Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
10/2008
10/29/2008CN100429385C Dual-use radial turbomachine
10/29/2008CN100429382C Turbine blade and method for producing turbine blade
10/29/2008CN100429381C Mounting method and device for gas turbine jet nozzle
10/28/2008US7442444 Bond coat for silicon-containing substrate for EBC and processes for preparing same
10/28/2008US7442417 Method for reaction control coating
10/28/2008US7442011 Locking device for turbine blades
10/28/2008US7442008 Cooled gas turbine aerofoil
10/28/2008US7442007 Angled blade firtree retaining system
10/28/2008US7441585 Apparatus and method for reducing operating stress in a turbine blade and the like
10/28/2008US7441410 Gas turbine and manufacturing process of gas turbine
10/27/2008CA2629877A1 Rotor supports and systems
10/27/2008CA2629803A1 Damper for turbine engine blades
10/23/2008WO2008125426A1 Heat-curing coating composition.
10/23/2008US20080260538 Spar and shell constructed turbine blade
10/23/2008US20080260537 Turbine Blade with an Impingement Cooling Insert
10/23/2008US20080260536 Blade arrangement
10/23/2008US20080260535 Blade/disk dovetail backcut for blade/disk stress reduction (6fa+e, stage2)
10/23/2008US20080260534 Blade/disk dovetail backcut for blade/disk stress reduction (7fa+e, stage 1)
10/23/2008DE102007017827A1 Abgasturbolader für oder in einem Kraftfahrzeug mit einer verdichterseitig an einer inneren Oberfläche vorgesehenen selbstreinigenden Beschichtung Exhaust gas turbocharger for or in a motor vehicle having a compressor side provided at an inner surface of self-cleaning coating
10/23/2008DE102007017822A1 Abgasturbolader Exhaust gas turbocharger
10/22/2008EP1983159A2 Shrouded single crystal dual alloy turbine disk
10/22/2008EP1983158A1 Method of determining maintenance intervals of a turbomachine and control system therefor
10/22/2008EP1983074A1 Heat hardened coating compound
10/22/2008EP1982791A2 Manufacturing method for a hollow fan blade
10/22/2008EP1711298B1 Process of brazing repairing of a part having a base material with oriented microstructure
10/22/2008CN201137516Y Semi-circle shaped double flow path turbo-charger
10/22/2008CN101291806A Durable thermal barrier coating having low thermal conductivity
10/21/2008US7438533 Wind turbine rotor blade
10/21/2008US7438532 Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 2)
10/21/2008US7438530 Method of assembling one-piece bladed disks, and a device for damping vibration of the blades of such disks
10/21/2008US7438529 Compressor and turbine wheel for a secondary air feed device
10/21/2008US7438528 Component having a cooling arrangement
10/21/2008US7438527 Airfoil trailing edge cooling
10/21/2008US7438523 Blade for a turbine engine and method for production of said blade
10/21/2008US7438518 Gas turbine nozzle guide vane
10/21/2008CA2506206C Blade structure in a gas turbine
10/21/2008CA2353265C Metallic article with integral end band under compression and method for making
10/20/2008CA2629460A1 Shrouded single crystal dual alloy turbine disk
10/18/2008CA2598877A1 Wind turbine blade having curved camber and method of manufacturing same
10/16/2008WO2008123418A1 Coating material, method for production thereof, coating method, rotor blade equipped with shroud
10/16/2008WO2008122492A1 Arrangement for axially securing rotating blades in a rotor, and gas turbine having such an arrangement
10/16/2008US20080253896 High efficiency fan blades with airflow-directing baffle elements
10/16/2008US20080253895 Blade retention system for use in a gas turbine engine
10/16/2008US20080253894 Co-forged steel rotor component for steam and gas turbine engines
10/16/2008US20080253890 Co-forged nickel-steel rotor component for steam and gas turbine engines
10/16/2008US20080253885 Gas turbine engine vane
10/16/2008US20080251642 method and a device for de-icing an aircraft wall
10/16/2008DE102007017692A1 Exhaust gas turbocharger for internal combustion engine of commercial vehicle, has compressor wheel connected with shaft over pivot in torque proof manner, and joint provided between pivot and shaft in area of radial bearings of shaft
10/15/2008EP1980720A2 Turbine engine variable stator vane
10/15/2008EP1980716A2 Damper configured turbine blade
10/15/2008EP1980715A1 Damping of vibrations in blades and guide vanes with grains
10/15/2008EP1980714A2 Turbomachine blade
10/15/2008EP1980713A2 Local application of a protective coating on a shrouded gas turbine engine component
10/15/2008EP1980634A1 Metal alloy compositions and articles comprising the same
10/15/2008EP1980631A1 Method for shot peening a turbine blade for the hot area of a gas turbine
10/15/2008EP1980366A1 Facility and device concept for a shotpeening facility for strengthening rotor blade bases in gas turbines
10/15/2008EP1979706A1 Measuring apparatus
10/15/2008CN201133282Y Double flow path turbo-charger
10/15/2008CN201133281Y Turbo-charger
10/15/2008CN101285404A Steam turbine rotor blades cover band structure and its machining process
10/15/2008CN101285403A Turbine blades microchannel inner cooling system airflow channel structure
10/15/2008CN101285402A Aeromechanical blade
10/15/2008CN101285401A Firtree -type bucket root steam turbine rotor blades and its locking notch vane
10/15/2008CN101285400A Firtree-type bucket root rotor blades
10/15/2008CN100425812C Element of turbomachinery with cool unit
10/14/2008US7435058 Ceramic matrix composite vane with chordwise stiffener
10/14/2008US7435055 Locking spacer assembly for a turbine engine
10/14/2008US7435053 Turbine blade cooling system having multiple serpentine trailing edge cooling channels
10/14/2008US7435049 Sealing device and method for turbomachinery
10/13/2008CA2628626A1 Fan blade
10/12/2008CA2625591A1 Blade retention system for use in a gas turbine engine
10/10/2008CA2620484A1 Damper configured turbine blade
10/09/2008WO2008121047A1 A gas turbine engine component, a turbojet engine provided therewith, and an aircraft provided therewith
10/09/2008WO2008120748A1 Wall of turbo machine and turbo machine
10/09/2008WO2007116176A3 Composite material component with silicon-containing ceramic matrix, protected against corrosion
10/09/2008US20080247872 Method of Operation of a High-Efficiency Turbine With Variable Attack Angle Foils
10/09/2008US20080247868 Fan and impeller thereof
10/09/2008US20080247865 Device and Method for Axially Displacing a Turbine Rotor
10/09/2008DE102007016369A1 Verfahren zur Ermittlung der Schaufelverstimmung bei Laufrädern in Integralbauweise Method for determining the blade upset with wheels integral structure
10/09/2008CA2682489A1 Wall of turbo machine and turbo machine
10/08/2008EP1978212A2 Stator assembly for gas turbine engine
10/08/2008EP1978211A1 Assembly for axial protection on rotor blades in a rotor and gas turbine with such an assembly
10/08/2008EP1978210A1 Methods and apparatus for coating gas turbine engines
10/08/2008EP1978209A2 Vortex spoiler for delivery of cooling airflow in a turbine engine
10/08/2008EP1978208A2 Multi-alloy turbine rotors and methods of manufacturing the rotors
10/08/2008EP1978133A1 Coating removal from turbine components via tumble strip
10/08/2008EP1977083A1 Turbine blade with recessed tip
10/08/2008EP1977082A2 Electric turbine bypass fan and compressor for hybrid propulsion
10/08/2008EP1208290B1 Cooled airfoil
10/08/2008CN101280694A Thermal insulation board, bearing casing and turbo casing for exhaust-gas-turbine, and exhaust-gas-turbine
10/08/2008CN101280692A Turbine blade middle part microchannel inner-cooling structure
10/08/2008CN100424338C Rotor blade for a wind power installation with a damping device
10/07/2008US7431565 Method of repairing a threaded generator rotor blower assembly
10/07/2008US7431564 Turbine blisk
10/07/2008US7431562 Method and apparatus for cooling gas turbine rotor blades
10/07/2008US7431561 Method and apparatus for cooling gas turbine rotor blades
10/07/2008US7431559 Dirt separation for impingement cooled turbine components
10/07/2008US7431197 Method of fabricating a hollow mechanical part by diffusion welding and superplastic forming
10/07/2008US7430852 Turbojet having a large bypass ratio
10/07/2008US7430802 Labyrinth seal in a stationary gas turbine
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