| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
|---|
| 07/12/2002 | CA2506484A1 Blade structure in a gas turbine |
| 07/12/2002 | CA2506293A1 Blade structure in a gas turbine |
| 07/12/2002 | CA2506105A1 Blade structure in a gas turbine |
| 07/11/2002 | WO2002053875A1 Assembly method and jig for integrally covered axially inserted bucket blades |
| 07/11/2002 | US20020091459 Method for reconditioning blades |
| 07/11/2002 | US20020090527 Method for improving the oxidation-resistance of metal substrates coated with thermal barrier coatings |
| 07/11/2002 | US20020090302 Turbomachine blade |
| 07/11/2002 | US20020090301 Method and apparatus for reducing turbine blade tip temperatures |
| 07/11/2002 | US20020090300 Mounting arrangement for fixing a fan blade to a disk of a turbojet engine |
| 07/11/2002 | US20020090298 Component of a flow machine, with inspection aperture |
| 07/11/2002 | US20020090296 Division wall and shroud of gas turbine |
| 07/11/2002 | US20020090295 Cooling structure for a gas turbine |
| 07/11/2002 | US20020090294 Truncated rib turbine nozzle |
| 07/11/2002 | US20020089248 Gas turbomachinery generator |
| 07/11/2002 | US20020088270 Water-flow testing apparatus |
| 07/11/2002 | DE10126896A1 Protective coating used for turbines comprises a mono- or multi-layer sealing layer made from an amorphous material |
| 07/11/2002 | DE10063653A1 Feed pump such as exhaust gas supercharger has one pump vane or entire pumpwheel of different material from shaft, namely carbon fiber or graphite |
| 07/11/2002 | DE10063309A1 Cooling air aperture fabricating system for metallic component of gas turbine, including turbine blade, involves removal of metal layers by sublimation |
| 07/11/2002 | CA2364128A1 Retention system for combined or cascade blades |
| 07/10/2002 | EP1221604A2 Water-flow testing apparatus |
| 07/10/2002 | EP1221539A2 Sealing for shrouds of a gas turbine |
| 07/10/2002 | EP1221538A2 Cooled turbine stator blade |
| 07/10/2002 | EP1221537A2 Method and apparatus for reducing turbine blade tip temperatures |
| 07/10/2002 | EP1221536A2 Cooling structure for a gas turbine |
| 07/10/2002 | CN1357642A Low-density antioxidant superalloy material capable of maintaining heat insulating coating without needing adhesive layer |
| 07/10/2002 | CN1087389C Working vane assembly method and equipment |
| 07/09/2002 | US6416289 Axial flow turbines |
| 07/09/2002 | US6416286 System and method for securing a radially inserted integral closure bucket to a turbine rotor wheel assembly having axially inserted buckets |
| 07/09/2002 | US6416284 Turbine blade for gas turbine engine and method of cooling same |
| 07/09/2002 | US6416283 Electrochemical machining process, electrode therefor and turbine bucket with turbulated cooling passage |
| 07/09/2002 | US6416282 Rotor for a gas turbine |
| 07/09/2002 | US6416279 Cooled gas turbine component with adjustable cooling |
| 07/09/2002 | US6416278 Turbine nozzle segment and method of repairing same |
| 07/09/2002 | US6416276 Heat shield device in gas turbines |
| 07/09/2002 | US6416275 Recessed impingement insert metering plate for gas turbine nozzles |
| 07/09/2002 | US6416246 Connecting arrangement for two rotor disks of an axial-flow turbomachine |
| 07/09/2002 | CA2261184C Cooled stationary blade of a gas turbine |
| 07/09/2002 | CA2260230C Cooled stationary blade of a gas turbine |
| 07/04/2002 | WO2002052126A2 Method of reducing burr formation during turbine bucket cover machining |
| 07/04/2002 | WO2002052056A1 HIGH Cr FERRITIC HEAT RESISTANCE STEEL |
| 07/04/2002 | WO2002051586A1 Method for smoothing the surface of a gas turbine blade |
| 07/04/2002 | WO2002051578A1 Method for laser welding a workpiece |
| 07/04/2002 | US20020086117 Dense vertically cracked thermal barrier coating process to facilitate post-coat surface finishing |
| 07/04/2002 | US20020085918 Turbine blade airfoil, turbine blade and turbine blade cascade for axial-flow turbine |
| 07/04/2002 | US20020085917 System and method for securing a radially inserted integral closure bucket to a turbine rotor wheel assembly having axially inserted buckets |
| 07/04/2002 | US20020085910 Apparatus and methods for localized cooling of gas turbine nozzle walls |
| 07/04/2002 | US20020085908 Gas Turbine |
| 07/04/2002 | DE10065406A1 Verfahren zum Reparieren von Schadstellen an einem Metallbauteil Method for repairing damaged areas in a metal component |
| 07/04/2002 | DE10064271A1 Vorrichtung zur Prallkühlung eines in einer Strömungskraftmaschine hitzeexponierten Bauteils sowie Verfahren hierzu Apparatus for impingement cooling a heat-exposed in a turbomachine component and method therefor |
| 07/04/2002 | DE10064269A1 Komponente einer Strömungsmaschine mit Inspektionsöffnung Component of a turbomachine with inspection hole |
| 07/04/2002 | DE10064267A1 Verfahren zum schnellen Herstellen von hohlen Turbinenschaufeln für die Fertigungsentwicklung und Bauteiltests Method for rapidly producing hollow turbine blades for production development and component tests |
| 07/04/2002 | DE10064266A1 Verfahren zur Verringerung der Varianz im Kühlmediumverbrauch von Komponenten einer Strömungsmaschine A method for reducing the variance in the cooling medium consumption of components of a turbomachine |
| 07/04/2002 | DE10064265A1 Vorrichtung und Verfahren zur Kühlung einer Plattform einer Turbinenschaufel Apparatus and method for cooling a platform of a turbine blade |
| 07/03/2002 | EP1219786A2 Vane installation tool |
| 07/03/2002 | EP1219784A2 Apparatus and method for localized cooling of gas turbine nozzle walls |
| 07/03/2002 | EP1219782A2 Bladed rotor assembly |
| 07/03/2002 | EP1219781A2 Device and method to cool a platform of a turbine blade |
| 07/03/2002 | EP1219780A2 Impingement cooling of a turbomachine component |
| 07/03/2002 | EP1219779A2 Turbo machine component with inspection hole |
| 07/03/2002 | EP1219778A2 Gas turbine blade with platform undercut |
| 07/03/2002 | EP1219728A1 Process for stripping a turbine blade |
| 07/03/2002 | EP1219721A2 A dense vertically cracked thermal barrier coating process to facilitate post-coat surface finishing |
| 07/03/2002 | EP1219389A1 Method for smoothing the external surface of a gas turbine blade |
| 07/03/2002 | EP1219381A1 Method of laser welding |
| 07/03/2002 | EP1219375A2 Method for repairing damaged areas on a metallic workpiece |
| 07/03/2002 | EP1218564A1 In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components |
| 07/03/2002 | EP1218145A1 Method and device for treating the surface of a part |
| 07/03/2002 | EP0814234B1 Stationary blade for gas turbine |
| 07/02/2002 | US6413650 Method for repairing superalloy castings using a metallurgically bonded tapered plug |
| 07/02/2002 | US6413584 Electrodepositing platinum on a nickel superalloy, vapor depositing aluminum to form aluminide, and allowing interdiffusion; improved durability |
| 07/02/2002 | US6413578 Applying ceramic paste; heating |
| 07/02/2002 | US6413051 Article including a composite laminated end portion with a discrete end barrier and method for making and repairing |
| 07/02/2002 | US6413050 Friction damped turbine blade and method |
| 07/02/2002 | US6413045 Turbine blades |
| 07/02/2002 | US6413044 Blade cooling in gas turbine |
| 07/02/2002 | US6413042 Stationary flowpath components for gas turbine engines |
| 07/02/2002 | US6413041 Method and apparatus for closing holes in superalloy gas turbine blades |
| 07/02/2002 | US6413040 Support pedestals for interconnecting a cover and nozzle band wall in a gas turbine nozzle segment |
| 07/02/2002 | US6412541 Process for producing a thermally loaded casting |
| 07/02/2002 | US6412161 Shim removing method |
| 06/27/2002 | WO2002050411A2 Tangential on board injector with auxiliary supply of cooled air |
| 06/27/2002 | WO2002050402A1 Impingement cooling scheme for platform of turbine bucket |
| 06/27/2002 | WO2002050323A2 Nickel diffusion braze alloy and method for repair of superalloys |
| 06/27/2002 | WO2002049795A1 Laser machining cooling holes in gas turbine components |
| 06/27/2002 | US20020081396 Turbomachines and similar apparatus having components formed of silicon nitride ceramic and includes an outer layer formed of an oxide compound, preferably tantalum oxide |
| 06/27/2002 | US20020081206 Turbine bucket natural frequency tuning rib |
| 06/27/2002 | US20020081205 Reduced stress rotor blade and disk assembly |
| 06/27/2002 | US20020081204 Flush bucket cover |
| 06/27/2002 | US20020081199 Bolted joint for rotor disks and method of reducing thermal gradients therein |
| 06/27/2002 | US20020081197 Fabricating turbine rotors composed of separate components |
| 06/27/2002 | US20020081196 Low windage loss, light weight closure bucket design and related method |
| 06/27/2002 | US20020081192 Bolted joint for rotor disks and method of reducing thermal gradients therein |
| 06/27/2002 | US20020078563 Pneumatic press vane lift installation tool |
| 06/27/2002 | DE10134611A1 Fixing device for a blade mounting of a compressor or turbine stage of a gas turbine system comprises a blade having a counter-contour corresponding to a connecting element of a wedge element to produce a form-locking connection |
| 06/27/2002 | CA2559618A1 Pneumatic press vane lift installation tool |
| 06/27/2002 | CA2366179A1 Method for removing a coating from a turbine blade |
| 06/26/2002 | EP1217231A1 Bolted joint for rotor disks and method of reducing thermal gradients therein |
| 06/26/2002 | EP1217173A2 Vane for use in turbo machines |
| 06/26/2002 | EP1217172A2 Method for the reduction of the variance of the cooling medium consumption in components of a turbomachine |
| 06/26/2002 | EP1217171A2 Turbine bucket natural frequency tuning rib |