| 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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| 04/04/2001 | EP1088963A2 Method and apparatus for purging turbine wheel cavities |
| 04/04/2001 | EP1088910A1 A method for improving the oxidation-resistance of metal substrates coated with thermal barrier coatings |
| 04/04/2001 | EP1088909A2 Thermal barrier coating system of a turbine component |
| 04/04/2001 | EP1088908A2 A method for smoothing the surface of a protective coating |
| 04/04/2001 | EP1088903A1 Simultaneous offset dual sided laser shock peening |
| 04/03/2001 | US6210812 For thermal barrier coating systems exposed to high temperatures, such as in a gas turbine engine |
| 04/03/2001 | US6210791 Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation |
| 04/03/2001 | US6210744 Placing component in coating chamber with an atmosphere having controllable atmosphere composition; maintaining component at constant temperature; establishing vacuum in coating chamber; controlling; depositing material forming thermal barrier |
| 04/03/2001 | US6210630 Process for manufacturing a hollow turbomachine blade and a multiple-action furnace press for use in said process |
| 04/03/2001 | US6210488 Method of removing a thermal barrier coating |
| 04/03/2001 | US6210283 Composite drive shaft |
| 04/03/2001 | US6210112 Apparatus for cooling an airfoil for a gas turbine engine |
| 04/03/2001 | US6210111 Turbine blade with platform cooling |
| 04/03/2001 | US6210108 Method for making an article portion subject to tensile stress and stress relieved article |
| 04/03/2001 | US6210104 Removal of cooling air on the suction side of a diffuser vane of a radial compressor stage of gas turbines |
| 04/03/2001 | US6209216 Methods and apparatus for measuring airfoil coordinates |
| 03/29/2001 | WO2001021847A2 Superalloys with improved weldability for high temperature applications |
| 03/28/2001 | EP1087103A2 Ceramic turbine nozzle |
| 03/28/2001 | EP1087102A2 Gas turbine bucket with impingement cooled platform |
| 03/28/2001 | EP1087101A2 Method for connecting air ducts in gas turbine rotors |
| 03/28/2001 | EP1087100A2 Compressor rotor configuration |
| 03/28/2001 | EP1087037A2 Porous element for the effusive cooling of machine components |
| 03/28/2001 | EP1086298A1 Turbine nozzle vane |
| 03/28/2001 | EP0866920B1 Process for forming a surface for contact with a flowing fluid and body with such surface regions |
| 03/27/2001 | US6207295 Article with protective coating and alloy for turbines |
| 03/27/2001 | US6206642 Compressor blade for a gas turbine engine |
| 03/27/2001 | US6206639 Enhanced fan and fan drive assembly |
| 03/27/2001 | US6206638 Low cost airfoil cooling circuit with sidewall impingement cooling chambers |
| 03/27/2001 | US6206637 Gas turbine blade |
| 03/27/2001 | US6206634 Steam turbine blade, method of manufacturing the same, steam turbine power generating plant and low pressure steam turbine |
| 03/27/2001 | US6206378 Gas turbine spindle bolt seal device |
| 03/27/2001 | CA2203299C Heat resisting steel and steam turbine rotor shaft |
| 03/22/2001 | WO2001020133A1 Film cooling hole construction in gas turbine moving-vanes |
| 03/22/2001 | DE19944923A1 Turbine blade for rotor of gas turbine; has blade crown with cap having bars and hollow spaces inside bars connected to cooling channels to supply cooling air to inside of bars |
| 03/22/2001 | CA2347888A1 Film cooling hole structure of gas turbine moving blade |
| 03/21/2001 | EP1085172A2 Composite blade root attachment |
| 03/21/2001 | EP1085171A2 Thermal barrier coated squealer tip cavity |
| 03/21/2001 | EP1085170A2 Turbine airfoil |
| 03/21/2001 | EP1084327A1 Gas turbine and method for cooling a turbine stage |
| 03/20/2001 | US6203927 Substrate with ceramic coating on surface and sintering |
| 03/20/2001 | US6203847 Coating of a discrete selective surface of an article |
| 03/20/2001 | US6203274 Steam turbine |
| 03/20/2001 | US6203269 Centrifugal air flow control |
| 03/20/2001 | US6203021 Abradable seal having a cut pattern |
| 03/20/2001 | US6202273 Shim removing tool |
| 03/15/2001 | WO2001018277A1 In-situ formation of multiphase electron beam physical vapor deposited barrier coatings for turbine components |
| 03/15/2001 | WO2001018274A1 In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components |
| 03/15/2001 | DE19939179A1 Gas turbine blade with cooling has rows of cooling channels associated with suction side and pressure side |
| 03/14/2001 | EP1083345A2 High-stiffness composite shaft |
| 03/14/2001 | EP1083299A2 Internally cooled blade tip shroud |
| 03/14/2001 | EP1082523A1 A component for a gas turbine |
| 03/14/2001 | EP1082216A2 Product with an anticorrosion protective layer and a method for producing an anticorrosion protective |
| 03/14/2001 | EP0593736B1 Heat treatment and repair of cobalt-base superalloy articles |
| 03/14/2001 | CN1063256C 叶轮 Impeller |
| 03/13/2001 | US6201315 Wind power motor |
| 03/13/2001 | US6200092 Ceramic turbine nozzle |
| 03/13/2001 | US6200088 On-line monitor for detecting excessive temperatures of critical components of a turbine |
| 03/13/2001 | US6200087 Pressure compensated turbine nozzle |
| 03/13/2001 | US6199746 Method for preparing superalloy castings using a metallurgically bonded tapered plug |
| 03/13/2001 | US6199276 Method for removing a dense ceramic thermal barrier coating from a surface |
| 03/08/2001 | WO2001015869A2 Shim removing tool and method |
| 03/08/2001 | WO2001015866A1 Method and device for treating the surface of a part |
| 03/08/2001 | CA2383082A1 Method and device for the surface threatment of a component |
| 03/08/2001 | CA2346035A1 Shim removing tool and method |
| 03/07/2001 | EP1081337A2 Cover plates for turbomachine blades |
| 03/07/2001 | EP1081335A2 Stator assembly for a rotary machine and method for making the stator assembly |
| 03/07/2001 | EP1081334A1 Turbine airfoil or vane having movable nozzle ribs |
| 03/07/2001 | EP1081333A2 Plastically formed hybrid airfoil |
| 03/07/2001 | EP1081332A1 Axial flow turbines |
| 03/07/2001 | EP1081239A1 Method for setting up and controlling confinement media flow in laser shock peening |
| 03/07/2001 | CN1062938C Fluid machinery having blade apparatus and blade apparatus for fluid machinery |
| 03/06/2001 | US6196799 Gas turbine moving blade platform |
| 03/06/2001 | US6196798 Gas turbine cooling blade |
| 03/06/2001 | US6196794 Gas turbine stator vane structure and unit for constituting same |
| 03/06/2001 | US6196792 Preferentially cooled turbine shroud |
| 03/06/2001 | US6196791 Gas turbine cooling moving blades |
| 03/06/2001 | US6195983 Leaned and swept fan outlet guide vanes |
| 03/06/2001 | US6195982 Apparatus and method of active flutter control |
| 03/06/2001 | US6195979 Cooling apparatus for gas turbine moving blade and gas turbine equipped with same |
| 03/06/2001 | US6195891 Method for identification and repair of indications in hardware |
| 03/01/2001 | DE19940556A1 Cooling device for guide and rotor blades of gas turbines has intermediate part with smooth surface between neighboring blades to form spatial and gas-proof seal |
| 03/01/2001 | DE19940525A1 Wärmestaueinheit für eine Rotoranordnung Heat storage unit for a rotor assembly |
| 02/28/2001 | EP1079075A2 Stator assembly for a rotary machine and clip member for a stator assembly |
| 02/28/2001 | EP1079074A2 Stator vane and stator assembly for a rotary machine |
| 02/28/2001 | EP1079073A2 Modified diffusion aluminide coating for internal surfaces of gas turbine components |
| 02/28/2001 | EP1079072A2 Blade tip cooling |
| 02/28/2001 | EP1079071A2 Turbine blade with preferentially cooled trailing edge pressure wall |
| 02/28/2001 | EP1079070A2 Heatshield for a turbine rotor |
| 02/28/2001 | EP1079069A2 Steam cooling system for a gas turbine |
| 02/28/2001 | EP1079068A2 Connector tube for a turbine rotor cooling circuit |
| 02/28/2001 | EP1079067A2 A cooling air supply system for a rotor |
| 02/27/2001 | US6194086 Nickel and cobalt superalloy substrate; low pressure plasma spraying of abrasives |
| 02/27/2001 | US6193469 High toughness heat-resistant steel, turbine rotor and method of producing the same |
| 02/27/2001 | US6193465 Trapped insert turbine airfoil |
| 02/27/2001 | US6193141 Single crystal turbine components made using a moving zone transient liquid phase bonded sandwich construction |
| 02/27/2001 | US6192670 Radial flow turbine with internal evaporative blade cooling |
| 02/22/2001 | WO2001012954A2 Turbine or system with internal evaporative blade cooling |
| 02/22/2001 | WO2001012382A1 Method for replacing a turbine vane airfoil |
| 02/22/2001 | WO2001012381A1 Laser cladding a turbine engine vane platform |
| 02/22/2001 | DE10031137A1 Method and device for fastening air-conducting blades on rotor includes running air-conducting blades onto rotor from opposite sides fastening them with no edge using resistance welding |