| 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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| 08/14/2002 | EP1231358A2 Airfoil shape for a turbine nozzle |
| 08/14/2002 | EP1231010A1 Transient liquid phase bonding repair for turbine blades and vanes |
| 08/14/2002 | DE10110102A1 Rotorschaufel Rotor blade |
| 08/14/2002 | CN1364213A Hydraulic seal for rotary pumps |
| 08/13/2002 | US6432487 Applying layers of thermal barrier coating on component, utilizing nozzle at first distance from component; applying outer layer of thermal barrier coating on component, with nozzle at second distance from component |
| 08/13/2002 | US6432478 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 08/13/2002 | US6431837 Stitched composite fan blade |
| 08/13/2002 | US6431836 Blade lock and process for manufacturing a blade lock |
| 08/13/2002 | US6431835 Fan blade compliant shim |
| 08/13/2002 | US6431833 Gas turbine bucket with impingement cooled platform |
| 08/13/2002 | US6431832 Gas turbine engine airfoils with improved cooling |
| 08/13/2002 | US6431829 Turbine device |
| 08/13/2002 | US6431820 Methods and apparatus for cooling gas turbine engine blade tips |
| 08/13/2002 | US6431781 Ceramic to metal joint assembly |
| 08/13/2002 | US6430917 Single rotor turbine engine |
| 08/13/2002 | CA2252658C Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
| 08/08/2002 | US20020106279 Locking device |
| 08/08/2002 | US20020106275 Cooling of gas turbine engine aerofoils |
| 08/08/2002 | US20020104594 Intermetallic composite comprising: 19- 24 atomic percent titanium; 1-5 atomic percent hafnium; 16-22 atomic percent silicon; 7-14 atomic percent chromium; and a balance of niobium. |
| 08/08/2002 | US20020104317 Method of operation of gas turbine engine |
| 08/08/2002 | DE10102606A1 Kühlung von Gehäusen, Rotor, Schaufeln und/oder Brennern von Turbinen Cooling of housings, rotor blades and / or turbine burners |
| 08/07/2002 | EP1229214A2 Turbomachine blade-to-rotor sealing arrangement |
| 08/07/2002 | EP1229212A2 Locking device |
| 08/07/2002 | EP1229146A2 Oxidation resistant coatings for niobium-based silicide composites |
| 08/07/2002 | EP1228958A2 Method for reducing the noise emission of propellers |
| 08/07/2002 | EP1228293A1 Turbine blade and method for producing a turbine blade |
| 08/07/2002 | EP1227905A1 Multipiece core assembly for cast airfoil |
| 08/07/2002 | EP1015306A4 Ducted turbine |
| 08/07/2002 | EP0839284B1 Multi-stage rotary fluid handling apparatus |
| 08/06/2002 | US6428683 Comprises stripping tank containing an electrolyte bath for removing a coating from workpiece (air foil), rinse tank, and distillation unit for receiving electrolyte containing dissolved metals |
| 08/06/2002 | US6428602 Method for recovering platinum from platinum-containing coatings on gas turbine engine components |
| 08/06/2002 | US6428281 Turbine vane with enhanced profile |
| 08/06/2002 | US6428280 Structure with ceramic foam thermal barrier coating, and its preparation |
| 08/06/2002 | US6428279 Low windage loss, light weight closure bucket design and related method |
| 08/06/2002 | US6428278 Mistuned rotor blade array for passive flutter control |
| 08/06/2002 | US6428273 Truncated rib turbine nozzle |
| 08/06/2002 | US6428272 Bolted joint for rotor disks and method of reducing thermal gradients therein |
| 08/06/2002 | US6428271 Compressor endwall bleed system |
| 08/06/2002 | US6428270 Stage 3 bucket shank bypass holes and related method |
| 08/06/2002 | US6427752 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting |
| 08/06/2002 | US6427448 Gas turbine and method of cooling a turbine stage |
| 08/01/2002 | WO2002059484A1 Fan blade with accelerated twist angle |
| 08/01/2002 | WO2002059464A1 Fluid machinery |
| 08/01/2002 | WO2002044538A3 Device for centring a tube in a turbine shaft |
| 08/01/2002 | US20020100793 Method for repairing damaged areas in a metal component |
| 08/01/2002 | DE10047307A1 Dichtungsanordnung Seal assembly |
| 07/31/2002 | EP1227218A2 Turbine nozzle segment and method of repairing same |
| 07/31/2002 | EP1227217A2 Gas turbine |
| 07/31/2002 | EP1227164A2 Laser shock peening integrally bladed rotor blade edges |
| 07/31/2002 | CN1361308A Ionic TiALN coating for blade of air compressor in naval aircraft engine |
| 07/30/2002 | US6425736 Stator assembly for a rotary machine and method for making the stator assembly |
| 07/30/2002 | CA2250169C Cooled stationary blade of gas turbine |
| 07/30/2002 | CA2233821C Gas turbine cooled moving blade |
| 07/25/2002 | WO2002057599A1 Improved vane for variable nozzle turbocharger |
| 07/25/2002 | US20020098776 Method and device for treating the surface of a part |
| 07/25/2002 | US20020098294 Method of providing a protective coating on a metal substrate, and related articles |
| 07/25/2002 | US20020098083 Low-pressure steam turbine |
| 07/25/2002 | US20020098082 Gas turbine |
| 07/25/2002 | US20020098078 Device and method for cooling a platform of a turbine blade |
| 07/25/2002 | DE10101165A1 Befestigungsvorrichtung für ein radial durchströmtes Verdichterrad Fastening device for a radial compressor wheel throughflow |
| 07/24/2002 | EP1225322A1 Apparatus to centre a tube in a turbine shaft |
| 07/24/2002 | EP1225308A2 Split ring for gas turbine casing |
| 07/24/2002 | EP1225304A2 Nozzle fillet backside cooling |
| 07/24/2002 | EP1225303A2 Blade structure in a gas turbine |
| 07/23/2002 | US6423432 High temperature corrosion-resistant and abrasion-resistant coating member, and manufacturing method thereof |
| 07/23/2002 | US6422821 Method and apparatus for reducing turbine blade tip temperatures |
| 07/23/2002 | US6422820 Corner tang fan blade |
| 07/23/2002 | US6422819 Cooled airfoil for gas turbine engine and method of making the same |
| 07/23/2002 | US6422818 Lubricating system for thermal medium delivery parts in a gas turbine |
| 07/23/2002 | US6422817 Cooling circuit for and method of cooling a gas turbine bucket |
| 07/23/2002 | US6422812 Bolted joint for rotor disks and method of reducing thermal gradients therein |
| 07/23/2002 | US6422811 Cooling arrangement for blades of a gas turbine |
| 07/23/2002 | US6422810 Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles |
| 07/18/2002 | WO2002055844A1 Rotary nozzle turbine |
| 07/18/2002 | WO2002055754A2 Method and device for gas phase diffusion coating of metal components |
| 07/18/2002 | US20020094284 Vane for variable nozzle turbocharger |
| 07/18/2002 | US20020094276 Blade of a gas turbine |
| 07/18/2002 | US20020094272 Turbulated cooling holes |
| 07/18/2002 | US20020094270 Blade structure in a gas turbine |
| 07/18/2002 | US20020094268 Split ring for gas turbine casing |
| 07/18/2002 | US20020092165 Method for the manufacture of a welded rotor of a fluid-flow machine |
| 07/18/2002 | DE10100790A1 Nickel-Basislegierung für die gießtechnische Herstellung einkristallin erstarrter Bauteile Nickel-base alloy for casting-producing monocrystalline solidified components |
| 07/17/2002 | EP1223309A1 Redundant blade retention system |
| 07/17/2002 | EP1223308A2 Cooling of a turbo machine component |
| 07/17/2002 | EP1223307A2 Blade of a gas turbine |
| 07/17/2002 | EP1223229A1 Nickel based alloy for casting single crystal components |
| 07/17/2002 | EP1222367A1 Heat transfer promotion structure for internally convectively cooled airfoils |
| 07/17/2002 | EP1222366A1 Cast airfoil structure with openings which do not require plugging |
| 07/17/2002 | CN1359446A Component and method for producing a protective coating on a component |
| 07/17/2002 | CN1359445A Turbomachine blade |
| 07/16/2002 | US6420677 Laser machining cooling holes in gas turbine components |
| 07/16/2002 | US6419464 Vane for variable nozzle turbocharger |
| 07/16/2002 | US6419453 Steam turbine rotor shaft |
| 07/16/2002 | US6419452 Securing devices for blades for gas turbines |
| 07/16/2002 | US6419449 Cooled flow deflection apparatus for a fluid-flow machine which operates at high temperatures |
| 07/16/2002 | US6419447 Gas turbine equipment and turbine blade |
| 07/16/2002 | US6419446 Apparatus and method for inhibiting radial transfer of core gas flow within a core gas flow path of a gas turbine engine |
| 07/16/2002 | US6419445 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment |
| 07/16/2002 | US6418804 Fluid flow inspection and video recording system and method for turbine buckets |
| 07/16/2002 | US6418618 Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling |