Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2002
12/24/2002US6497920 Gas turbine airfoil
12/24/2002US6497758 Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles
12/24/2002CA2077843C Turbine blade platform damper
12/19/2002WO2002101204A1 Turbine blade and turbine power generating equipment
12/19/2002US20020194450 Apparatus and structure for rapid enablement
12/19/2002US20020193897 Method and apparatus for electronically determining nozzle throat area and harmonics
12/19/2002US20020192491 Oxidation resistant coatings for niobium-based silicide composites
12/19/2002US20020190039 Ceramic matrix composite turbine components
12/19/2002US20020189722 Turbine engine component having wear coating and method for coating a turbine engine component
12/19/2002US20020189262 Method for operating a steam turbine , and a turbine system provided with a steam turbine that functions according to said method
12/19/2002US20020189229 Gas turbine for power generation and combined power generation system
12/18/2002EP1267042A2 Shrouded gas turbine blade
12/18/2002EP1267041A2 Cooled turbine blade
12/18/2002EP1267040A2 Gas turbine blade
12/18/2002EP1267039A1 Cooling configuration for an airfoil trailing edge
12/18/2002EP1267038A2 Air cooled aerofoil
12/18/2002EP1267037A2 Cooled hollow tip shroud of a turbine blade
12/18/2002EP1266129A1 Fastening of the blades of a compression machine
12/18/2002EP1266128A1 Reinforcement and cooling structure of a turbine blade
12/18/2002EP1266127A1 Cooling system for a turbine blade
12/18/2002EP0906494B1 Turbine shaft and process for cooling it
12/18/2002CN1385281A Method for making and repairing wing surface of integral propeller rotator
12/18/2002CN1096562C Method for producing wear-endangered component of a turbo-machine
12/17/2002US6495793 Laser repair method for nickel base superalloys with high gamma prime content
12/17/2002US6495207 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
12/17/2002US6494684 Locking devices
12/17/2002US6494683 Repaired turbine rotor wheel
12/17/2002US6494682 Ceiling fan assembly and method for assembling same
12/17/2002US6494678 Film cooled blade tip
12/17/2002US6494677 Turbine nozzle segment and method of repairing same
12/17/2002US6494672 Method and apparatus for antisurge control of turbocompressors having complex and changing surge limit lines
12/17/2002US6494044 Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
12/17/2002US6493936 Method of making steam turbine blade
12/12/2002WO2002099254A1 Abradeable seal system
12/12/2002WO2002099253A1 Gas turbine
12/12/2002US20020188494 Method and apparatus for managing an operation
12/12/2002US20020187336 Protective coatings; heat resistance; mixing powders
12/12/2002US20020187327 Overcoating interior passageway with protective coating; gas turbine engines
12/12/2002US20020187061 Vane design for use in variable geometry turbocharger
12/12/2002US20020187046 Turbomachine rotor assembly with two bladed-discs separated by a spacer
12/12/2002US20020187044 Turbine airfoil and method for manufacture and repair thereof
12/12/2002US20020187043 Airfoil trailing edge cooling construction
12/12/2002US20020187042 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
12/12/2002US20020187039 Gas turbine engine blade
12/12/2002US20020185524 Bonded niobium silicide and molybdenum silicide composite articles using brazes
12/12/2002US20020185247 Single crystal seed
12/12/2002US20020185198 Repair of single crystal nickel based superalloy article
12/12/2002DE10223701A1 Einzelkristallkeim Single crystal seed
12/11/2002EP1264964A1 Arrangement for turbomachine rotor with two blade discs separated by a spacer
12/11/2002EP1263997A1 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting
12/11/2002EP0774045B1 Centrifugal chopper pump
12/10/2002US6492038 Thermally-stabilized thermal barrier coating and process therefor
12/10/2002US6491498 Turbine blade pocket shroud
12/10/2002US6491497 Method and apparatus for supporting rotor assemblies during unbalances
12/10/2002US6491496 Turbine airfoil with metering plates for refresher holes
12/10/2002US6491495 Closed circuit blade-cooled turbine
12/10/2002US6491493 Turbine nozzle vane
12/10/2002US6491208 Cold spray repair process
12/10/2002US6490899 Method and apparatus for peening tops of cooled blades
12/10/2002US6490791 Method for repairing cracks in a turbine blade root trailing edge
12/10/2002CA2349154C Rotary-turbine internal combustion engine
12/10/2002CA2260498C Material for gas turbine disk
12/10/2002CA2232897C Gas turbine cooling moving blade
12/10/2002CA2118557C A cooled turbine nozzle assembly and a method of calculating the diameters of cooling holes for use in such an assembly
12/05/2002WO2002097241A1 Turbine blade with sealing element
12/05/2002WO2002097162A1 Thermal barrier coatings and fabrication of same using electrochemical methods
12/05/2002WO2002097160A1 Coating forming method and coating forming material, and abrasive coating forming sheet
12/05/2002US20020182362 Method for repairing a thermal barrier coating and repaiied coating formed thereby
12/05/2002US20020182100 High strength, heat resistance, aircraft
12/05/2002US20020182081 Device for fastening a moving blade to the rotor of a turbomachine
12/05/2002US20020182074 Film cooled blade tip
12/05/2002US20020182073 Turbine rotor
12/05/2002US20020182070 Bonded niobium silicide and molybdenum silicide composite articles and method of manufacture
12/05/2002US20020182069 Turbo machines
12/05/2002US20020182059 Centripetal air-bleed system
12/05/2002US20020182056 Closed loop steam cooled airfoil
12/05/2002US20020178727 Methods and apparatus for injecting fuel into gas turbine engines
12/04/2002EP1262635A1 Variable vane for use in turbo machines
12/04/2002EP1262633A1 Turbine blade with knife edge sealing
12/04/2002EP1262632A1 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
12/04/2002EP1262631A2 Film cooled blade or vane
12/04/2002EP1262630A1 Centripetal air bleed device
12/04/2002EP0964981B1 Turbine blade and its use in a gas turbine system
12/04/2002CN1382837A Fin stripping system with feedback control of water treatment and acid reusing system
12/03/2002US6489582 Non-submersion electrodischarge machining using conditioned water as a medium
12/03/2002US6488473 Retaining arrangement for rotor blades of axial-flow turbomachinery
12/03/2002US6488238 Boundary layer control of aerodynamic airfoils
11/2002
11/28/2002US20020176776 Component of a flow machine
11/28/2002US20020175190 Valve, in particular pressure reducing valve
11/27/2002EP1260678A1 Cooling device for gas turbine components
11/27/2002EP1260674A1 Turbine blade and turbine
11/27/2002EP1260673A2 Turbine cooling circuit
11/27/2002EP1260612A1 A bond or overlay MCrAIY-coating
11/27/2002EP1260610A2 High temperature resistant object
11/27/2002EP1260608A1 Method of depositing a MCrAIY bond coating
11/27/2002EP1260602A1 Process for producing a thermally insulating coating system on a metallic substrate
11/27/2002EP1259711A1 Aerofoil for an axial flow turbomachine
11/27/2002EP1259348A1 Clean melt nucleated casting systems and methods with cooling of the casting
11/27/2002EP0972128B1 Surface structure for the wall of a flow channel or a turbine blade
11/26/2002US6485845 Thermal barrier coating system with improved bond coat