| 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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| 02/12/2007 | CA2555113A1 Metal part processed by compression of sub-layers, production process therefor |
| 02/08/2007 | WO2007015916A2 Reinforcement rings for a diffuser section of a tip turbine engine fan rotor assembly |
| 02/08/2007 | WO2007014828A1 A method and a device for production of a set of holes |
| 02/08/2007 | WO2007014543A1 Securing element for fastening moving blades |
| 02/08/2007 | WO2007001435A3 Adaptive machining and weld repair process |
| 02/08/2007 | US20070031261 Turbine having variable throat |
| 02/08/2007 | US20070031252 Component comprising a multiplicity of cooling passages |
| 02/08/2007 | US20070031251 Blade cooling |
| 02/08/2007 | US20070031249 Gas turbine engine and a rotor for a gas turbine engine |
| 02/08/2007 | US20070031241 Cooling arrangement |
| 02/08/2007 | DE102005047739B3 Substrate with matrix layer for turbine systems and production process has multilayer of and or encapsulated nanoparticles that release a colored material above a threshold temperature |
| 02/07/2007 | EP1750018A2 Surfaces and articles resistant to impacting liquids |
| 02/07/2007 | EP1749975A2 Cooled turbine shroud |
| 02/07/2007 | EP1749972A2 Turbine component comprising a multiplicity of cooling passages |
| 02/07/2007 | EP1749971A2 Gas turbine blade |
| 02/07/2007 | EP1749970A2 Turbine airfoil platform extension for low buttress stress |
| 02/07/2007 | EP1749969A1 Inspection of the blades of a turbine |
| 02/07/2007 | EP1749968A2 Turbine blades |
| 02/07/2007 | EP1749967A2 Cooling arrangement for a gas turbine |
| 02/07/2007 | EP1748967A1 Cement-based systems using plastification/extrusion auxiliaries prepared from raw cotton linters |
| 02/07/2007 | EP1040736B1 Synthetic jet actuators for cooling heated bodies and environments |
| 02/07/2007 | CN1910346A Curved face vane for turbocharger |
| 02/07/2007 | CN1910344A Turbine blade and gas turbine equipped with a turbine blade of this type |
| 02/07/2007 | CN1910343A Cooled blade for a gas turbine |
| 02/07/2007 | CN1910307A Alloy coating for diffusion barrier, method for forming same, and high-temperature device member |
| 02/07/2007 | CN1908380A Turbine blades |
| 02/07/2007 | CN1908379A Duckbill-shape structure of turbine airfoil platform for low buttress stress |
| 02/07/2007 | CN1908378A Energy-gathering pulse type steam turbine |
| 02/07/2007 | CN1908221A Method for microstructure control of ceramic thermal spray coating |
| 02/07/2007 | CN1298978C Cooling system for gas turbine |
| 02/07/2007 | CN1298977C Turbocharger comprising a torsional-vibration damper |
| 02/07/2007 | CN1298965C Turbine and its manufacture |
| 02/06/2007 | US7172820 Strengthened bond coats for thermal barrier coatings |
| 02/06/2007 | US7172787 Multilayer element of Nickel alloy, spraying and removing layer by peeling |
| 02/06/2007 | CA2554341A1 Thermally compliant turbine shroud mounting |
| 02/06/2007 | CA2554137A1 Thermally compliant turbine shroud mounting assembly |
| 02/06/2007 | CA2554121A1 Thermally compliant turbine shroud assembly |
| 02/06/2007 | CA2165641C A method of applying a thermal barrier coating to a superalloy article and a thermal barrier coating |
| 02/05/2007 | CA2552794A1 Cooled turbine shroud |
| 02/01/2007 | WO2007014005A1 Cmc with multiple matrix phases separated by diffusion barrier |
| 02/01/2007 | WO2007013892A2 Composite turbomachine impeller and method of manufacture |
| 02/01/2007 | WO2007012592A1 Cooled turbine blade for a gas turbine and use of such a turbine blade |
| 02/01/2007 | WO2007012590A1 Cooled turbine blade for a gas turbine and use of such a turbine blade |
| 02/01/2007 | WO2007012587A1 Gas turbine blade and platform element for a gas-turbine blade ring, supporting structure for fastening it, gas-turbine blade ring and its use |
| 02/01/2007 | WO2007012338A1 Method of repairing a component comprising a directed microstructure, by setting a temperature gradient during exposure to the laser heat; a component produced by such a method |
| 02/01/2007 | US20070026256 Capable of enhancing oxidation resistance of an Ni-base superalloy and at the same time, controlling the formation of secondary reaction zone |
| 02/01/2007 | US20070025855 Checking of turbomachine blades |
| 02/01/2007 | US20070025852 Cooling channel formed in a wall |
| 02/01/2007 | US20070025851 Core for turbomachine blades |
| 02/01/2007 | US20070025846 Vortical flow rotor |
| 02/01/2007 | US20070023485 Method of repairing a blade of a one-piece bladed disc of a turbomachine and test piece for implementing the method |
| 02/01/2007 | US20070023403 Method and device for welding structural parts |
| 02/01/2007 | US20070023392 Method for removing at least one area of a layer of a component consisting of metal or a metal compound |
| 02/01/2007 | US20070023157 Apparatus and method for reducing operating stress in a turbine blade and the like |
| 02/01/2007 | DE102005035901A1 Rotor blades` position securing unit for gas turbine, has plate-like base body having recess formed between its two end sections, where recess defines middle section of body and sections have contact surfaces running parallel to each other |
| 02/01/2007 | DE102005033625A1 Production and/or repair of an integrated gas turbine rotor comprises preparing a rotor base body, forming a moving blade by powder metallurgical injection molding and joining the moving blade to the rotor base body |
| 02/01/2007 | DE102005033591A1 Hollow blade for a gas turbine comprises a hollow chamber containing a heat resistant filler to provide a sulfitation protection for the surfaces of the hollow chamber |
| 02/01/2007 | DE102004041392B4 Dickenprofil eines Verdichterlaufrads mit lokalisierter Verdickung Thickness profile of a compressor rotor with localized thickening |
| 02/01/2007 | CA2553240A1 Method for restoring portion of turbine component |
| 01/31/2007 | EP1748169A1 Fixation of a seal arrangement on a rotor of a turbomachine |
| 01/31/2007 | EP1748154A2 Locking mechanism for fan blades |
| 01/31/2007 | EP1748153A1 Turbomachine blade and turbomachine comprising such a blade |
| 01/31/2007 | EP1747840A1 Method of repairing a blade of an integrally bladed turbine rotor disc and test-piece for carrying out the method |
| 01/31/2007 | EP1747834A1 Cooling channel within a part of the wall |
| 01/31/2007 | EP1747349A1 Blade for turbomachinery comprising a shroud and a weight-optimised sealing strip |
| 01/31/2007 | CN1906380A Turbine blade and gas turbine with such a turbine blade |
| 01/31/2007 | CN1903494A Method for repairing a blade of a one-piece bladed disc of aturbine engine and a test piece for implementing the method |
| 01/30/2007 | US7169242 Method of removing casting defects |
| 01/30/2007 | US7169241 Ni-based superalloy having high oxidation resistance and gas turbine part |
| 01/30/2007 | US7168921 Cooling system for an airfoil |
| 01/30/2007 | US7168919 Turbine blade and turbine rotor assembly |
| 01/30/2007 | US7168916 Welded rotor for a thermal machine, and process for producing a rotor of this type |
| 01/30/2007 | US7168914 Gas turbine stationary blade |
| 01/29/2007 | CA2554092A1 Fan rotor blade locking system |
| 01/29/2007 | CA2551614A1 Method for repairing a blade of a one-piece bladed disc of a turbine engine and a test piece for implementing the method |
| 01/28/2007 | CA2553880A1 Turbine engine blade control |
| 01/28/2007 | CA2551889A1 Cooled shroud assembly and method of cooling a shroud |
| 01/26/2007 | CA2553860A1 Cooling channel inside a wall |
| 01/25/2007 | WO2007011355A1 Variable nozzle turbocharger |
| 01/25/2007 | WO2007010329A1 Wind turbine blade |
| 01/25/2007 | US20070020399 Diffusion barrier and protective coating for turbine engine component and method for forming |
| 01/25/2007 | US20070020102 Gas turbine blade or vane and platform element for a gas turbine blade or vane ring of a gas turbine, supporting structure for securing gas turbine blades or vanes arranged in a ring, gas turbine blade or vane ring and the use of a gas turbine blade or vane ring |
| 01/25/2007 | US20070020101 Fan rotor design for coincidence avoidance |
| 01/25/2007 | US20070020099 Noise reduction of aircraft flap |
| 01/25/2007 | US20070017958 Method for coating a substrate and articles coated therewith |
| 01/24/2007 | EP1746252A2 Structural strut and shroud element |
| 01/24/2007 | EP1746250A1 Vibration damping elements for an axial holding ring of turbomachine fan blades |
| 01/24/2007 | EP1746249A2 Fan rotor |
| 01/24/2007 | EP1745195A1 Non-positive-displacement machine bucket |
| 01/24/2007 | EP1744953A1 Boundary layer suction arrangement |
| 01/24/2007 | CN1902379A Profiled blades for turbocharger turbines, compressors, and the like |
| 01/24/2007 | CN1902378A Disk of a disk rotor for a gas turbine |
| 01/24/2007 | CN1297057C Electric rotating machinery |
| 01/24/2007 | CN1296611C Exhaust diffuser for axial-flow turbine |
| 01/24/2007 | CN1296173C Method for removing coating material from a cooling hole of a gas turbine engine component |
| 01/23/2007 | USRE39479 Durable turbine nozzle |
| 01/23/2007 | US7167364 Cooler with blower between two heatsinks |
| 01/23/2007 | US7166373 Ceramic compositions for thermal barrier coatings with improved mechanical properties |
| 01/23/2007 | US7166372 creep resistance and high strength overcoatings comprising alloys of chromium, aluminum, yttrium and nickel, cobalt, iron or hafnium having discrete nitride particles, used on substrates such as blades and vanes for gas turbine engines |
| 01/23/2007 | US7166175 Method and device for hardening a metal component by plasma pulse technology |