Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2002
05/08/2002EP1203104A2 Superalloys with improved weldability for high temperature applications
05/08/2002DE10053356A1 Gekühltes Bauteil, Gusskern für die Herstellung eines solchen Bauteils, sowie Verfahren zum Herstellen eines solchen Bauteils Cooled component, casting core for the production of such a component, and methods of making such a component
05/07/2002US6383602 Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture
05/07/2002US6383570 Thermal barrier coating system utilizing localized bond coat and article having the same
05/07/2002US6382920 Article with thermal barrier coating and method of producing a thermal barrier coating
05/07/2002US6382914 Cooling medium transfer passageways in radial cooled turbine blades
05/07/2002US6382913 Method and apparatus for reducing turbine blade tip region temperatures
05/07/2002US6382908 Nozzle fillet backside cooling
05/07/2002US6382907 Component for a gas turbine
05/07/2002US6382906 Floating spoolie cup impingement baffle
05/07/2002US6382903 Rotor bore and turbine rotor wheel/spacer heat exchange flow circuit
05/07/2002US6381945 Fuel preheating in a gas turbine
05/03/2002CA2359291A1 Turbine blade for gas turbine engine and method of cooling same
05/03/2002CA2359288A1 Turbine blade for gas turbine engine and method of cooling same
05/02/2002US20020051706 Cooled component, casting core for manufacturing such a component, as well as method for manufacturing such a component
05/02/2002EP1202053A1 Contoured surface eddy current inspection system
05/02/2002EP1201880A2 Cascade for turbomachines
05/02/2002EP1201879A2 Cooled component, casting core and method for the manufacture of the same
05/02/2002EP1201878A2 Bladed rotor
05/02/2002EP1201877A2 Method of positioning turbine stage arrays
05/02/2002EP1201778A2 Low density oxidation resistant superalloy materials capable of thermal barrier coating retention without a bond coat
05/02/2002EP1201343A2 Electrochemical machining process, electrode therefor and turbine bucket with turbulated cooling passage
05/02/2002EP1200713A1 Turbine guide vane for exhaust gas turbocharger
05/02/2002EP1200217A1 Directional solidification method and apparatus
05/02/2002DE10053770A1 Steam turbine regulating wheel producing process involves using entire rotor or part rotor piece as full material
05/01/2002CN1346724A Nozzle for gas turbine, electric generation gas turbine, Co-based alloy and welding material
04/2002
04/30/2002US6380512 Method for removing coating material from a cooling hole of a gas turbine engine component
04/30/2002US6379749 Method of removing ceramic coatings
04/30/2002US6379480 Method for obtaining thin, light and rigid metal parts
04/30/2002US6379118 Cooled blade for a gas turbine
04/30/2002US6379117 Cooling air supply system for a rotor
04/30/2002US6379113 Propeller apparatus
04/30/2002US6379112 Quadrant rotor mistuning for decreasing vibration
04/30/2002US6379108 Controlling a rabbet load and air/oil seal temperatures in a turbine
04/30/2002US6378755 Joined structure utilizing a ceramic foam bonding element, and its fabrication
04/25/2002WO2002033224A1 Fan blade compliant shim
04/25/2002WO2002032614A1 Process for drilling holes in a metallic workpiece having a thermal barrier coating
04/25/2002US20020048683 Low-sulfur article having a platinum-aluminide protective layer, and its preparation
04/25/2002US20020048514 High efficiency blade configuration for steam turbine
04/25/2002US20020048510 Method of positioning turbine stage arrays, particularly for aircraft engines
04/24/2002EP1199439A2 Configuration for reducing circumferential rim stress in a rotor assembly
04/24/2002EP1198675A1 System and method for manipulating and controlling fluid flow over a surface
04/24/2002EP1198619A2 Bond coats for turbine components and method of applying the same
04/24/2002CN1346424A 涡轮叶片 Turbine blades
04/24/2002CN1083525C 涡轮轴 Turboshaft
04/23/2002US6376801 Gas turbine component refurbishment apparatus and repair method
04/23/2002US6375429 Turbomachine blade-to-rotor sealing arrangement
04/23/2002US6375428 Turbine blisk rim friction finger damper
04/23/2002US6375425 Transpiration cooling in thermal barrier coating
04/23/2002US6375423 Method for removal of dovetailed turbine bucket from a turbine wheel
04/23/2002US6375421 Piggyback rotor blisk
04/23/2002US6375420 High efficiency blade configuration for steam turbine
04/23/2002US6375419 Flow directing element for a turbine engine
04/23/2002US6375415 Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment
04/23/2002US6375412 Viscous drag impeller components incorporated into pumps, turbines and transmissions
04/23/2002CA2262539C Gas turbine rotor
04/23/2002CA2261107C Gas turbine moving blade
04/18/2002WO2002030619A1 Peening method and machine therefor
04/18/2002US20020045053 Where the surface has an original chemical composition that varies with depth and at least a portion of the surface is missing from the substrate
04/18/2002US20020044870 Fan blade compliant layer and seal
04/18/2002US20020042978 Method of shot blasting and a machine for implementing such a method
04/18/2002DE10047826A1 Verfahren und Vorrichtung zum Vermindern von Resonanzerscheinungen Method and apparatus for reducing resonance phenomena
04/17/2002EP1197636A2 Cooling of gas turbine engine aerofoils
04/17/2002EP1197635A2 Gas turbine engine airfoil cooling
04/17/2002EP1197585A2 Method for repairing a thermal barrier coating and repaired coating formed thereby
04/17/2002EP1197574A1 Turbine blade coating tool
04/17/2002EP1197290A2 Braze repair of a gas turbine engine stationary shroud
04/17/2002EP1197289A1 Gas turbine component refurbishment apparatus and repair method
04/17/2002EP1197284A2 NON-submersion electrodischarge machining using conditioned water as a medium
04/17/2002EP1196696A2 Rotor with a split rotor blade
04/17/2002CN1083051C Wall cooled by reflecting flow
04/16/2002US6372679 Sintering powder mixture of alumina and dichromium trioxide in vacuum to form solid solution; resistance to molten salts and corrosion; coatings for rotor blades
04/16/2002US6372299 Applying aluminum-rich mixture to substrate to form a discontinuous layer of aluminum-rich particles in a matrix of metallic bond coat alloy
04/16/2002US6371727 Turbine blade tip shroud enclosed friction damper
04/16/2002US6371725 Conforming platform guide vane
04/16/2002US6371414 System and method for manipulating and controlling fluid flow over a surface
04/16/2002US6370752 Method for repositioning or repairing holes
04/11/2002US20020041805 Turbo Machines
04/10/2002EP0953100B1 Steam turbine
04/10/2002EP0929733B1 Turbine inter-disk cavity cooling air compressor
04/10/2002CN1343799A Method of adopting inorganic seriflux mixture for applicating coating contg aluminium
04/09/2002US6368672 Method for forming a thermal barrier coating system of a turbine engine component
04/09/2002US6368060 Shaped cooling hole for an airfoil
04/09/2002US6368057 Steam turbine
04/09/2002US6368055 Turbine nozzle and moving blade of axial-flow turbine
04/09/2002US6367687 Method for preparing a plate rim for brazing
04/04/2002WO2002027190A1 Multi-stage impeller
04/04/2002WO2002027147A1 Cooled turbine vane with endcaps
04/04/2002WO2002027146A1 Gas turbine blade
04/04/2002WO2002027145A2 Vane assembly for a turbine and combustion turbine with this vane assembly
04/04/2002US20020039647 Heat-resisting fiber-reinforced composite material and manufacturing method thereof
04/04/2002CA2420767A1 Multi-stage impeller
04/03/2002EP1193461A2 Method and apparatus for reduction of resonance phenomena
04/03/2002EP1193371A2 Baffle for the interstage disc cavity of a gas turbine
04/03/2002EP1193370A2 Turbocharger rotor with alignment couplings
04/03/2002EP1193235A2 A heat-resisting fiber-reinforced composite material and manufacturing method thereof
04/03/2002EP1192333A1 Component that can be subjected to hot gas, especially a turbine blade
04/02/2002US6365288 Barium-strontium aluminosilicate protective coating for silicon containg substrate which inhibits the formation of cracks and the formation of silicon gases when the article is exposed to a high temperature, aqueous environment
04/02/2002US6365236 Alternating the temperature during electron beam vapor deposition, layers are applied at different temperature conditions for different porosities
04/02/2002US6364971 Apparatus and method of repairing turbine blades