Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
07/2008
07/23/2008CN100404795C Turbo-machine and rotor therefor
07/23/2008CN100404794C Steam turbine
07/23/2008CN100404793C Gas turbine bucket tip cap
07/23/2008CN100404792C Gas turbine blade shroud
07/23/2008CN100404791C Compressor rotor blade
07/23/2008CA2619306A1 Turboprop engine comprising a propeller made up of adjustable blades
07/22/2008US7402347 In-situ formed thermal barrier coating for a ceramic component
07/22/2008US7402335 Layer structure and method for producing such a layer structure
07/18/2008CA2619299A1 Turbomachine fan rotor disc
07/17/2008WO2008064868A3 Turbocharger
07/17/2008US20080172267 Rotation Planning Apparatus and Rotation Planning System
07/17/2008US20080170946 Impingement cooled bucket shroud, turbine rotor incorporating the same, and cooling method
07/17/2008US20080170945 Aerofoil configuration
07/17/2008US20080170943 Composite inlet guide vane
07/17/2008US20080170942 Assembly for an aircraft engine compressor comprising blades with hammer attachment with inclined root
07/17/2008DE102008003412A1 In einen Turbinenrotor eingebaute Turbinenschaufelabdeckung mit Prallkühlung sowie Kühlverfahren In a turbine rotor built turbine blade cover with baffle cooling and cooling process
07/17/2008DE10128507B4 Verwendung einer Vorrichtung zum chemischen oder elektrochemischen Bearbeiten von Bauteilen Use of a device for chemical or electrochemical machining components
07/16/2008EP1944472A1 Axial rotor section for a rotor in a turbine, sealing element for a turbine rotor equipped with rotor blades and rotor for a turbine
07/16/2008EP1944471A1 Axial rotor section for a rotor in a turbine
07/16/2008EP1944470A2 Turbine vane with an impingement cooling insert
07/16/2008EP1944469A2 Turbine blade trip strip orientation
07/16/2008EP1944468A2 Gas turbine blade
07/16/2008EP1944467A2 Cooling circuit flow path for a turbine section airfoil
07/16/2008EP1944466A1 Coupling of two rotor blades
07/16/2008EP1944465A2 Gas turbine blade
07/16/2008EP1944387A1 System and method for restoring or regenerating an article
07/16/2008EP1944280A2 Environmental barrier coating for silicon-containing substrates and process therefor
07/16/2008EP1944120A2 Weld repair of metallic components
07/16/2008EP1944117A1 High temperature laser welding
07/16/2008EP1944100A1 Bending apparatus for bending a locking plate of a rotor in a turbine
07/16/2008CN101223355A Water turbine with bi-symmetric airfoil
07/16/2008CN101220756A Axial rotor section for a rotor of a turbine
07/16/2008CN101220755A Gas turbine blade
07/16/2008CN100402930C Splashboard and method for producing the same
07/16/2008CN100402812C Turbocharger system for an internal combustion engine
07/16/2008CN100402802C Coolable component and method for the production of a through opening in a coolable component
07/16/2008CN100402801C Guide blade for turbine and turbine containing the guide blade
07/16/2008CN100402800C Synthetic high-temp assembly and manufacturing method therefor
07/15/2008US7400994 Method and test component for rotatable disc parts
07/15/2008US7399164 Turbine engine and bladed rotor for a compression stage of a turbine engine
07/15/2008US7399163 Rotor blade for a compressor or a gas turbine
07/15/2008US7399162 Wind turbine
07/15/2008US7399161 Centrifugal fan
07/15/2008US7399160 Turbine component
07/15/2008US7399159 Detachable leading edge for airfoils
07/15/2008US7399158 Blade arrangement
07/14/2008CA2675107A1 Device for protecting components having a flammable titanium alloy from titanium fire and production method therefor
07/10/2008WO2008081486A1 Spacer for gas turbine blade insert
07/10/2008WO2008080655A1 Component with diagonally extending recesses in the surface and method for operating a turbine
07/10/2008WO2008057627A3 Flow-control technique to vector bulk flow leaving a vane
07/10/2008US20080166548 Coating material for thermal barrier coating having excellent corrosion resistance and heat resistance and method of producing the same
07/10/2008US20080166241 Wind turbine blade brush
07/10/2008US20080166240 Advanced cooling method for combustion turbine airfoil fillets
07/10/2008US20080166235 Wind Turbine Airfoil Family
07/10/2008US20080166225 Turbine blade tip and shroud clearance control coating system
07/10/2008US20080166222 Turbine rotor and steam turbine
07/10/2008US20080166221 Apparatus and Method for Active Gap Monitoring for a Continuous Flow Machine
07/10/2008US20080166220 Airfoil, sleeve, and method for assembling a combustor assembly
07/10/2008US20080163604 Turbine blade with reverse cooling air film hole direction
07/10/2008CA2674092A1 Tidal electricity generating apparatus
07/09/2008EP1942254A2 Methods and apparatus for fabricating a fan assembly for use with turbine engines
07/09/2008EP1942252A2 Airfoil tip for a rotor assembly
07/09/2008EP1942251A2 Cooled airfoil having reduced trailing edge slot flow
07/09/2008EP1942250A1 Component with bevelled grooves in the surface and method for operating a turbine
07/09/2008EP1942249A2 Heat transfer system for turbine engine using heat pipes
07/09/2008EP1941077A1 Technology for cleaning thermal fatigue cracks in nickel-based superalloys with a high chromium content
07/09/2008EP1940581A1 Method of producing a welded joint
07/09/2008EP1738060B1 Turbine blade with an impact cooling insert
07/09/2008EP1563167B1 Self-regulating turbine
07/09/2008CN100400889C Turbocharger for internal-combustion engine and compressor impeller used therein
07/09/2008CN100400799C Variable geometry turbocharger
07/09/2008CN100400798C Curved face vane for turbocharger
07/09/2008CN100400796C Turbine blade and gas turbine equipped with a turbine blade of this type
07/09/2008CN100400795C Turbine blade and gas turbine with such a turbine blade
07/08/2008US7396592 Composite target of a bar made of ceramic powders, zirconia and a zirconia stabilizer, after sintering of the target, zirconia contains a monoclinic phase; barrier is deposited on a superalloy substrate; low thermal conductivity, high thermomechanical strength
07/08/2008US7396208 Divided blade rotor
07/08/2008US7396205 Rotor blade for a rotary machine
07/08/2008US7395668 Turbo charged diesel-type piston engine and method for controlling such an engine
07/03/2008WO2008077374A1 Method for the production of a blisk or a bling and component produced thereby
07/03/2008US20080159874 Turbine blade trip strip orientation
07/03/2008US20080159872 Air conditioner fan
07/03/2008US20080159871 Method of Manufacturing a Wind Turbine Blade Shell Member
07/03/2008US20080159870 Method and coating for protecting and repairing an airfoil surface using molded boots, sheet or tape
07/03/2008US20080159869 Methods and apparatus for fabricating a rotor assembly
07/03/2008US20080159866 Fan blade for a gas turbine engine
07/03/2008US20080159864 Non-Positive-Displacement Machine and Rotor for a Non-Positive-Displacement Machine
07/03/2008US20080159861 Compressor with centripetal air takeoff
07/03/2008US20080159857 Turbine or compressor device and method for assembling the device
07/03/2008US20080159856 Guide vane and method of fabricating the same
07/03/2008US20080159853 Heat transfer device in a rotating structure
07/03/2008US20080159849 Welded Turbine Shaft and Method For Producing Said Shaft
07/03/2008US20080157429 Helicopter blade mandrel
07/03/2008DE102006061915A1 Hybrid-Fanschaufel und Verfahren zu deren Herstellung Hybrid fan blade and methods for their preparation
07/03/2008DE102006041505B4 Anordnung zum Erzeugen von Energie an einer Abtriebswelle nach dem Tornadoprinzip (Tornadoturbine) Arrangement for generating energy to an output shaft after the tornado principle (Tornado turbine)
07/03/2008CA2672150A1 Method and device for applying a protective medium to a turbine blade a nd method for introducing cooling bores into a turbine blade
07/02/2008EP1939405A2 Gas turbine engines including lean stator vanes and methods of assembling the same
07/02/2008EP1939403A2 Hybrid fan blade and method for their manufacture
07/02/2008EP1939402A2 Composite fan blade for a gas turbine engine
07/02/2008EP1939401A2 Methods and apparatus for load transfer in rotor assemblies
07/02/2008EP1939400A2 Airfoil cooling with staggered refractory metal cores forming microcircuits