| 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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| 11/26/2002 | US6485590 Method of forming a multilayer ceramic coating |
| 11/26/2002 | US6485262 Methods and apparatus for extending gas turbine engine airfoils useful life |
| 11/26/2002 | US6485255 Cooling air flow control device for a gas turbine engine |
| 11/24/2002 | WO2002103206A1 Low noise fan stationary blade |
| 11/23/2002 | CA2373591A1 A process for applying a heat shielding coating system on a metallic substrate |
| 11/21/2002 | WO2002092980A1 Surface-reformed exhaust gas guide assembly of vgs type turbo charger, and method of surface-reforming component member thereof |
| 11/21/2002 | WO2002092979A1 Exhaust guide assembly for vgs type turbo charger improved in heat resistance and method of producing heat-resisting members applicable thereto, and method of producing raw material for variable vanes applicable thereto |
| 11/21/2002 | WO2002092970A1 Inner platform impingement cooling by supply air from outside |
| 11/21/2002 | WO2002092969A1 Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure |
| 11/21/2002 | WO2002092874A1 Member coated with thermal barrier coating film and thermal spraying powder |
| 11/21/2002 | US20020172838 For use in gas turbine engines |
| 11/21/2002 | US20020172808 Gas turbine airfoil protected by aluminide and platinum aluminide coatings, and its preparation |
| 11/21/2002 | US20020172596 Film cooled article with improved temperature tolerance |
| 11/21/2002 | US20020172595 Steam turbine |
| 11/21/2002 | US20020172594 Turbine blade and turbine |
| 11/21/2002 | US20020172591 Turbine cooling circuit |
| 11/21/2002 | US20020172590 Inner platform impingement cooling by supply air from outside |
| 11/21/2002 | US20020172587 Method for welding together two parts which are exposed to different temperatures, and turbomachine produced using a method of this type |
| 11/21/2002 | US20020170176 Turbine airfoil process sequencing for optimized tip performance |
| 11/21/2002 | DE10217040A1 Keramischer Kern sowie Verfahren und Vorrichtung zum Herstellen desselben Of the same ceramic core as well as methods and apparatus for producing |
| 11/21/2002 | DE10124398A1 Applying a ceramic layer to a metallic base body comprises joining a metallic intermediate support having recesses with the base body, and subsequently applying the ceramic layer on the intermediate support |
| 11/20/2002 | EP1258598A2 Turbine airfoil tip |
| 11/20/2002 | EP1258597A2 Gas turbine engine blade |
| 11/20/2002 | EP1258545A1 Method for isothermal brazing of single crystal components |
| 11/20/2002 | EP1258312A2 Repair of a single crystal nickel based superalloy article |
| 11/20/2002 | EP1257732A1 Moving turbine blade |
| 11/20/2002 | EP1257680A1 Iron base high temperature alloy |
| 11/20/2002 | EP1257373A1 Device and method for casting a workpiece and workpiece |
| 11/20/2002 | EP1107867A4 Removal of thermal barrier coatings |
| 11/20/2002 | EP0873466B1 Turbine shaft of a steam turbine with internal cooling |
| 11/20/2002 | CN1380487A 燃气轮机 Gas turbine |
| 11/20/2002 | CN1380486A Method for manufacturing turbine blade and turbine blade |
| 11/19/2002 | US6483211 Turbine rotor sub-slot scoops |
| 11/19/2002 | US6482533 Article having imbedded cavity |
| 11/19/2002 | US6481972 Turbine bucket natural frequency tuning rib |
| 11/19/2002 | US6481971 Blade spacer |
| 11/19/2002 | US6481969 Apparatus and methods for balancing turbine rotors |
| 11/19/2002 | US6481967 Gas turbine moving blade |
| 11/19/2002 | US6481966 Blade for gas turbines with choke cross section at the trailing edge |
| 11/19/2002 | US6481959 Gas turbine disk cavity ingestion inhibitor |
| 11/19/2002 | US6481917 Tie-boltless shaft lock-up mechanism |
| 11/19/2002 | CA2269889C Jet engine booster structure |
| 11/19/2002 | CA2199691C Method for affixing an addition to a localized zone of a part using a superalloy |
| 11/14/2002 | WO2002090039A1 Method of repairing a turbin blade tip |
| 11/14/2002 | US20020168537 Article having turbulation and method of providing turbulation on an article |
| 11/14/2002 | US20020168264 Apparatus and process for impingement cooling of a component exposed to heat in a flow power machine |
| 11/14/2002 | US20020166231 Method for applying diffusion aluminide coating on a selective area of a turbine engine component |
| 11/13/2002 | EP1256696A2 Axial turbine with a variable-geometry stator |
| 11/13/2002 | EP1256635A1 Method for applying diffusion aluminide coating on a selective area of a turbine engine component |
| 11/13/2002 | EP1214172A4 Laser cladding a turbine engine vane platform |
| 11/13/2002 | EP1212167A4 Method for replacing a turbine vane airfoil |
| 11/13/2002 | CN1379170A Combustion turbine |
| 11/13/2002 | CN1379165A Turbine propeller and turbine engine |
| 11/13/2002 | CN1378890A Method for making turbine vanes |
| 11/13/2002 | CN1094173C 水轮机涡轮及配有这种涡轮的皮尔顿式水轮机 Turbine and Turbine with this turbine Pier Dun turbines |
| 11/12/2002 | US6478545 Fluted blisk |
| 11/12/2002 | US6478544 Blade arrangement with damping elements |
| 11/12/2002 | US6478540 Bucket platform cooling scheme and related method |
| 11/12/2002 | US6478539 Blade structure for a gas turbine engine |
| 11/12/2002 | US6478537 Pre-segmented squealer tip for turbine blades |
| 11/12/2002 | US6478535 Thin wall cooling system |
| 11/12/2002 | US6477916 Methods of installing a balance weight for a rotary component in turbomachinery |
| 11/12/2002 | US6477773 Methods for disassembling, replacing and assembling parts of a steam cooling system for a gas turbine |
| 11/11/2002 | CA2385840A1 Stator of a variable-geometry axial turbine for aeronautical applications |
| 11/08/2002 | CA2383468A1 Method for applying diffusion aluminide coating on a selective area of a turbine engine component |
| 11/07/2002 | US20020164430 Plasma spraying; evaporation; overcoating gas turbine blades |
| 11/07/2002 | US20020164417 Method of repairing a ceramic coating |
| 11/07/2002 | US20020164253 Apparatus for passive damping of flexural blade vibration in turbo-machinery |
| 11/07/2002 | US20020164250 Thin wall cooling system |
| 11/07/2002 | US20020164248 Hollow nozzle partition with recessed end caps |
| 11/07/2002 | US20020164247 Turbomachine with double-faced rotor-shroud seal structure |
| 11/07/2002 | US20020162220 Method of repairing a turbine blade tip |
| 11/07/2002 | DE10121390A1 Exhaust gas turbocharger for internal combustion engine, has shroud ring on turbine wheel around blades, and tunnel-like flow path is formed between adjacent turbine blades |
| 11/06/2002 | EP1254967A1 Improved plasma sprayed thermal bond coat system |
| 11/06/2002 | EP1254738A2 Automated system for repairing components |
| 11/06/2002 | EP1254332A1 Valve, in particular pressure reducing valve |
| 11/06/2002 | EP1254301A2 Turbine blade arrangement |
| 11/06/2002 | CN1378035A Turbine blade and method for producing turbine blade |
| 11/05/2002 | USRE37900 Blade group with pinned root |
| 11/05/2002 | US6475642 Oxidation-resistant coatings, and related articles and processes |
| 11/05/2002 | US6475289 Cleaning of internal passages of airfoils |
| 11/05/2002 | US6474948 Third-stage turbine bucket airfoil |
| 11/05/2002 | US6474947 Film cooling hole construction in gas turbine moving-vanes |
| 11/05/2002 | US6474946 Attachment air inlet configuration for highly loaded single crystal turbine blades |
| 11/05/2002 | US6474944 Hollow nozzle partition with recessed end caps |
| 11/05/2002 | US6474942 Airfoil configured for moisture removal from steam turbine flow path |
| 11/05/2002 | CA2229915C Gas turbine stationary blade |
| 10/31/2002 | WO2002086292A1 Turbine or compressor device and method for assembling the device |
| 10/31/2002 | WO2002086291A1 Blade for a turbine comprising a cooling air deflector |
| 10/31/2002 | WO2002048525A3 System to feed cooling air into a gas turbine rotor |
| 10/31/2002 | US20020161483 Automated system for repairing components |
| 10/31/2002 | US20020159889 Turbine blade having a cooled tip shroud |
| 10/31/2002 | US20020159888 Methods and systems for cooling gas turbine engine airfoils |
| 10/31/2002 | US20020159886 Axial-flow turbine having stepped portion formed in axial-flow turbine passage |
| 10/31/2002 | US20020159882 Methods and apparatus for damping rotor assembly vibrations |
| 10/31/2002 | US20020159880 Gas turbine disk cavity ingestion inhibitor |
| 10/31/2002 | US20020157738 A high-temperature component made of a nickel super-alloy consists of in wt %: 11-13% of Chromium, 3-5% of tungsten, 0.5- 2.5% of molybdenum, 3-5% aluminum, 3-5% of titanium , 3-7% of tantalum, 1-5% Re, reminder Nickel |
| 10/31/2002 | US20020157737 Nickel diffusion braze alloy and method for repair of superalloys |
| 10/31/2002 | US20020157251 Method of producing a turbine blade |
| 10/31/2002 | US20020157250 Turbine blade and turbine |