| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
|---|
| 06/28/2001 | WO2001046576A1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method |
| 06/28/2001 | WO2001046564A1 Viscous drag impeller components incorporated into pumps, turbines and transmissions |
| 06/28/2001 | WO2001046563A1 Machine set |
| 06/28/2001 | WO2001046084A1 High temperature erosion resistant coating and material containing compacted hollow geometric shapes |
| 06/28/2001 | WO2001045877A2 Multi-wall core and process |
| 06/28/2001 | US20010005480 Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages |
| 06/28/2001 | DE19963349A1 Schaufel für Gasturbinen mit Drosselquerschnitt an Hinterkante Bucket for gas turbines with throttle cross section at the rear edge |
| 06/28/2001 | DE19963099A1 Gas turbine blade has cooling air hole in outer wall in region of flow stagnation zone in outer corner on outlet side of corresponding deflection region |
| 06/28/2001 | DE19962244A1 Kühlluft-Führungssystem im Hochdruck-Turbinenabschnitt eines Gasturbinen Triebwerkes Cooling air guide system in the high pressure turbine section of a gas turbine engine |
| 06/28/2001 | DE19960896A1 Retaining device for rotor blades of axial turbine engine, with recesses in outer circumference of retainer corresponding to sections of blade receivers |
| 06/28/2001 | DE19960895A1 Multi-stage axial turbine for turbine engine, with boiler in space between rotor disks which has input and output apertures for cooling air flow |
| 06/27/2001 | EP1111323A2 Article surface with metal wires and method for making |
| 06/27/2001 | EP1111193A2 Axial blade retention system for turbomachines |
| 06/27/2001 | EP1111192A1 Articles provided with corrosion resistant coatings |
| 06/27/2001 | EP1111191A2 Periodic stator airfoils |
| 06/27/2001 | EP1111190A1 Cooled turbine blade with slanted and chevron shaped turbulators |
| 06/27/2001 | EP1111189A2 Cooling air path for the rotor of a gas turbine engine |
| 06/27/2001 | EP1111188A2 Swept airfoil with barrel shaped leading edge |
| 06/27/2001 | EP1111091A1 Method of forming an active-element containing aluminide as stand alone coating and as bond coat and coated article |
| 06/27/2001 | EP1111085A1 Method for producing ceramic coatings |
| 06/26/2001 | US6251526 Coated cast part |
| 06/26/2001 | US6251504 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 06/26/2001 | US6251315 Method for disposing a laser blocking material on the interior of an airfoil |
| 06/26/2001 | US6250883 Integral ceramic blisk assembly |
| 06/26/2001 | US6250878 Method and assembly for connecting air ducts in gas turbine engines |
| 06/26/2001 | CA2229324C Gas turbine tip shroud blade cavity |
| 06/21/2001 | WO2001044623A1 Axial flow turbine type rotor machine for elastic fluid operation |
| 06/21/2001 | WO2001043912A1 Method for producing an opening in a metallic structural part |
| 06/21/2001 | US20010004475 Improving durability of turbine blade composed of a superalloy material and defining an airfoil by applying corrosion resistant overlay coating to underside of platform and blade neck |
| 06/21/2001 | US20010004474 Methods of providing article with corrosion resistant coating and coated article |
| 06/21/2001 | DE19961565A1 Coolant flow at a turbine paddle is adjusted by an inserted body into an opening in the coolant channel which reduces its cross section to give the required coolant flow vol |
| 06/21/2001 | DE10052176A1 Dampfturbinenrotor und Verfahren zur Herstellung desselben Steam turbine rotor and method of manufacturing the same |
| 06/21/2001 | CA2394132A1 Axial flow turbine type rotor machine for elastic fluid operation |
| 06/20/2001 | EP1108856A2 Turbine nozzle with sloped film cooling |
| 06/20/2001 | EP1107867A1 Removal of thermal barrier coatings |
| 06/20/2001 | EP0935703B1 Cooling passages for airfoil leading edge |
| 06/19/2001 | US6247897 Vane system |
| 06/19/2001 | US6247896 Method and apparatus for cooling an airfoil |
| 06/19/2001 | US6247895 Locking member for processing a flow directing assembly |
| 06/19/2001 | US6247893 Hydraulic turbine for enhancing the level of dissolved gas in water |
| 06/19/2001 | US6247892 Continuous flow rotary pump |
| 06/14/2001 | WO2001042654A1 Turbocharger with design for improved mechanical performance |
| 06/14/2001 | WO2001012954A3 Turbine or system with internal evaporative blade cooling |
| 06/14/2001 | US20010003631 Method for sealing a porous layer at the surface of a body, in particular for the sealing of a thermal spray layer |
| 06/13/2001 | EP1106836A2 Double bowed compressor airfoil |
| 06/13/2001 | EP1106835A2 Bowed compressor airfoil |
| 06/13/2001 | EP1106787A2 Turbine nozzle segment band cooling |
| 06/13/2001 | EP1106783A2 Method to produce a turbomachine blade |
| 06/13/2001 | EP1106782A2 Cooled airfoil for gas turbine engine and method of making the same |
| 06/13/2001 | EP1106781A1 Coolable vane or blade for a turbomachine |
| 06/13/2001 | EP1106780A2 Turbine rotor torque transmission |
| 06/13/2001 | EP1106280A1 Core to control turbine bucket wall thickness and method |
| 06/13/2001 | EP1105243A1 Turbine rotor modernization and repair method |
| 06/13/2001 | DE19959598A1 Verfahren zum Herstellen einer Schaufel einer Strömungsmaschine A method of manufacturing a blade of a turbomachine |
| 06/13/2001 | DE19957718C1 Schaufel mit optimiertem Schwingungsverhalten Blade with optimized vibration behavior |
| 06/13/2001 | CN1299003A Double bending booster blades |
| 06/13/2001 | CA2325218A1 Method for sealing a porous layer at the surface of a body, in particular for the sealing of a thermal spray layer |
| 06/12/2001 | US6244822 Precision crowning of blade attachments in gas turbines |
| 06/12/2001 | US6244817 Method and apparatus for a fan noise controller |
| 06/12/2001 | US6244492 Cover for a component surface |
| 06/12/2001 | US6244327 Method of making single-cast, high-temperature thin wall structures having a high thermal conductivity member connecting the walls |
| 06/12/2001 | US6243948 Modification and repair of film cooling holes in gas turbine engine components |
| 06/12/2001 | CA2009595C Consolidated member and method and preform for making |
| 06/09/2001 | CA2327203A1 Cooled airfoil for gas turbine engine and method of making the same |
| 06/07/2001 | WO2001040660A2 Centrifugal impeller assembly |
| 06/07/2001 | WO2001040631A1 Shear pin with locking cam |
| 06/07/2001 | WO2001040548A1 Chemical cleaning solution for gas turbine blades |
| 06/07/2001 | US20010002667 Post-cast EDM method for reducing the thickness of a turbine nozzle wall |
| 06/07/2001 | DE19957771A1 Repair of honeycomb sealing elements on turbine discs involves applying suitable molten metal alloy to already reassembled sealing bridge using laser beam directed at sealing element |
| 06/07/2001 | DE19957225A1 Cooling-air conduction system, esp. for high-pressure turbine section of gas-turbine engine or power unit, has part of the air flowing past the gas-turbine combustion chamber conducted radially at the height of the second pre-spin chamber |
| 06/07/2001 | DE19956444A1 Leichtbauteil in Verbundweise Lightweight component in composite manner |
| 06/05/2001 | US6242715 Progressive hot twisting apparatus for use in a process for manufacturing a hollow turbomachine blade |
| 06/05/2001 | US6242109 High-temperature-resistant component and method of providing protection thereof against oxidation |
| 06/05/2001 | US6241471 Turbine bucket tip shroud reinforcement |
| 06/05/2001 | US6241469 Turbine blade |
| 06/05/2001 | US6241468 Coolant passages for gas turbine components |
| 06/05/2001 | US6241467 Stator vane for a rotary machine |
| 06/05/2001 | US6241466 Turbine airfoil breakout cooling |
| 06/05/2001 | US6241000 Method for removing cores from castings |
| 05/31/2001 | WO2001038707A1 Gas turbine equipment, gas turbine sealing device, and gas turbine cooling air leakage suppressing method |
| 05/31/2001 | WO2001038698A1 Lightweight structural component having a sandwich structure |
| 05/31/2001 | WO2001038697A1 A single or multi-bladed rotor |
| 05/31/2001 | WO2000068461A3 Thermal barrier coating |
| 05/31/2001 | US20010002235 Blade with optimized vibration behavior |
| 05/31/2001 | US20010001897 Method of forming hollow channels within a component |
| 05/30/2001 | EP1103628A2 A coating system for providing environmental protection to a metal substrate |
| 05/30/2001 | EP1102918A1 Gas turbine steam cooled vane |
| 05/30/2001 | EP0815423B1 Method of balancing a bladed rotor |
| 05/29/2001 | US6238743 Removal yttria-stabilized zirconia layer on gas turbine engine; using aqueous solution of ammonium bifluoride |
| 05/29/2001 | US6238187 Method using laser shock peening to process airfoil weld repairs pertaining to blade cut and weld techniques |
| 05/29/2001 | US6238186 Method of manufacturing a blade for fluid machinery |
| 05/29/2001 | US6238183 Cooling systems for gas turbine engine airfoil |
| 05/29/2001 | US6238182 Joint for a turbine component |
| 05/29/2001 | US6237344 Dimpled impingement baffle |
| 05/29/2001 | CA2229317C Cooling medium path structure for gas turbine blade |
| 05/25/2001 | WO2001036792A1 Turbine blade and method for production thereof |
| 05/25/2001 | WO2001036791A1 Turbine blade and method for production thereof |
| 05/25/2001 | WO2001036790A1 Turbine blade and method for producing a turbine blade |
| 05/23/2001 | EP1101901A1 Turbine blade and method of manufacture for the same |
| 05/23/2001 | EP1101900A1 Turbine blade and method of manufacture for the same |