| 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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| 06/16/2004 | EP1137866B1 Impeller containment system |
| 06/15/2004 | US6749942 Durable refractory ceramic coating |
| 06/15/2004 | US6749518 Inertia welded shaft and method therefor |
| 06/15/2004 | US6749400 Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots |
| 06/15/2004 | US6749396 Failsafe film cooled wall |
| 06/10/2004 | WO2004048775A2 Method and apparatus for determining the thermal performance of actively cooled turbine components |
| 06/10/2004 | US20040110021 High velocity spraying; deformation ,adhesion to target; alloy of Group 4 and Group 5 metrals and lubricant |
| 06/10/2004 | US20040109786 Nickel-base superalloy composition and its use in single-crystal articles |
| 06/10/2004 | US20040109767 Metallic article with integral end band under compression |
| 06/10/2004 | US20040109766 Bucket dovetail design for turbine rotors |
| 06/10/2004 | US20040109765 Turbine blade |
| 06/10/2004 | US20040109764 Turbine, in particular a gas turbine, and a blade |
| 06/10/2004 | US20040109763 Method of producing and assembling a cooling device inside an axial-flow gas turbine blade, and axial-flow gas turbine blade produced using such a method |
| 06/10/2004 | US20040109754 Blade cooling |
| 06/10/2004 | US20040107554 Spreader for separating turbine buckets on wheel |
| 06/09/2004 | EP1426556A2 Gas turbine bucket dovetail design for turbine rotors |
| 06/09/2004 | EP1426555A2 Method and apparatus for reducing flow across compressor airfoil tips |
| 06/09/2004 | EP1426554A1 Blade cooling |
| 06/09/2004 | EP1426553A1 Weight reduction of rotor blades |
| 06/09/2004 | EP1426457A2 Nickel-base superalloy composition and its use in single-crystal articles |
| 06/09/2004 | EP1426142A1 Device for defining a designated flow path through a dovetail slot in a gas turbine engine disk |
| 06/09/2004 | EP1426141A1 Method and apparatus for removing a predetermined amount of material from a bottom portion of a dovetail slot in gas turbine engine disk |
| 06/09/2004 | DE10355449A1 Turbinenschaufel Turbine blade |
| 06/09/2004 | DE10255346A1 Verfahren zum Herstellen einer Turbinenschaufel A method of manufacturing a turbine blade |
| 06/09/2004 | CN2620090Y Steam turbine rotor reaction type T type blade root vane circumference expansion device |
| 06/09/2004 | CN1502788A 涡轮叶片和燃气轮机 Turbine blades and turbine |
| 06/08/2004 | US6746783 High-temperature articles and method for making |
| 06/08/2004 | US6746755 Ceramic matrix composite structure having integral cooling passages and method of manufacture |
| 06/08/2004 | US6746209 Methods and apparatus for cooling gas turbine engine nozzle assemblies |
| 06/08/2004 | US6746208 Closed circuit blade-cooled turbine |
| 06/08/2004 | US6746204 Turbine rotor |
| 06/08/2004 | US6745622 Apparatus and method for inspecting dovetail slot width for gas turbine engine disk |
| 06/03/2004 | WO2004046560A1 Method of repairing turbine blade |
| 06/03/2004 | WO2004046522A2 Miniature gas turbine engine with unitary rotor shaft for power generation |
| 06/03/2004 | WO2004046414A2 Method of forming a vibration damping coating on a metallic substrate |
| 06/03/2004 | WO2004045844A1 Layer system |
| 06/03/2004 | WO2004004953A3 Diffusion bond mixture for healing single crystal alloys |
| 06/03/2004 | US20040106365 Device for defining a designated flow path through a dovetail slot in a gas turbine engine disk |
| 06/03/2004 | US20040106359 Method and apparatus for removing a predetermined amount of material from a bottom portion of a dovetail slot in gas turbine engine disk |
| 06/03/2004 | US20040106000 Cobalt-based alloy for the coating of organs subject to erosion by liquid |
| 06/03/2004 | US20040105756 Mixed flow turbine and mixed flow turbine rotor blade |
| 06/03/2004 | US20040105732 Method and apparatus for producing forked roots of turbine blades |
| 06/03/2004 | DE10255009A1 Schwingungsdämpfungsvorrichtung sowie Verfahren zur Schwingungsdämpfung zur aktiven Dämpfung von Schwingungen eines Bauteils A vibration damping device as well as procedures for vibration damping for the active damping of vibrations of a component |
| 06/03/2004 | DE10206447B4 Verfahren und Vorrichtung zum Halten eines zu verbindenden, metallischen Bauteils und Verfahren zum Verbinden eines metallischen Bauteils mit einem weiteren Bauteil Method and apparatus for holding a to be connected, the metallic component and method of joining a metallic member to a further component |
| 06/02/2004 | EP1424468A2 Gas turbine blade cooling arrangement |
| 06/02/2004 | EP1424467A2 Row of long and short chord length turbine airfoils |
| 06/02/2004 | EP1424466A2 Production method of a turbine blade |
| 06/02/2004 | EP1424465A1 HYBRID ROTOR, METHOD OF MANUFACTURING THE HYBRID ROTOR, AND GAS TURBINE |
| 06/02/2004 | EP1424158A1 A method for fabricating, modifying or repairing of single crystal or directionally solidified articles |
| 06/02/2004 | EP1423230A1 A method for manufacturing a hollow blade for a stator or rotor component |
| 06/02/2004 | EP1250516A4 Turbine engine damper |
| 06/02/2004 | EP1204776B1 High-temperature part and method for producing the same |
| 06/02/2004 | CN1500971A Composite tubular woven seal for steam turbine diaphragm horizontal joint interfaces |
| 06/02/2004 | CN1500970A Turbine nozzle retention apparatus at the carrier horizontal joint face |
| 06/02/2004 | CN1500969A Method and apparatus for reducing flow across compressor airfoil tips |
| 06/02/2004 | CN1500917A The electrical process for the simultaneous stripping of diverse coatings from a metal substrate |
| 06/01/2004 | US6743350 Apparatus and method for rejuvenating cooling passages within a turbine airfoil |
| 06/01/2004 | US6742991 Turbine blade and gas turbine |
| 06/01/2004 | US6742989 Structures of turbine scroll and blades |
| 06/01/2004 | US6742988 Composite tubular woven seal for steam turbine diaphragm horizontal joint interfaces |
| 06/01/2004 | US6742984 Divided insert for steam cooled nozzles and method for supporting and separating divided insert |
| 06/01/2004 | US6742698 Refractory metal backing material for weld repair |
| 05/27/2004 | WO2004044387A1 Slotted guide vane |
| 05/27/2004 | WO2004044384A2 A dual-use radial turbomachine |
| 05/27/2004 | WO2004043691A1 Extremely strain tolerant thermal protection coating and related method and apparatus thereof |
| 05/27/2004 | US20040102309 Thermal insulating material and method of producing same |
| 05/27/2004 | US20040101433 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof |
| 05/27/2004 | US20040101410 Axial flow fluid machine |
| 05/27/2004 | US20040101407 Fan assembly and method |
| 05/27/2004 | US20040101406 Fan with collapsible blades, redundant fan system, and related method |
| 05/27/2004 | US20040101405 Row of long and short chord length and high and low temperature capability turbine airfoils |
| 05/27/2004 | US20040101402 Turbine |
| 05/27/2004 | DE10350230A1 Als Diffusor wirkende Kupplungsabdeckung für axial gekuppelte Turbinen As a diffuser acting clutch cover for axially coupled turbines |
| 05/27/2004 | DE10304529B3 Axial steam or gas turbine for energy plant has ring fitted around radial outer ends of turbine blades for damping blade vibration |
| 05/26/2004 | EP1422440A1 Device and method for active control of vibrations of an element |
| 05/26/2004 | EP1422402A1 Method of closing working hole in gas turbine blade top |
| 05/26/2004 | EP1422383A2 Gas turbine blade cooling |
| 05/26/2004 | EP1422382A1 Axial flow turbine |
| 05/26/2004 | EP1422381A2 Method of repairing a turbine nozzle segment, and turbine nozzle segment |
| 05/26/2004 | EP1422380A2 Method and system for automated repair design of damaged blades of a compressor or turbine |
| 05/26/2004 | EP1422379A2 Systems and methods for automated sensing and machining for repairing turbine blades |
| 05/26/2004 | EP1422054A1 Layered structure for use in gas turbines |
| 05/26/2004 | EP1421258A1 Blade for a turbine engine and method for production of said blade |
| 05/26/2004 | EP1421257A1 Double flow compressor |
| 05/26/2004 | CN1499044A Flow passage sealing of turbine and streamline structure thereof |
| 05/26/2004 | CN1499043A Continuous radial loader for steam turbine reaction blade and its method |
| 05/26/2004 | CN1499042A 涡轮机 Turbines |
| 05/25/2004 | US6740364 Method of depositing a compositionally-graded coating system |
| 05/25/2004 | US6740292 Improved castability and resistance to oxidation, especially at high temperatures; large gas turbine single crystal components |
| 05/25/2004 | US6739839 First-stage high pressure turbine bucket airfoil |
| 05/25/2004 | US6739838 Airfoil shape for a turbine bucket |
| 05/25/2004 | US6739837 Bladed rotor with a tiered blade to hub interface |
| 05/25/2004 | US6739836 Connection of blades on a rotor disc of a gas turbine |
| 05/25/2004 | US6739594 Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint |
| 05/25/2004 | US6739381 Method of producing a turbine blade |
| 05/25/2004 | US6739120 Counterrotatable booster compressor assembly for a gas turbine engine |
| 05/25/2004 | CA2186562C Process for the fabrication of a turbine engine hollow vane |
| 05/21/2004 | WO2004042199A2 Turbo engine |
| 05/21/2004 | WO2004042198A2 Self-regulating turbine |
| 05/21/2004 | WO2002103074A8 Thermal barrier coating material and method for production thereof, gas turbine member using the thermal barrier coating material, and gas turbine |