Patents
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
10/07/2008CA2467188C Internal cooled gas turbine vane or blade
10/07/2008CA2430285C Device for centring a tube in a turbine shaft
10/07/2008CA2366692C Method and apparatus for reducing turbine blade tip temperatures
10/07/2008CA2333011C A component for a gas turbine
10/03/2008CA2627788A1 Method for determining blade mistuning on integrally manufactured rotor wheels
10/02/2008WO2008117802A1 Heat resistant component
10/02/2008WO2008116906A1 Eccentric chamfer at inlet of branches in a flow channel
10/02/2008WO2008116757A2 Turbomachine blade with erosion and corrosion protective coating and method of manufacturing the same
10/02/2008WO2008116738A1 Gas turbine comprising a tie-rod with interior ventilation
10/02/2008WO2008116285A1 Coating removal from vane rings via tumble strip
10/02/2008WO2008081187A3 Tidal electricity generating apparatus
10/02/2008WO2008078024A3 Composite material part with a silicon-containing ceramic matrix protected against corrosion
10/02/2008WO2008012530A3 Impulse turbine for use in bi-directional flows
10/02/2008US20080240927 Turbine blade for a turbine with a cooling medium passage
10/02/2008US20080240926 Cobalt-Free Ni-Base Superalloy
10/02/2008US20080240925 Separable blade for wind turbine
10/02/2008US20080240924 Turbine blade
10/02/2008US20080240921 Fan and impeller thereof
10/02/2008US20080240917 Turbofan case and method of making
10/02/2008US20080240913 Fan frame with diversion structure
10/02/2008US20080237195 Welding slot sealing structure and welding method
10/02/2008DE102007015669A1 Turbomaschine Turbomachine
10/02/2008CA2676827A1 Coating removal from vane rings via tumble strip
10/01/2008EP1975581A1 Ceramic heat insulation coating, in particular for a turbine part, and device and method for determining the temperature of a turbine part
10/01/2008EP1975372A1 Eccentric chamfer at inlet of branches in a flow channel
10/01/2008EP1975371A2 Preswirl system for a gas turbine
10/01/2008EP1974071A1 Component for arrangement in the duct of a turbine engine and spray method for production of a coating
10/01/2008EP1973688A1 Method of making a hole
10/01/2008EP1815209A4 Improved measurement system
10/01/2008CN201126094Y Roll forming large and middle symmetrical solid dish type forgings
10/01/2008CN201126093Y Roll forming large and middle symmetrical hollow dish type forgings
10/01/2008CN201126092Y Roll forming large and middle asymmetry hollow dish type forgings
10/01/2008CN201126091Y Roll forming large and middle asymmetry solid dish type forgings
10/01/2008CN201125750Y Large-sized complete rotary speed 60Hz steam turbine last stage blade
10/01/2008CN101277783A A method and a device for production of a set of holes
10/01/2008CN100422510C Improved vane for variable nozzle turbocharger
10/01/2008CN100422508C Turbine airfoil trailing edge repair and methods therefor
09/2008
09/30/2008US7430119 Impeller and aligned cold plate
09/30/2008US7429403 Gas distributor for vapor coating method and container
09/30/2008US7429350 Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating
09/30/2008US7429337 Method for removing at least one area of a layer of a component consisting of metal or a metal compound
09/30/2008US7429166 Methods and apparatus for gas turbine engines
09/30/2008US7429165 Hybrid blade for a steam turbine
09/30/2008US7429164 Turbine moving blade
09/30/2008CA2498057C Gas turbine sealing air supply system
09/26/2008CA2625382A1 Metal injection molding process for bimetallic applications and airfoil
09/25/2008WO2008113695A2 Ceramic thermal insulation coating, in particular for a turbine component, and device and method for determining the temperature of a turbine component
09/25/2008WO2008113506A1 Rotor assembly for an exhaust gas turbocharger
09/25/2008US20080233831 Motive inflatable display
09/25/2008US20080233427 Thermomechanical fatigue resistance, ductility; diffusing platinum then aluminum into substrate surface; gas turbine blades
09/25/2008US20080232972 Blade fixing for a blade in a gas turbine engine
09/25/2008US20080232971 Coated turbine blade
09/25/2008US20080232970 Mold Assembly and Method for Injection Molding of an Impeller, and Impeller Formed by Said Method
09/25/2008US20080232969 Rotary assembly for a turbomachine fan
09/25/2008US20080232968 Non-axisymmetric end wall contouring for a turbomachine blade row
09/25/2008US20080232963 Turbine shroud segment transpiration cooling with individual cast inlet and outlet cavities
09/25/2008US20080232959 Compressor
09/25/2008US20080232956 Turbine Blade and Gas Turbine Equipped with a Turbine Blade
09/25/2008US20080229742 Extended Leading-Edge Compressor Wheel
09/25/2008US20080229737 Extruded stator blade, stator with extruded blade, and method of forming a stator assembly with extruded blades
09/25/2008US20080229567 Method for Repairing a Component of a Turbomachine
09/25/2008DE102008013773A1 Turboladeranordnung mit Katalysatorbeschichtung Turbocharger assembly with catalyst coating
09/25/2008DE102007014253A1 Turbine einer Gasturbine Turbine of a gas turbine
09/25/2008DE102007014030A1 Verfahren zur Instandsetzung von Bauteilen einer Gasturbine A process for the repair of components of a gas turbine
09/24/2008EP1972403A2 Methods and systems for forming turbulated cooling holes
09/24/2008EP1972396A1 Cast features for a turbine engine airfoil
09/24/2008EP1971761A1 Method and apparatus for balancing an electrically assisted turbocharger rotor
09/24/2008EP1971705A1 Layer system comprising two pyrochlore phases
09/24/2008EP1971443A1 Nozzle arrangement for, and method of, spraying cold gas
09/24/2008EP1761708A4 Device and method for detachably connecting an impeller to a shaft
09/24/2008CN101272880A Method for mending component with orienting micro-mechanism through setting temperature gradient in course of laser heat action, component manufactured by the same
09/24/2008CN101270688A Piston rotor internal combustion engine
09/24/2008CN100420825C Welded turbine shaft and method for producing said shaft
09/23/2008US7427188 Turbomachine blade with fluidically cooled shroud
09/23/2008CA2622945A1 Blade fixing for a blade in a gas turbine engine
09/23/2008CA2412989C Improvements to the thermal behaviour of the trailing edge of a high pressure turbine blade
09/21/2008CA2626118A1 Turbomachine fan rotor assembly
09/18/2008WO2008111585A1 Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE VANE USING THE SAME
09/18/2008WO2008110543A1 Covering strip connection of a turbine blade
09/18/2008WO2008110431A1 Rotor for a gas turbine
09/18/2008WO2008110430A1 Turbine comprising at least one rotor that consists of rotor disks and a tie bolt
09/18/2008WO2008110429A1 Rotor of a gas turbine
09/18/2008WO2008110161A1 Layer system and method for the production thereof
09/18/2008US20080226871 Layer System, Use and Process for Producing a Layer System
09/18/2008US20080226474 Flattened Brushless Motor Pump and Vehicle Electric Pump Unit Using Flattened Brushless Motor Pump
09/18/2008US20080226462 Cast features for a turbine engine airfoil
09/18/2008US20080226461 Intensively cooled trailing edge of thin airfoils for turbine engines
09/18/2008US20080226460 Compressor rotor
09/18/2008US20080226459 Rotor blade for a bearingless rotor of a rotorcraft
09/18/2008US20080226458 Turbomachine fan
09/18/2008US20080226457 Turbomachine rotor disk
09/18/2008US20080226456 Fan assembly and method
09/18/2008US20080226455 Quick click
09/18/2008US20080226454 High efficiency cooling fan
09/18/2008US20080226453 Balanced Turbine Rotor Fan Blade for a Tip Turbine Engine
09/18/2008US20080226452 Modular fan housing
09/18/2008US20080226450 Turbine with Coaxial Sets of Blades
09/18/2008US20080223099 Component With Compressive Residual Stresses, Process For Producing And Apparatus For Generating Compressive Residual Stresses
09/18/2008DE102007012941A1 Electrical energy generating device for wind turbine, has tailback blades rotation-symmetrically arranged at shaft component, overlapping to each other and arranged in angular position diagonal to longitudinal axis of component
09/18/2008DE102007012641A1 Laufzeug für einen Abgasturbolader Rotor assembly for an exhaust gas turbocharger