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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12/24/2002 | US6497920 Gas turbine airfoil |
12/24/2002 | US6497758 Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles |
12/24/2002 | CA2077843C Turbine blade platform damper |
12/19/2002 | WO2002101204A1 Turbine blade and turbine power generating equipment |
12/19/2002 | US20020194450 Apparatus and structure for rapid enablement |
12/19/2002 | US20020193897 Method and apparatus for electronically determining nozzle throat area and harmonics |
12/19/2002 | US20020192491 Oxidation resistant coatings for niobium-based silicide composites |
12/19/2002 | US20020190039 Ceramic matrix composite turbine components |
12/19/2002 | US20020189722 Turbine engine component having wear coating and method for coating a turbine engine component |
12/19/2002 | US20020189262 Method for operating a steam turbine , and a turbine system provided with a steam turbine that functions according to said method |
12/19/2002 | US20020189229 Gas turbine for power generation and combined power generation system |
12/18/2002 | EP1267042A2 Shrouded gas turbine blade |
12/18/2002 | EP1267041A2 Cooled turbine blade |
12/18/2002 | EP1267040A2 Gas turbine blade |
12/18/2002 | EP1267039A1 Cooling configuration for an airfoil trailing edge |
12/18/2002 | EP1267038A2 Air cooled aerofoil |
12/18/2002 | EP1267037A2 Cooled hollow tip shroud of a turbine blade |
12/18/2002 | EP1266129A1 Fastening of the blades of a compression machine |
12/18/2002 | EP1266128A1 Reinforcement and cooling structure of a turbine blade |
12/18/2002 | EP1266127A1 Cooling system for a turbine blade |
12/18/2002 | EP0906494B1 Turbine shaft and process for cooling it |
12/18/2002 | CN1385281A Method for making and repairing wing surface of integral propeller rotator |
12/18/2002 | CN1096562C Method for producing wear-endangered component of a turbo-machine |
12/17/2002 | US6495793 Laser repair method for nickel base superalloys with high gamma prime content |
12/17/2002 | US6495207 Open cell metal foam core layer bonded to an inner and an outer cladding layer; manufacturing a combustor for a gas turbine engine having an air permeable open cell metal foam core bounded by perforated thin metal or ceramic walls |
12/17/2002 | US6494684 Locking devices |
12/17/2002 | US6494683 Repaired turbine rotor wheel |
12/17/2002 | US6494682 Ceiling fan assembly and method for assembling same |
12/17/2002 | US6494678 Film cooled blade tip |
12/17/2002 | US6494677 Turbine nozzle segment and method of repairing same |
12/17/2002 | US6494672 Method and apparatus for antisurge control of turbocompressors having complex and changing surge limit lines |
12/17/2002 | US6494044 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method |
12/17/2002 | US6493936 Method of making steam turbine blade |
12/12/2002 | WO2002099254A1 Abradeable seal system |
12/12/2002 | WO2002099253A1 Gas turbine |
12/12/2002 | US20020188494 Method and apparatus for managing an operation |
12/12/2002 | US20020187336 Protective coatings; heat resistance; mixing powders |
12/12/2002 | US20020187327 Overcoating interior passageway with protective coating; gas turbine engines |
12/12/2002 | US20020187061 Vane design for use in variable geometry turbocharger |
12/12/2002 | US20020187046 Turbomachine rotor assembly with two bladed-discs separated by a spacer |
12/12/2002 | US20020187044 Turbine airfoil and method for manufacture and repair thereof |
12/12/2002 | US20020187043 Airfoil trailing edge cooling construction |
12/12/2002 | US20020187042 Turbine airfoil with separately formed tip and method for manufacture and repair thereof |
12/12/2002 | US20020187039 Gas turbine engine blade |
12/12/2002 | US20020185524 Bonded niobium silicide and molybdenum silicide composite articles using brazes |
12/12/2002 | US20020185247 Single crystal seed |
12/12/2002 | US20020185198 Repair of single crystal nickel based superalloy article |
12/12/2002 | DE10223701A1 Einzelkristallkeim Single crystal seed |
12/11/2002 | EP1264964A1 Arrangement for turbomachine rotor with two blade discs separated by a spacer |
12/11/2002 | EP1263997A1 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting |
12/11/2002 | EP0774045B1 Centrifugal chopper pump |
12/10/2002 | US6492038 Thermally-stabilized thermal barrier coating and process therefor |
12/10/2002 | US6491498 Turbine blade pocket shroud |
12/10/2002 | US6491497 Method and apparatus for supporting rotor assemblies during unbalances |
12/10/2002 | US6491496 Turbine airfoil with metering plates for refresher holes |
12/10/2002 | US6491495 Closed circuit blade-cooled turbine |
12/10/2002 | US6491493 Turbine nozzle vane |
12/10/2002 | US6491208 Cold spray repair process |
12/10/2002 | US6490899 Method and apparatus for peening tops of cooled blades |
12/10/2002 | US6490791 Method for repairing cracks in a turbine blade root trailing edge |
12/10/2002 | CA2349154C Rotary-turbine internal combustion engine |
12/10/2002 | CA2260498C Material for gas turbine disk |
12/10/2002 | CA2232897C Gas turbine cooling moving blade |
12/10/2002 | CA2118557C A cooled turbine nozzle assembly and a method of calculating the diameters of cooling holes for use in such an assembly |
12/05/2002 | WO2002097241A1 Turbine blade with sealing element |
12/05/2002 | WO2002097162A1 Thermal barrier coatings and fabrication of same using electrochemical methods |
12/05/2002 | WO2002097160A1 Coating forming method and coating forming material, and abrasive coating forming sheet |
12/05/2002 | US20020182362 Method for repairing a thermal barrier coating and repaiied coating formed thereby |
12/05/2002 | US20020182100 High strength, heat resistance, aircraft |
12/05/2002 | US20020182081 Device for fastening a moving blade to the rotor of a turbomachine |
12/05/2002 | US20020182074 Film cooled blade tip |
12/05/2002 | US20020182073 Turbine rotor |
12/05/2002 | US20020182070 Bonded niobium silicide and molybdenum silicide composite articles and method of manufacture |
12/05/2002 | US20020182069 Turbo machines |
12/05/2002 | US20020182059 Centripetal air-bleed system |
12/05/2002 | US20020182056 Closed loop steam cooled airfoil |
12/05/2002 | US20020178727 Methods and apparatus for injecting fuel into gas turbine engines |
12/04/2002 | EP1262635A1 Variable vane for use in turbo machines |
12/04/2002 | EP1262633A1 Turbine blade with knife edge sealing |
12/04/2002 | EP1262632A1 Turbine airfoil with separately formed tip and method for manufacture and repair thereof |
12/04/2002 | EP1262631A2 Film cooled blade or vane |
12/04/2002 | EP1262630A1 Centripetal air bleed device |
12/04/2002 | EP0964981B1 Turbine blade and its use in a gas turbine system |
12/04/2002 | CN1382837A Fin stripping system with feedback control of water treatment and acid reusing system |
12/03/2002 | US6489582 Non-submersion electrodischarge machining using conditioned water as a medium |
12/03/2002 | US6488473 Retaining arrangement for rotor blades of axial-flow turbomachinery |
12/03/2002 | US6488238 Boundary layer control of aerodynamic airfoils |
11/28/2002 | US20020176776 Component of a flow machine |
11/28/2002 | US20020175190 Valve, in particular pressure reducing valve |
11/27/2002 | EP1260678A1 Cooling device for gas turbine components |
11/27/2002 | EP1260674A1 Turbine blade and turbine |
11/27/2002 | EP1260673A2 Turbine cooling circuit |
11/27/2002 | EP1260612A1 A bond or overlay MCrAIY-coating |
11/27/2002 | EP1260610A2 High temperature resistant object |
11/27/2002 | EP1260608A1 Method of depositing a MCrAIY bond coating |
11/27/2002 | EP1260602A1 Process for producing a thermally insulating coating system on a metallic substrate |
11/27/2002 | EP1259711A1 Aerofoil for an axial flow turbomachine |
11/27/2002 | EP1259348A1 Clean melt nucleated casting systems and methods with cooling of the casting |
11/27/2002 | EP0972128B1 Surface structure for the wall of a flow channel or a turbine blade |
11/26/2002 | US6485845 Thermal barrier coating system with improved bond coat |