| 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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| 01/08/2004 | WO2004003346A1 Steam turbine |
| 01/08/2004 | US20040005477 Product having a layer which protects against corrosion, and process for producing a layer which protects against corrosion |
| 01/08/2004 | US20040005410 Process for internally coating gas turbine blades or vanes and internally coated gas turbine blade or vane produced thereby |
| 01/08/2004 | US20040005238 For the production of single-crystal components or components with a directionally solidified microstructure such as for example blades or vanes for gas turbines; can also be used for conventionally cast components. |
| 01/08/2004 | US20040005219 Rotor disc for gas turbine engine |
| 01/08/2004 | DE10256778A1 Schwingungsdämpfer Vibration |
| 01/08/2004 | DE10226295A1 Wärmedämmschicht aus einem komplexen Perowskit Thermal barrier coating from a complex perovskite |
| 01/08/2004 | CA2490619A1 Gas turbine ventilation circuitry |
| 01/07/2004 | EP1378630A1 Steam turbine |
| 01/07/2004 | EP1378629A1 Rotor for a rotating thermal engine as well as manufacturing method for such a rotor |
| 01/07/2004 | EP1378587A1 High-temperature articles and method for making |
| 01/07/2004 | EP1378583A1 Method of forming a hollow channel on the surface of a metal substrate, and related articles |
| 01/07/2004 | EP1378579A1 Precipitation hardened Co-Ni based heat-resistant alloy and production method therefor |
| 01/07/2004 | CN1465862A Improved end blade guiding propeller |
| 01/07/2004 | CN1133797C Turbo-power blade |
| 01/06/2004 | US6673709 Formation of an aluminide coating, incorporating a reactive element, on a metal substrate |
| 01/06/2004 | US6673169 Method and apparatus for repairing superalloy components |
| 01/06/2004 | US6672838 Method for making a metallic article with integral end band under compression |
| 01/06/2004 | US6672836 Coolable rotor blade for an industrial gas turbine engine |
| 01/06/2004 | US6672832 Step-down turbine platform |
| 01/06/2004 | US6672829 Turbine blade having angled squealer tip |
| 01/06/2004 | US6672786 Ceramic to metal joint assembly |
| 01/06/2004 | US6672630 Flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine |
| 01/06/2004 | US6672501 Method for repairing damaged areas in a metal component |
| 01/06/2004 | US6672075 Liquid cooling system for gas turbines |
| 01/06/2004 | US6672074 Gas turbine |
| 01/06/2004 | US6672072 Pressure boosted compressor cooling system |
| 01/06/2004 | US6672059 Vane design for use in variable geometry turbocharger |
| 01/06/2004 | US6671938 Pneumatic press vane lift installation tool |
| 01/06/2004 | CA2321640C Compressor endwall bleed system |
| 01/06/2004 | CA2289420C High temperature corrosion-resistant and abrasion-resistant coating member, and manufacturing method thereof |
| 01/02/2004 | EP1377140A2 Improved film cooling for microcircuits |
| 01/02/2004 | EP1375826A1 Radial turbine with guide vanes for reducing vibrations |
| 01/02/2004 | EP1375825A1 Failsafe film cooled wall |
| 01/02/2004 | EP1375824A2 Linked, non-plugging cooling microcircuits |
| 01/02/2004 | EP1375823A2 A method for repairing shroud tip overlap on turbine buckets |
| 01/02/2004 | EP1375701A1 Thermal barrier coating material |
| 01/02/2004 | EP1373685A1 Gas turbine blade |
| 01/02/2004 | EP1373684A1 Environmental and thermal barrier coating for ceramic components |
| 01/02/2004 | EP1373598A1 Thermal barrier coating having subsurface inclusions for improved thermal shock resistance |
| 01/02/2004 | EP1373593A2 Method and device for gas phase diffusion coating of metal components |
| 01/02/2004 | EP1010860B1 Gas turbine blade |
| 01/01/2004 | US20040002138 Alpha,2,8-sialyltransferase |
| 01/01/2004 | US20040001977 In-situ formation of multiphase deposited thermal barrier coatings |
| 01/01/2004 | US20040001965 High-temperature articles and method for making |
| 01/01/2004 | US20040001757 Methods of assembling airfoils to turbine components and assemblies thereof |
| 01/01/2004 | US20040001753 Air and steam cooled platform of a turbine blade or vane |
| 01/01/2004 | US20040000050 Method of repairing shroud tip overlap on turbine buckets |
| 12/31/2003 | WO2004001222A1 Impeller for compact turbo machines |
| 12/31/2003 | WO2004001090A1 Ceramic particle-containing self-melting alloy thermal spraying material |
| 12/31/2003 | CN1464912A Ni base sintered alloy |
| 12/31/2003 | CN1132994C Joggle joint between joggling fitting parts and its use |
| 12/30/2003 | US6670049 Metal/ceramic composite protective coating and its application |
| 12/30/2003 | US6670046 Metal substrate with composite ceramic-comprising coating embedded in recess capable of withstanding temperatures in excess of 1500 degrees F., second ceramic-comprising coating over edge of substrate adjacent periphery of first coating |
| 12/30/2003 | US6670026 Ceramic matrix composite turbine components |
| 12/30/2003 | US6669791 High strength, toughness |
| 12/30/2003 | US6669447 Turbomachine blade |
| 12/30/2003 | US6669445 Endwall shape for use in turbomachinery |
| 12/30/2003 | US6669443 Rotor platform modification and methods using brush seals in diaphragm packing area of steam turbines to eliminate rotor bowing |
| 12/30/2003 | US6669441 Exhaust-gas turbine |
| 12/30/2003 | US6668556 Gas transfer energy recovery and effervescence prevention apparatus and method |
| 12/25/2003 | US20030235494 Linked, manufacturable, non-plugging microcircuits |
| 12/24/2003 | WO2003106372A1 Heat-insulating layer made of complex perovskite |
| 12/24/2003 | DE20220621U1 Micro gas turbine for generation of electrical energy and heat has working medium heated by combustion gases from combustion chamber for combustion of biomass |
| 12/24/2003 | CN1463321A 燃气轮机 Gas turbine |
| 12/24/2003 | CN1463302A Coating forming method and coating forming material and abrasive coating forming sheet |
| 12/24/2003 | CN1463299A Method for repairing component made from Ni-based alloy |
| 12/23/2003 | US6667076 Processes for coating a temperature-stable component with a thermal protection layer |
| 12/23/2003 | US6666654 Turbine blade airfoil and turbine blade for axial-flow turbine |
| 12/23/2003 | US6666653 Inertia welding of blades to rotors |
| 12/23/2003 | US6666646 Drag reduction for gas turbine engine components |
| 12/23/2003 | US6666017 Counterrotatable booster compressor assembly for a gas turbine engine |
| 12/19/2003 | CA2432492A1 Linked manufacturable, non-plugging microcircuits |
| 12/19/2003 | CA2432490A1 Improved film cooling for microcircuits |
| 12/18/2003 | WO2003104616A1 Turbine bucket assembly and its assembling method |
| 12/18/2003 | WO2003104615A1 Workpiece with erosion-reducing surface structure |
| 12/18/2003 | US20030231961 Cylindrical blades for axial steam turbines |
| 12/18/2003 | US20030231957 Compressor stator vane |
| 12/18/2003 | US20030231955 Failsafe film cooled wall |
| 12/18/2003 | US20030230070 Single rotor turbine |
| 12/17/2003 | EP1371815A1 Abradable metallic or ceramic material; articles, casings comprising said material and its process for preparing |
| 12/17/2003 | EP1371813A1 Blading of a turbomachine |
| 12/17/2003 | EP1371812A1 Method of repairing the damaged rotor blades of a gas turbine |
| 12/17/2003 | EP1371439A1 Method of weld repairing a component with a refractory metal backing material |
| 12/17/2003 | EP1370711A2 High temperature coatings for gas turbines |
| 12/17/2003 | EP1347073A9 HIGH Cr FERRITIC HEAT RESISTANCE STEEL |
| 12/17/2003 | EP1214172B1 Laser cladding a turbine engine vane platform |
| 12/17/2003 | EP0918923B1 Configuration of cooling channels for cooling the trailing edge of gas turbine vanes |
| 12/17/2003 | EP0894943B1 Gas turbine rotor for steam cooling |
| 12/17/2003 | CN1462330A Method for forming abrasion-resistant layer for moving blade, abrasion-resistant layer and method for regeneration thereof, and gas turbine |
| 12/17/2003 | CN1461874A Housing for tubine blade and assembling method thereof |
| 12/17/2003 | CN1461872A Method and device for reducing temp. of turbine blade top region |
| 12/16/2003 | US6664506 Method using laser shock processing to provide improved residual stress profile characteristics |
| 12/16/2003 | US6663983 Yttria-stabilized zirconia containing a dispersion of chromia precipitates or particles |
| 12/16/2003 | US6663919 Process of removing a coating deposit from a through-hole in a component and component processed thereby |
| 12/11/2003 | WO2003102380A1 Control of leak zone under blade platform |
| 12/11/2003 | WO2003102378A1 Turbine moving blade |
| 12/11/2003 | WO2002027145A3 Vane assembly for a turbine and combustion turbine with this vane assembly |
| 12/11/2003 | US20030228226 Turbine rotor blade |
| 12/11/2003 | US20030228225 Turbine bucket |