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
07/02/2008EP1939399A2 Turbine assembly
07/02/2008EP1939398A2 Stator vane with lean and sweep
07/02/2008EP1939397A2 Turbine nozzle with bullnose step-down platform
07/02/2008EP1939396A2 Power turbine speed control system
07/02/2008EP1939395A2 Turbine engine shaft
07/02/2008EP1939325A2 Strain tolerant corrosion protecting coating and tape method of application
07/02/2008EP1939317A2 Thermal barrier coating
07/02/2008EP1939315A1 Component with a substrate and a protective layer
07/02/2008CN101213353A 涡轮机叶片 Turbine blades
07/02/2008CN101210498A Turbine blade and cooling system thereof
07/02/2008CN101210328A System and method for restoring or regenerating an article
07/02/2008CN100398838C Quick connect ceiling fan blade
07/02/2008CN100398810C Francis turbine
07/02/2008CN100398784C Guide blade with consistent base, its construction, and assembling method thereof
07/02/2008CN100398699C Cleaning and servicing technology for turbine blade basal body surface by strong current pulsed ionizing beam
07/02/2008CN100398256C Turbine blade of turine and its puller
07/01/2008US7393183 Trailing edge attachment for composite airfoil
07/01/2008US7393182 Composite tip shroud ring
07/01/2008US7392927 Combinatorial production of material compositions from a single sample
06/2008
06/30/2008CA2615620A1 Method and apparatus for increasing fatigue notch capability of airfoils
06/29/2008CA2615625A1 Methods and apparatus for fabricating a rotor assembly
06/29/2008CA2615606A1 Method for restoring or regenerating an article and restored or regenerated article
06/29/2008CA2610670A1 Airfoil component with internally machined cooling holes
06/28/2008CA2614406A1 Methods and apparatus for fabricating a fan assembly for use with turbine engines
06/26/2008WO2008076724A2 Method of forming yttrium-modified platinum aluminide diffusion coating
06/26/2008WO2008075716A1 Turbine blade
06/26/2008WO2008075400A1 Gas turbine
06/26/2008WO2008074371A1 Component with a substrate and a protective layer
06/26/2008US20080152506 Fan blade for a gas-turbine engine
06/26/2008US20080152502 Fan with spiral supercharging device
06/26/2008US20080152501 Turbomachine blade
06/26/2008US20080152494 Ice Management System For Rotary-Wing Aircraft
06/26/2008US20080152493 Method and system for utilizing lateral tower acceleration to detect asymmetric icing
06/26/2008US20080152481 Pump with Cutting Impeller and Pre-Chopper
06/26/2008US20080152475 Method for preventing backflow and forming a cooling layer in an airfoil
06/26/2008US20080148564 Turbine assembly for a gas turbine engine and method of manufacturing the same
06/26/2008DE202006020323U1 Einrichtung zur Wirbelumformung einer Strömung Means for forming a vortex flow
06/26/2008DE102007061564A1 Turbine blade for use in gas turbine engine, has cooling slot with inlet end that is in flow connection with cooling duct for receiving fluid, and outlet end adjacent to rear edge of blade
06/26/2008DE102007060930A1 Verfahren zur Rückflussverhinderung und Erzeugung einer Kühlschicht an einem Schaufelblatt Method for backflow prevention and generating a cooling layer of an airfoil
06/26/2008DE102006061916A1 Fanschaufel für ein Gasturbinentriebwerk A fan blade for a gas turbine engine
06/26/2008DE102006061448A1 Verfahren zur Herstellung einer Blisk oder eines Blings und damit hergestelltes Bauteil A method of manufacturing a blisk or a bling and thus produced component
06/26/2008DE102006061446A1 Verfahren und Vorrichtung zur Ermittlung des Austrittsquerschnitts eines Bauteils einer Gasturbine Method and device for determining the outlet cross-section of a component of a gas turbine
06/26/2008DE102006061444A1 Verfahren und Vorrichtung zur Aufbringung eines Schutzmediums auf eine Turbinenschaufel sowie Verfahren zur Einbringung von Kühlbohrungen in eine Turbinenschaufel Method and apparatus for applying a protective medium to a turbine blade as well as methods for the introduction of cooling holes in a turbine blade
06/26/2008DE102006060836A1 Fan wheel, for a turbocharger compressor/turbine, has a plastics body and a metal bush for the shaft with centrifugal forces contained within the body
06/26/2008DE102006060674A1 Receiving device for rotor blades being machined has blade able to be positioned in each receiving position with surface for blade foot against surface of receiving position
06/26/2008CA2673588A1 Turbine blade with temperature-dependent separation prevention means
06/26/2008CA2614031A1 Cooled airfoil and method for making an airfoil having reduced trail edge slot flow
06/25/2008EP1936120A2 A transition duct for a gas turbine engine
06/25/2008EP1936119A2 Turbine blade with device preventing wear at tip shroud
06/25/2008EP1936118A2 Turbine blade main core modifications for peripheral serpentine microcircuits
06/25/2008EP1936117A2 Airfoil with plasma generator at leading edge for vortex reduction and corresponding operating method
06/25/2008EP1936116A2 Airfoil with plasma generator on trailing edge and corresponding operating method
06/25/2008EP1936115A2 Turbine rotor and steam turbine
06/25/2008EP1936114A2 Methods and systems for balancing a rotatable member
06/25/2008EP1936007A2 Microwave process for forming a coating
06/25/2008EP1936002A1 Environmentally friendly wear resistant coating
06/25/2008EP1935532A1 Cluster bridged casting core
06/25/2008EP1935531A2 Process to cast seal slots in turbine vane shrouds
06/25/2008EP1934387A1 Method for removing the coating from a gas turbine component
06/25/2008EP1618287B1 Turbine bucket with curved aft shank walls for stress reduction
06/25/2008CN201078246Y Radial direction double-flow turbine
06/25/2008CN201078245Y Single-stage double-flow steam turbine
06/25/2008CN101208497A Turbine thermal shield and guide vane for a gas turbine
06/25/2008CN101205833A Thermal barrier coating
06/25/2008CN101205814A Turbine blade with device preventing wear at tip shroud
06/25/2008CN101205813A Methods and apparatus for load transfer in rotor assemblies
06/24/2008US7390171 High efficiency rotor for the second phase of a gas turbine
06/24/2008US7390170 Device for assembling annular flanges together, in particular in a turbomachine
06/24/2008US7390168 Vortex cooling for turbine blades
06/24/2008US7390167 Compressor with centripetal air takeoff
06/24/2008US7390165 High efficiency stator for the second phase of a gas turbine
06/24/2008US7390162 Rotary ram compressor
06/22/2008CA2613601A1 A turbine assembly for a gas turbine engine and method of manufacturing the same
06/21/2008CA2613781A1 Method for preventing backflow and forming a cooling layer in an airfoil
06/21/2008CA2613763A1 Airfoil with improved cooling slot arrangement
06/20/2008CA2613603A1 Methods and systems for balancing a rotatable member
06/19/2008WO2008072303A1 Friction welding, process for producing centrifugal gas turbine, and process for producing turbo charger
06/19/2008WO2008071467A2 Method for coating a component
06/19/2008WO2008071253A1 Turbocharger
06/19/2008WO2008071166A1 Device and method for the surface peening of a rotor of a gas turbine
06/19/2008WO2008071165A1 Device and method for the repair or production of blade tips of blades of a gas turbine, in particular of an aircraft engine
06/19/2008WO2008071164A1 Device and method for the surface peening of a component of a gas turbine
06/19/2008WO2008071161A1 Device and method for the surface peening of a component of a gas turbine
06/19/2008WO2008046556A3 Turbocharger
06/19/2008US20080145674 Yttria containing thermal barrier coating topcoat layer and method for applying the coating layer
06/19/2008US20080145236 Cooling arrangement for a tapered turbine blade
06/19/2008US20080145235 Airfoil cooling with staggered refractory metal core microcircuits
06/19/2008US20080145234 Cluster bridged casting core
06/19/2008US20080145233 Plasma induced virtual turbine airfoil trailing edge extension
06/19/2008US20080145230 Axial flow fan
06/19/2008US20080145229 Lightning Arrester System for a Wind Generator Blade
06/19/2008US20080145228 Aero-mixing of rotating blade structures
06/19/2008US20080145227 Methods and apparatus for load transfer in rotor assemblies
06/19/2008US20080145226 Process to cast seal slots in turbine vane shrouds
06/19/2008US20080145224 Vertical axis wind turbine system
06/19/2008US20080145223 Method and Device For Identifying the State of the Rotor of a Non-Positive-Displacement Machine
06/19/2008US20080145219 Vortex generators on rotor blades to delay an onset of large oscillatory pitching moments and increase maximum lift
06/19/2008US20080145210 Airfoil leading edge end wall vortex reducing plasma
06/19/2008DE102006058415A1 Flow machine, especially turbo-power plant for jet aircraft, has rotor blades with front edge on inflow side having curved shape
06/19/2008CA2672149A1 Device and method for the surface-peening of a component of a gas turbine