | US8353668 Airfoil insert having a tab extending away from the body defining a portion of outlet periphery |
| 01/15/2013 | CA2649035C Blade under platform pocket cooling |
| 01/10/2013 | WO2013004656A1 Liquid metal cooled blade |
| 01/10/2013 | WO2012140049A3 Wind turbine blade comprising cylindrical metal inserts in a root region thereof |
| 01/10/2013 | WO2012140043A3 Wind turbine blade with elongated fastening members in the root region thereof |
| 01/10/2013 | US20130011271 Ceramic matrix composite components |
| 01/10/2013 | US20130011268 Impeller Assembly and Method |
| 01/10/2013 | US20130011267 Hub structure |
| 01/10/2013 | US20130011266 Fan stagger angle for dirt rejection |
| 01/10/2013 | US20130011265 Chevron platform turbine vane |
| 01/10/2013 | US20130011264 Turbine blade |
| 01/10/2013 | US20130011260 Vibration reduction device and vibration reduction method |
| 01/10/2013 | US20130011247 Centrifugal fan with a multistage impeller |
| 01/10/2013 | US20130008170 Subsonic swept fan blade |
| 01/10/2013 | US20130008146 Efficient, low pressure ratio propulsor for gas turbine engines |
| 01/09/2013 | EP2543851A1 Gas turbine engine |
| 01/09/2013 | EP2543825A2 Gas turbine shroud arrangement |
| 01/09/2013 | EP2543823A2 Ceramic matrix composite components |
| 01/09/2013 | EP2543822A1 Turbine blade with serpentine cooling microcircuit |
| 01/09/2013 | EP2543821A1 Rotor blade for gas turbine, method for manufacturing same, and gas turbine using rotor blade |
| 01/09/2013 | EP2543820A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 01/09/2013 | EP2543819A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 01/09/2013 | EP2543818A2 Subsonic swept fan blade |
| 01/09/2013 | EP2543467A1 Method of welding a gamma-prime precipitate strengthened material |
| 01/09/2013 | EP2542762A1 Cooled vane of a turbine and corresponding turbine |
| 01/09/2013 | CN102869855A Gas turbine and thermodynamic power generation system |
| 01/09/2013 | CN102869851A Wear-resistant part for the support of a blade of a turbojet engine fan |
| 01/09/2013 | CN102869812A Removable mask for a turbomachine blade or distributor sector platform |
| 01/09/2013 | CN102865141A 燃气涡轮发动机 A gas turbine engine |
| 01/08/2013 | US8352117 Turbine component tracking system |
| 01/08/2013 | US8348622 Wind turbine blades made of two separate sections, and method of assembly |
| 01/08/2013 | US8348620 Device for axially retaining blades mounted on a turbomachine rotor disk |
| 01/08/2013 | US8348619 Platform and blade for a bladed wheel of a turbomachine, bladed wheel and compressor or turbomachine comprising such a bladed wheel |
| 01/08/2013 | US8348615 Turbine engine rotor disc with cooling passage |
| 01/08/2013 | US8348614 Coolable airfoil trailing edge passage |
| 01/08/2013 | US8348612 Turbine blade tip shroud |
| 01/08/2013 | US8348608 Turbomachine rotor cooling |
| 01/08/2013 | US8348599 Turbine rotor wheel |
| 01/08/2013 | US8347632 Open-cooled component for a gas turbine, combustion chamber, and gas turbine |
| 01/08/2013 | CA2712366C Turbine rotor for a gas turbine |
| 01/08/2013 | CA2563824C Ceramic matrix composite airfoil trailing edge arrangement |
| 01/08/2013 | CA2526717C Multiform film cooling holes |
| 01/03/2013 | WO2013001185A2 Tertiary locking assembly for a thrust reverser |
| 01/03/2013 | WO2013001091A1 Seal system for a gas turbine |
| 01/03/2013 | WO2013000691A1 Impingement cooling of turbine blades or vanes |
| 01/03/2013 | US20130004332 Gas turbine blade and method for producing a blade |
| 01/03/2013 | US20130004331 Turbine blade or vane with separate endwall |
| 01/03/2013 | US20130004328 Abrasive airfoil tip |
| 01/03/2013 | US20130004327 Aluminum fan blade root |
| 01/03/2013 | US20130004326 Cmc blade with integral 3d woven platform |
| 01/03/2013 | US20130004325 Hybrid part made from monolithic ceramic skin and cmc core |
| 01/03/2013 | US20130004324 Nano-structured fan airfoil sheath |
| 01/03/2013 | US20130004323 Fan blade protection system |
| 01/03/2013 | US20130004322 Fan blade with sheath |
| 01/03/2013 | US20130004321 Turbine wheel |
| 01/03/2013 | US20130004319 Rotor assembly and reversible turbine blade retainer therefor |
| 01/03/2013 | US20130004317 Turbine disk preform, welded turbine rotor made therewith and methods of making the same |
| 01/03/2013 | US20130004316 Multi-piece centrifugal impellers and methods for the manufacture thereof |
| 01/03/2013 | US20130004315 Mateface gap configuration for gas turbine engine |
| 01/03/2013 | US20130004314 Radial spline arrangement for lpt vane clusters |
| 01/03/2013 | US20130004313 Damper for an integrally bladed rotor |
| 01/03/2013 | US20130004302 Supersonic Turbine Moving Blade and Axial-Flow Turbine |
| 01/03/2013 | DE102010014556B4 Leitschaufel eines Verdichters Vane of a compressor |
| 01/03/2013 | CA2831488A1 Tertiary locking assembly for a thrust reverser |
| 01/02/2013 | EP2540984A2 Impingement Cooled Nozzle Liner |
| 01/02/2013 | EP2540980A2 Damper for an integrally bladed rotor |
| 01/02/2013 | EP2540979A2 Rotor assembly and reversible turbine blade retainer therefor |
| 01/02/2013 | EP2540978A2 Fan blade protection system |
| 01/02/2013 | EP2540977A2 Method of improving fatigue strength in a fan blade and corresponding fan blade |
| 01/02/2013 | EP2540976A2 Grit blast free thermal barrier coating rework |
| 01/02/2013 | EP2540975A2 Hybrid part made from monolithic ceramic skin and cmc core |
| 01/02/2013 | EP2540974A2 Fan blade with sheath |
| 01/02/2013 | EP2540973A1 Seal system for a gas turbine |
| 01/02/2013 | EP2540972A1 Blade for a gas turbine and method for producing such a blade |
| 01/02/2013 | EP2540971A1 Method for creating a platform cooling passage in a turbine rotor blade and corresponding platform cooling passage |
| 01/02/2013 | EP2540970A1 Liquid metal cooled blade |
| 01/02/2013 | EP2540969A1 Impingement cooling of turbine blades or vanes |