Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
---|
06/21/2000 | DE19858913A1 High temperature fretting protective layer, especially for vane foot-disk groove regions of titanium alloy gas turbine engine guide vanes, consists of a copper-aluminum alloy containing chromium and optionally iron |
06/20/2000 | US6077615 Gas turbine nozzle, power generation gas turbine, co-base alloy and welding material |
06/20/2000 | US6077036 Bowed nozzle vane with selective TBC |
06/20/2000 | US6077035 Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine |
06/20/2000 | US6077034 Blade cooling air supplying system of gas turbine |
06/20/2000 | US6077002 Step milling process |
06/15/2000 | WO2000034651A1 Reduction in the noise produced by a rotor blade of a wind turbine |
06/15/2000 | WO2000034628A1 Impeller containment system |
06/15/2000 | WO2000021746A8 Method for obtaining thin, light and rigid metal parts |
06/15/2000 | DE19857554A1 Verbindungsanordnung zweier Laufscheiben einer Axial-Strömungsmaschine Connection arrangement of two pulleys of an axial-flow machine |
06/14/2000 | EP1008727A2 Cooling in gas turbines |
06/14/2000 | EP1008724A2 Airfoil cooling configuration |
06/14/2000 | EP1008723A1 Platform cooling in turbomachines |
06/14/2000 | EP1008722A1 Method for manufacturing a welded turbomachine rotor |
06/14/2000 | EP1008672A1 Platinum modified diffusion aluminide bond coat for a thermal barrier coating system |
06/14/2000 | EP1007823A1 Hydrogen fueled power plant |
06/14/2000 | EP1007271A1 Gas turbine vane and method for producing a gas turbine vane |
06/13/2000 | US6074706 Adhesion of a ceramic layer deposited on an article by casting features in the article surface |
06/13/2000 | US6074169 High and low pressure sides-integrating steam turbine, long blades thereof and combined cycle power generation system |
06/13/2000 | CA2036904C Gas turbine blades |
06/08/2000 | WO2000032331A1 Multipiece core assembly |
06/08/2000 | DE19856199A1 Kühlung in Gasturbinen Cooling in gas turbines |
06/07/2000 | EP1006263A1 Vane cooling |
06/07/2000 | EP1006262A1 Cooling method and apparatus for rotor vanes of a thermodynamic engine |
06/07/2000 | EP1006261A2 Gas turbine plant |
06/07/2000 | CN1255581A Cooling for vane |
06/06/2000 | US6071627 Heat resistant alloy with ceramic coating layer |
06/06/2000 | US6071556 Method of coating an article of manufacturing having a substrate formed of a nickel or cobalt-based superalloy |
06/06/2000 | US6071363 Single-cast, high-temperature, thin wall structures and methods of making the same |
06/06/2000 | US6071077 Swept fan blade |
06/06/2000 | US6071075 Cooling structure to cool platform for drive blades of gas turbine |
06/06/2000 | US6070404 Gaseous fuel compression and control method |
06/02/2000 | WO2000031379A1 Ceiling fan assembly and method of assembling same |
06/02/2000 | WO2000031378A1 Turbine blade to disk retention device |
05/31/2000 | EP1004749A2 Damper for rotating machinery |
05/31/2000 | EP1004748A2 Rotor for a turbomachine |
05/31/2000 | EP1004686A2 High temperature vapor coating container |
05/31/2000 | EP0670956B1 Gas turbine blade damper |
05/31/2000 | DE19854908A1 Schaufel und Laufscheibe einer Strömungsmaschine Blade and rotor disk of a turbomachine |
05/31/2000 | DE19854907A1 Cooling air conduction for high pressure axial aviation gas turbines with air flow guided through radial turbine, turbine plate, through ring gap, towards hub cob for cooling |
05/31/2000 | DE19831736C2 Verfahren zur Reparatur und Herstellung eines integral beschaufelten Rotors für eine Strömungsmaschine Method for repairing and manufacturing an integrally bladed rotor for a turbomachine |
05/30/2000 | US6068806 Method of configuring a ceramic core for casting a turbine blade |
05/30/2000 | US6068445 Cooling system for the leading-edge region of a hollow gas-turbine blade |
05/30/2000 | US6068443 Gas turbine tip shroud blade cavity |
05/25/2000 | WO2000029721A1 Turbo-machine, especially a turbo-generator comprising a turbo-machine and an electric machine |
05/25/2000 | WO2000029634A1 Heat-insulating glass-metal/ceramic layers |
05/25/2000 | WO2000029352A2 Method for joining ceramic to metal |
05/25/2000 | WO2000029171A1 System for the precision machining of rotationally symmetrical components |
05/24/2000 | EP1002935A1 TiAl-rotor of a turbomachine and method of manufacturing |
05/24/2000 | EP1002619A2 Fixture for disposing a laser blocking material in an airfoill |
05/24/2000 | EP1002618A2 Method for disposing a laser blocking material on the interior of an airfoil |
05/24/2000 | EP1002617A2 Tool for disposing laser blocking material in an airfoil |
05/24/2000 | EP1002616A2 Method and material for processing a component for laser machining |
05/24/2000 | EP1002615A2 Method for orienting an airfoil for processing and forming a mask for the airfoil |
05/24/2000 | EP1002141A1 Component with high temperature resistance and method for producing an anti-oxidation element |
05/24/2000 | CN1253878A Thermal resistance coating system and its material |
05/23/2000 | US6065938 Rotor for a turbomachine having blades to be fitted into slots, and blade for a rotor |
05/23/2000 | US6065932 Turbine |
05/23/2000 | US6065931 Gas turbine moving blade |
05/23/2000 | US6065928 Turbine nozzle having purge air circuit |
05/23/2000 | CA2196481C Steam turbine |
05/18/2000 | WO2000027570A1 Method for making self-brazing components using powder metallurgy |
05/18/2000 | DE19852604A1 Rotor for gas turbine, with first cooling air diverting device having several radial borings running inwards through first rotor disk |
05/17/2000 | EP1001137A2 Axial serpentine cooled airfoil |
05/17/2000 | EP1001136A2 Airfoil isolated leading edge cooling |
05/17/2000 | EP1001135A2 Airfoil with serial impingement cooling |
05/17/2000 | EP1001046A1 High temperature corrosion-resistant and abrasion-resistant coating member, and manufacturing method thereof |
05/17/2000 | EP1000698A1 Cooled components with conical cooling passages |
05/17/2000 | EP1000225A1 Turbine blade and a method for the production thereof |
05/17/2000 | EP1000224A1 Distribution of cooling air in a turbine stage of a gas turbine |
05/17/2000 | CN1253230A Axial flow turbine |
05/16/2000 | US6063435 Vapor deposition; heating; rotation |
05/16/2000 | US6062817 Apparatus and methods for cooling slot step elimination |
05/16/2000 | US6062811 On-line monitor for detecting excessive temperatures of critical components of a turbine |
05/16/2000 | US6062018 Pulse detonation electrical power generation apparatus with water injection |
05/16/2000 | US6061886 Turbine blade fitting apparatus and fitting method |
05/11/2000 | WO2000025959A1 Single crystal vane segment and method of manufacture |
05/11/2000 | DE19850732A1 Axialturbine Axial flow turbine |
05/10/2000 | EP0999349A2 Axial turbine |
05/10/2000 | EP0999009A1 Method of applying wear-resistant materials to turbine blades, and turbine blades having wear-resistant materials |
05/10/2000 | EP0999008A2 Method of laser drilling an airfoil |
05/10/2000 | EP0998361A1 Turbine blade and method for producing a turbine blade |
05/10/2000 | CN1052266C Steam turbine power plant and steam turbine |
05/09/2000 | US6060174 Composite comprising a substrate and a layer of a basecoat of iron, cobalt and/or nickel and chromium, aluminum and yttrium where it contains boron in a concentration gradient; high density; quality |
05/09/2000 | US6059533 Damped blade having a single coating of vibration-damping material |
05/09/2000 | US6059530 Twin rib turbine blade |
05/09/2000 | US6059529 Turbine blade assembly with cooling air handling device |
05/04/2000 | WO2000025005A1 Product with a heat insulating layer and method for the production of a heat insulating layer |
05/04/2000 | WO2000010765B1 Turbine rotor modernization and repair method |
05/03/2000 | EP0997612A2 Bladed ducting for turbomachinery |
05/03/2000 | EP0997555A1 Process for producing a thin ceramic coating on a metallic substrate |
05/02/2000 | US6057047 Porous ceramic material of at least 10 layers where at least three layers have 20% by volume porosity and at least one other layer has less than 5% by vol. porosity; thermal barrier; coated gas turbine engine components |
05/02/2000 | US6056508 Cooling system for the trailing edge region of a hollow gas turbine blade |
05/02/2000 | US6056507 Article with brazed end plate within an open body end |
05/02/2000 | US6056505 Cooling circuits for trailing edge cavities in airfoils |
05/02/2000 | US6056204 Synthetic jet actuators for mixing applications |
05/02/2000 | US6055805 Active rotor stage vibration control |
05/02/2000 | CA2209851C Gas turbine blade |
05/02/2000 | CA2157091C Turbocharger turbine wheel and shaft assembly |
05/02/2000 | CA2011414C Turbine blade repair |