Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
11/2012
11/20/2012US8313303 Acoustical vibration dampener for a rotatable blade
11/20/2012US8313300 Rotor for centrifugal compressor
11/20/2012US8313296 Helicopter vibration control system and rotary force generator for canceling vibrations
11/20/2012US8313287 Turbine blade squealer tip rail with fence members
11/20/2012US8313285 Variable area nozzle assisted noise control of a gas turbine engine
11/20/2012CA2712143C Balancing apparatus for rotor assembly
11/15/2012WO2012153049A1 Turbine nozzle guide vane assembly in a turbomachine
11/15/2012WO2012152524A1 Single-crystal welding of directionally compacted materials
11/15/2012WO2012152259A1 Method for the production, reparation or replacement of a component, including a compacting step using pressure
11/15/2012WO2012152255A2 Checking a blade contour of a turbomachine
11/15/2012US20120288373 Rotor with asymmetric blade spacing
11/15/2012US20120286599 Generator with integrated blower
11/15/2012DE102012103991A1 Verschleissanzeigesystem zur Verwendung an Turbinenmaschinen und Verfahren zur Untersuchung derselben Verschleissanzeigesystem for use in turbine engines and methods for examination of the same
11/15/2012CA2833489A1 Turbine nozzle guide vane assembly in a turbomachine
11/14/2012EP2522816A2 A method of supporting a tool in an assembled apparatus
11/14/2012EP2522810A1 Method for generative production of a component, in particular of a compressor blade, and such a component
11/14/2012EP2522809A2 A method of reducing asymmetric fluid flow effects in a passage
11/14/2012EP2522454A1 Monocrystalline welding of directionally fixed materials
11/14/2012EP2522452A1 Combined heating by means of induction heating the workpiece and applying a coating by means of laser soldering
11/14/2012EP2522444A1 Ceramic core with composite insert for casting airfoils
11/14/2012CN202531278U Engine and eddy current pressurizing device thereof
11/14/2012CN1869408B Coated forward stub shaft dovetail slot
11/14/2012CN102782256A Composite material turbine engine blade and method for manufacturing same
11/14/2012CN102777312A Versatile kinetic energy recovery device
11/14/2012CN102777263A Fuel injection device of gas turbine
11/14/2012CN101737091B Last-stage moving blade of air-cooled feed pump steam turbine
11/14/2012CN101573510B Component with diagonally extending recesses in the surface and method for operating a turbine
11/13/2012US8308434 Wind turbine generator
11/13/2012CA2502791C High efficiency stator for the first phase of a gas turbine
11/08/2012WO2012150425A1 Turbomachine rotor with a means for axial retention of the blades
11/08/2012WO2012150413A1 Method for cleaning and stripping a turboshaft engine blade using a pulsed laser
11/08/2012WO2012131227A9 Device for locking blades in a groove of a turbomachine disc
11/08/2012WO2012075979A3 Process for electrochemically individually coating a component and apparatus
11/08/2012US20120283994 Turbine blade base load balancing
11/08/2012US20120282110 Inner ventilation blade
11/08/2012US20120282109 Blade, Integrally Bladed Rotor Base Body and Turbomachine
11/08/2012US20120282108 Turbine blade with chamfered squealer tip and convective cooling holes
11/08/2012US20120282107 Turbine airfoil cooling system with high density section of endwall cooling channels
11/08/2012US20120282106 Method of controlling grain size in forged precipitation-strengthened alloys and components formed thereby
11/08/2012US20120282104 Turbine engine fan disk
11/08/2012US20120282101 Gas turbine engine rotor construction
11/08/2012DE102011100783A1 Gasturbinenauswuchtvorrichtung Gasturbinenauswuchtvorrichtung
11/08/2012DE102011100221A1 Abdeckeinrichtung, integral beschaufelter Rotorgrundkörper, Verfahren und Strömungsmaschine Cover means integrally bladed rotor body, procedures and turbomachine
11/08/2012DE102011086831B3 Verfahren zur Reparatur eines Gasturbinenbauteils A method of repairing a gas turbine component
11/08/2012CA2834759A1 Turbomachine rotor with a means for axial retention of the blades
11/08/2012CA2834204A1 Method for cleaning and stripping a turboshaft engine blade using a pulsed laser
11/07/2012EP2520808A2 Gas turbine engine rotor construction
11/07/2012EP2520768A1 Sealing device for an integrated bladed rotor base body of a turbomachine
11/07/2012EP2520767A1 Gas turbine balancing device
11/07/2012EP2520764A1 Blade with cooled root
11/07/2012EP2520763A2 Impeller
11/07/2012EP2520762A1 Welding ti-6246 integrally bladed rotor airfoils
11/07/2012EP2520675A2 Treatment for preventing stress corrosion cracking
11/07/2012EP2519714A2 Gas turbine engine and main engine rotor assembly and disassembly
11/07/2012EP2519713A1 Inner ventilation blade
11/07/2012EP2519663A1 Method for the electrolytic deposition of a composite coating having a metal matrix containing particles for repairing a metal blade
11/07/2012EP2519437A1 Composite gas turbine engine component
11/07/2012CN202520572U Pneumatic submersible pump with idle overspeed protection function
11/07/2012CN202520385U Steam turbine blade
11/07/2012CN102770623A Turbine or compressor blade
11/07/2012CN102767398A Impeller and main shaft matched structure of turbo expander
11/07/2012CN102767397A Planar double-stroke gas turbine
11/07/2012CN102766837A Novel thermal barrier coating
11/07/2012CN102765957A Material for preparing turbine rotor of pressurizer and method for preparing turbine rotor by material
11/07/2012CN101802243B Heat-shielding coating material
11/06/2012US8303258 Fan platform fin
11/06/2012US8303257 Shiplap arrangement
11/06/2012US8303255 Shaft trim balancing devices, related systems and methods
11/06/2012US8303254 Turbine blade with tip edge cooling
11/06/2012US8303253 Turbine airfoil with near-wall mini serpentine cooling channels
11/06/2012US8303252 Airfoil with cooling passage providing variable heat transfer rate
11/05/2012DE202012009739U1 Integral gegossenes Turbinenrad Integral cast turbine
11/01/2012WO2012148012A1 Rotor blade for a tidal power generating turbine and method for manufacturing same
11/01/2012WO2012147938A1 Turbine blade
11/01/2012WO2012147723A1 Friction bonding method and bonding structure
11/01/2012WO2012146875A1 Turbine engine comprising a metal protector for a composite part
11/01/2012WO2012146483A1 Turbine component with coated balancing element for use at high temperatures
11/01/2012WO2012146480A1 An enhanced cooling surface
11/01/2012US20120275926 Welded rotor of a gas turbine engine compressor
11/01/2012US20120275923 Rotor for a turbo-machine
11/01/2012US20120275922 High area ratio turbine vane
11/01/2012US20120275921 Turbine engine and load reduction device thereof
11/01/2012US20120275920 Adaptor assembly for coupling turbine blades to rotor disks
11/01/2012US20120275918 Locking spacer assembly for a turbine engine
11/01/2012CA2834021A1 Friction joining method and joined structure
11/01/2012CA2833859A1 Turbine blade
10/2012
10/31/2012EP2518429A1 An enhanced cooling surface
10/31/2012EP2518280A1 Multistage radial turbine
10/31/2012EP2518277A1 Cooling method and device in single-flow turbine
10/31/2012EP2518271A2 Adaptor assembly for coupling turbine blades to rotor disks
10/31/2012EP2518270A2 Component and methods of fabricating a coated component using multiple types of fillers
10/31/2012EP2518269A2 Gas turbine stator vane
10/31/2012EP2518268A1 Turbine component with coated balancing weight for use in high temperatures
10/31/2012EP2518267A2 System and method for monitoring health of airfoils
10/31/2012EP2516808A1 Thermal barrier coating having low thermal conductivity
10/31/2012EP2516807A1 Method for cooling turbine stators and cooling system for implementing said method
10/31/2012EP2516697A1 Coating systems for protection of substrates exposed to hot and harsh environments and coated articles
10/31/2012EP2516696A1 Methods for coating articles exposed to hot and harsh environments
10/31/2012EP2516688A1 Method for producing a rotor/stator seal of a gas turbine
10/31/2012EP2516107A1 Method for creating metal reinforcement for a turbine engine blade
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