| 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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| 07/26/2005 | US6921586 Aluminum- containing overlay and a coating of 20-90% ruthenium, 2-60% chromium, </= 50% aluminum, </= 20% of a platinum group metal and a balance of nickel, cobalt and iron |
| 07/26/2005 | US6921251 Aluminide or chromide coating of turbine engine rotor component |
| 07/26/2005 | US6921246 Methods and apparatus for assembling gas turbine nozzles |
| 07/26/2005 | US6921207 Foil bearing |
| 07/26/2005 | US6921014 Method for forming a channel on the surface of a metal substrate |
| 07/26/2005 | US6920754 High-pressure ratio turbocharger |
| 07/26/2005 | CA2366726C Cooling structure for a gas turbine |
| 07/21/2005 | WO2005065002A2 Rotor for a turbomachine, and method for the production of such a rotor |
| 07/21/2005 | US20050158590 A superalloy substrate coated with a ceramic having microgaps between its columnar grains and an atomic layer-deposited inorganic overcoating which conformally fills the plurality of gaps; sintering-resistance; high-temperature heat resistance; noncracking; oxidation/corrosion resistance; stress-relief |
| 07/21/2005 | US20050158460 Method for protecting new/used engine parts |
| 07/21/2005 | US20050158174 Turbine blade attachment lightening holes |
| 07/21/2005 | US20050158171 Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
| 07/21/2005 | US20050158170 Wet friction device with inward and outward circulating cooling means |
| 07/20/2005 | EP1555392A2 Cantilevered stator stage |
| 07/20/2005 | EP1555391A2 Hybrid ceramic matrix composite turbine blade |
| 07/20/2005 | EP1555390A1 Cooling air exit openings for turbine blade |
| 07/20/2005 | EP1555333A2 Thermal barrier coating system |
| 07/20/2005 | EP1555329A1 Workpiece with internal compressive stresses, method and apparatus for producing internal compressive stresses |
| 07/20/2005 | EP1458981B1 Compressor for gas turbines |
| 07/20/2005 | EP1345732B1 Method for smoothing the surface of a gas turbine blade |
| 07/20/2005 | EP1082523B1 A component for a gas turbine |
| 07/20/2005 | CN2711391Y Final stage blade for large air cooling turbine |
| 07/20/2005 | CN1643236A Turbine blade pocket shroud |
| 07/19/2005 | US6919956 Method of automatically repairing cracks and apparatus for use in such method |
| 07/19/2005 | US6919121 For use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. |
| 07/19/2005 | US6918747 Method and system for detecting damage to the rotor of an aircraft engine |
| 07/19/2005 | US6918742 Combustion turbine with airfoil having multi-section diffusion cooling holes and methods of making same |
| 07/19/2005 | US6918723 Shaft/hub connection |
| 07/19/2005 | CA2356479C Shaft structure and bearing structure for tail end of rotor of gas turbine |
| 07/14/2005 | WO2005064121A1 Cambered vane for use in turbochargers |
| 07/14/2005 | WO2005064120A1 Disk of a disk rotor for a gas turbine |
| 07/14/2005 | WO2005022065A3 Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys |
| 07/14/2005 | WO2004113587A9 Metal component, turbine component, gas turbine engine, surface processing method, and steam turbine engine |
| 07/14/2005 | US20050153160 Metallic substrate with ceramic coating consisting of a formula of NdxZr1-xOy with yttria and hafnia added and dissolved in; protective coatings for turbine components, (e.g. blades and vanes) to prevent the components from overheating during high temperature operation |
| 07/14/2005 | US20050153158 Durable thermal barrier coating having low thermal conductivity |
| 07/14/2005 | US20050152805 Method for forming a wear-resistant hard-face contact area on a workpiece, such as a gas turbine engine part |
| 07/14/2005 | US20050152785 Turbine bucket cooling passages and internal core for producing the passages |
| 07/14/2005 | US20050152777 Resilent seal on leading edge of turbine inner shroud |
| 07/14/2005 | US20050152776 Comprising a shaft end associated with a compressor; used with regard to intermediate pressure compressors of a turbine engine |
| 07/14/2005 | DE10361882A1 Rotor for a high pressure turbine of an aircraft engine comprises a turbine plate with blades cooled via cooling channels and film cooling holes |
| 07/14/2005 | CA2551287A1 Disk of a disk rotor for a gas turbine |
| 07/13/2005 | EP1553261A2 Fanned trailing edge teardrop array |
| 07/13/2005 | EP1553203A1 Method for producing hollow airfoils, also to produce a rotor with hollow airfoils |
| 07/13/2005 | EP1553145A1 Touch-up of multi layer paint oxides for gas turbine disks and seals |
| 07/13/2005 | EP1552111A1 Gas turbine ventilation circuitry |
| 07/13/2005 | EP1552037A1 Method for removing a layer area of a component |
| 07/13/2005 | EP1466037B1 High-temperature protective coating |
| 07/13/2005 | EP1152848A4 Method and apparatus for production of a cast component |
| 07/13/2005 | CN1639446A Turbine moving blade |
| 07/13/2005 | CN1638897A Method of removing casting defects |
| 07/13/2005 | CN1638240A Electric rotating machinery |
| 07/13/2005 | CN1637246A Airfoil surface impedance modification for noise reduction in turbofan engines |
| 07/13/2005 | CN1637235A Cooled vane cluster |
| 07/12/2005 | US6916561 Thermal barrier coatings with lower porosity for improved impact and erosion resistance |
| 07/12/2005 | US6916551 Zirconium or erbium oxide; wear resistance, stability, durability |
| 07/12/2005 | US6916429 Comprises treatment with fluosilic acid; for turbine engines/air foils |
| 07/12/2005 | US6916387 Repairing a void on a nickel or cobalt base superalloy investment casting by vibrating the casting before repairing; vibrating the casting while filling the void; impinging each incremental deposit with a cooling gas |
| 07/12/2005 | US6916155 Cooling circuits for a gas turbine blade |
| 07/12/2005 | US6916151 Ventilation device for a high pressure turbine rotor of a turbomachine |
| 07/12/2005 | US6916150 Cooling system for a tip of a turbine blade |
| 07/12/2005 | US6916021 Sealing arrangement |
| 07/07/2005 | WO2005061856A1 Turbine component comprising a thermal insulation layer and an anti-erosion layer |
| 07/07/2005 | WO2005061854A1 Gas turbine tip shroud rails |
| 07/07/2005 | US20050147829 high glass transition temperature and excellent insulation volume resistance and insulation breakdown voltage at high ambient temperatures; film is a blend of polyester and a polyimide |
| 07/07/2005 | US20050147498 Heat-dissipating module, fan structure and impeller thereof |
| 07/07/2005 | US20050147497 Method of improving the flow conditions in an axial-flow compressor, and axial-flow compressor for carrying out the method |
| 07/07/2005 | US20050144969 Cold air refrigerating system and turborxpander turbine for this system |
| 07/07/2005 | DE10358625A1 Anordnung zur Lagerentlastung in einer Gasturbine Arrangement for storage discharge in a gas turbine |
| 07/07/2005 | DE10358421A1 Rotor für eine Turbomaschine Rotor for a turbomachine |
| 07/07/2005 | DE10357656A1 Verfahren zur Herstellung von Gasturbinenbauteilen und Bauteil für eine Gasturbine A process for the manufacture of gas turbine components and the component for a gas turbine |
| 07/07/2005 | DE10357075A1 Verfahren zur Lärmreduzierung von Turbomaschinen Procedures for noise reduction of turbomachinery |
| 07/07/2005 | DE10356586A1 Verdichterrotor Compressor rotor |
| 07/07/2005 | DE10355240A1 Strömungsarbeitsmaschine mit Fluidentnahme Turbomachine with fluid removal |
| 07/06/2005 | EP1550744A1 Thermal barrier coatings with lower porosity for improved impact and erosion resistance |
| 07/06/2005 | EP1550743A2 Thermal barrier coatings having lower layer for improved adherence to bond coat |
| 07/06/2005 | EP1550741A1 Rotor and coating method therefor |
| 07/06/2005 | EP1550737A1 Thermal barrier coatings with improved impact and erosion resistance |
| 07/06/2005 | EP1550645A2 Ceramic compositions for thermal barrier coatings stabilized in the cubic crystalline phase |
| 07/06/2005 | EP1550644A1 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
| 07/06/2005 | EP1550643A2 Ceramic compositions for low conductivity thermal barrier coatings |
| 07/06/2005 | EP1550642A2 Ceramic compositions useful for thermal barrier coatings having reduced thermal conductivity |
| 07/06/2005 | EP1549782A1 A thermal barrier coating and a method of applying such a coating |
| 07/06/2005 | EP1165941B1 High temperature erosion resistant, abradable thermal barrier composite coating |
| 07/06/2005 | CN1209548C Deformed material welding rotor of steam turbine |
| 07/05/2005 | US6915236 Method and system for automated repair design of damaged blades of a compressor or turbine |
| 07/05/2005 | US6914215 Real time laser shock peening quality assurance by natural frequency analysis |
| 07/05/2005 | US6914214 Method of forming a shaped hole |
| 07/05/2005 | US6914210 Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
| 07/05/2005 | US6913655 Niobium-silicide based composities resistant to high temperature oxidation |
| 07/05/2005 | US6913445 Center located cutter teeth on shrouded turbine blades |
| 07/05/2005 | US6913440 Variable-geometry turbine stator blade, particularly for aircraft engines |
| 06/30/2005 | WO2005059313A2 Vane and throat shaping for a radial turbine assembly |
| 06/30/2005 | WO2005042959A3 Engine balancing system and method |
| 06/30/2005 | US20050142395 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
| 06/30/2005 | US20050142394 Thermal barrier coatings with lower porosity for improved impact and erosion resistance |
| 06/30/2005 | US20050142393 Ceramic of zirconia stabilized in the cubic crystalline phase with three metal oxides (e.g. yttria, ytterbia, hafnia or tantalum oxide); physical vapor deposition onto metal substrate exposed to high temperatures |
| 06/30/2005 | US20050142392 zirconia and stabilizer with three metal oxides (yttria, lanthana and ytterbia); physical vapor deposition onto metal substrate exposed to high temperatures; columnar microstructure |
| 06/30/2005 | US20050141992 Fan assembly |
| 06/30/2005 | US20050141990 Turbomachine wtih fluid supply |
| 06/30/2005 | US20050139581 High-strength superalloy joining method for repairing turbine blades |