| 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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| 02/20/2003 | WO2003014528A1 Blade for a turbine engine and method for production of said blade |
| 02/20/2003 | WO2001064964A9 Nickel base superalloys and turbine components fabricated therefrom |
| 02/20/2003 | US20030035968 The roughness of the ceramic protective layer is reduced at at least one first location, and the original roughness is retained at at least one second location, especially on a turbine blade or vane at risk of detachment |
| 02/20/2003 | US20030035907 Protective overlayer for ceramics |
| 02/20/2003 | US20030035892 Nickel-base superalloy article with rhenium-containing protective layer, and its preparation |
| 02/20/2003 | US20030035727 Closed circuit blade-cooled turbine |
| 02/20/2003 | US20030035726 Turbine blade/vane |
| 02/20/2003 | US20030035723 Compressor outlet guide vane and diffuser assembly |
| 02/20/2003 | US20030035717 Gas turbine and method of operating a gas turbine |
| 02/20/2003 | US20030034379 Method of repairing superalloy directional castings |
| 02/20/2003 | US20030034101 Low-alloy heat-resistant steel, heat treatment method therefor, and turbine rotor comprising the same |
| 02/20/2003 | US20030033813 Cycle gas turbine engine |
| 02/19/2003 | EP1284339A1 Annular cover plate system for gas turbine rotors |
| 02/19/2003 | EP1284338A2 Tangential flow baffle |
| 02/19/2003 | EP1284337A1 Method for machining a coated gas turbine blade and a coated gas turbine blade |
| 02/19/2003 | EP1141442B1 METHOD FOR PRODUCING A METAL ALLOY POWDER SUCH AS MCrAlY AND COATINGS OBTAINED WITH SAME |
| 02/19/2003 | EP1141441B1 METHOD FOR FORMING A METAL ALLOY COATING OF THE TYPE MCrAlY |
| 02/19/2003 | EP1002141B1 Component with high temperature resistance and method for producing an anti-oxidation element |
| 02/19/2003 | CN1398322A 涡轮叶片布置 Turbine blades arranged |
| 02/18/2003 | US6521861 Method and apparatus for increasing welding rate for high aspect ratio welds |
| 02/18/2003 | US6521356 A turbine system having a component comprising a niobium-based refractory metal intermetallic composite of titanium hafnium, silicon, chromium and niobium with a high-temperature resistant protective coating of like metals minus |
| 02/18/2003 | US6521293 Method for producing a ceramic-coated blade of gas turbine |
| 02/18/2003 | US6521059 Blade and method for producing the blade |
| 02/18/2003 | US6520836 Method of forming a trailing edge cutback for a turbine bucket |
| 02/18/2003 | US6520743 Rotor blade retaining apparatus |
| 02/18/2003 | US6520742 Circular arc multi-bore fan disk |
| 02/18/2003 | US6520741 Turbomachine blade |
| 02/18/2003 | US6519849 Method for the manufacture of a welded rotor of a fluid-flow machine |
| 02/18/2003 | CA2262701C Gas turbine blade |
| 02/13/2003 | US20030031564 Stationary vanes for turbines and method for making the same |
| 02/13/2003 | US20030031556 Guide vane assembly |
| 02/13/2003 | US20030031555 Tangential flow baffle |
| 02/13/2003 | US20030029522 Coating a laser shock peening surface on the workpiece with an explosive coating; continuously firing a laser beam to to vaporize the coating and to explode and forming regions having deep compressive residual stresses |
| 02/13/2003 | US20030029171 External rotor gas turbine |
| 02/12/2003 | EP1283338A1 Gas turbine and method for operating a gas turbine |
| 02/12/2003 | EP1283328A1 Sealing bushing for cooled gas turbine blades |
| 02/12/2003 | EP1283327A2 Method for enhancing heat transfer inside a turbulated cooling passage |
| 02/12/2003 | EP1283326A1 Cooling of a turbine vane |
| 02/12/2003 | EP1283325A1 Turbomachine blade and method for production of such a blade |
| 02/12/2003 | EP1283278A2 Segmented thermal barrier coating and method of manufacturing the same |
| 02/12/2003 | EP1282780A1 An impeller for an axial flow fan and a method of mounting a blade on a hub for such fan |
| 02/11/2003 | US6517319 Gas turbine engine rotor blades |
| 02/11/2003 | US6517312 Turbine stator vane segment having internal cooling circuits |
| 02/06/2003 | WO2003010433A1 Radial impulse turbine for rotary ramjet engine |
| 02/06/2003 | WO2003010419A1 Device for reducing sealing gaps between moving and stationary components inside a non-positive-displacement machine |
| 02/06/2003 | US20030026952 Process and device for coating a temperature-stable component with a thermal protection layer |
| 02/06/2003 | US20030026700 Articles having improved residual stress profile characteristics produced by laser shock peening |
| 02/06/2003 | US20030026698 Trichannel airfoil leading edge cooling |
| 02/06/2003 | US20030026697 Cooling structure and method of manufacturing the same |
| 02/06/2003 | US20030026693 Stator of a variable-geometry axial turbine for aeronautical applications |
| 02/06/2003 | US20030026690 Extended tip turbine blade for heavy duty industrial gas turbine |
| 02/06/2003 | US20030026689 Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention |
| 02/06/2003 | US20030024915 Method using laser shock processing to provide improved residual stress profile characteristics |
| 02/06/2003 | US20030024609 Particularly suited to applications where such heat resisting steel are used as turbine members such as turbine rotors, turbine blades, turbine disks, bolts, or piping, and the like. |
| 02/06/2003 | US20030024430 Applying a slurry which comprises braze material also containing a volatile component to the substrate, drying and fusing |
| 02/05/2003 | EP1281837A1 Cooling device for turbine blade tips |
| 02/05/2003 | EP1280980A1 Method for cooling a shaft in a high-pressure expansion section of a steam turbine |
| 02/05/2003 | EP1115906B1 Method for processing the interior of a hollow part |
| 02/05/2003 | CN1395649A Device for centring tube in turbine shaft |
| 02/04/2003 | US6514629 Gas turbine blade; increased service life due to improved resistance to spallation degradation; reduced cracking in aluminum oxide layer and at its interface with platinum aluminide |
| 02/04/2003 | US6514046 Ceramic composite vane with metallic substructure |
| 02/04/2003 | US6514045 Rotor seal |
| 02/04/2003 | US6514042 Method and apparatus for cooling a wall within a gas turbine engine |
| 02/04/2003 | US6514040 Turbine engine damper |
| 02/04/2003 | US6514038 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor |
| 02/04/2003 | US6514037 Method for reducing cooled turbine element stress and element made thereby |
| 01/30/2003 | WO2003008792A1 Jet engine using exhaust gas |
| 01/30/2003 | US20030022012 Thermal barrier coating method and article |
| 01/30/2003 | US20030021905 Method for cooling engine components using multi-layer barrier coating |
| 01/30/2003 | US20030021686 Nonionic polyhydric alcohol humectant and water soluble wetting agent; fabric treatment without ironing |
| 01/30/2003 | US20030021685 Base material with cooling air hole |
| 01/30/2003 | US20030021684 Turbine blade tip cooling construction |
| 01/30/2003 | US20030021680 Second-stage turbine nozzle airfoil |
| 01/30/2003 | US20030021676 Turbine |
| 01/30/2003 | DE10140259C1 Axial turbine for exhaust gas turbocharger has blade foot of each rotor blade secured in axial slot of rotor disc via respective fixing element |
| 01/29/2003 | EP1279796A2 Selective step turbine nozzle |
| 01/29/2003 | EP1095207A4 High temperature airfoil |
| 01/29/2003 | EP0951579B1 Method of manufacturing hollow metal objects with elaborated cavities |
| 01/29/2003 | CN1100195C Blade and turbo-machine for blade machinery |
| 01/29/2003 | CN1100194C Blade for axial-flow type fluid machinery |
| 01/29/2003 | CN1100193C Turbomachine and process for cooling turbomachine |
| 01/28/2003 | US6511762 Multi-layer thermal barrier coating with transpiration cooling |
| 01/28/2003 | US6511294 Reduced-stress compressor blisk flowpath |
| 01/28/2003 | US6511293 Closed loop steam cooled airfoil |
| 01/28/2003 | US6511285 Tandem guide vanes |
| 01/28/2003 | US6510889 Directional solidification method and apparatus |
| 01/28/2003 | US6510684 Gas turbine engine |
| 01/28/2003 | CA2142924C Steam-turbine power plant and steam turbine |
| 01/23/2003 | WO2003006883A1 Coolable segment for a turbomachinery and combustion turbine |
| 01/23/2003 | WO2003006798A1 Third-stage turbine nozzle airfoil |
| 01/23/2003 | WO2003006797A1 Second-stage turbine nozzle airfoil |
| 01/23/2003 | WO2003006796A1 First-stage high pressure turbine bucket airfoil |
| 01/23/2003 | US20030017053 Method for making a fiber reinforced composite article and product |
| 01/23/2003 | US20030017052 Fourth-stage turbine bucket airfoil |
| 01/23/2003 | US20030017051 Double-wall blade for a turbine, particularly for aeronautical applications |
| 01/23/2003 | US20030017050 Turbine disk side plate |
| 01/23/2003 | US20030014972 Variable geometry turbocharger having internal bypass exhaust gas flow |
| 01/22/2003 | EP1277966A2 Serrated fan blade |
| 01/22/2003 | EP1277918A1 Double-wall blade for a variable geometry turbine nozzle |
| 01/22/2003 | EP1277917A1 Turbine disk side plate |