Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2008
05/29/2008US20080124219 Turbine exhaust strut airfoil profile
05/29/2008US20080124218 Tip Turbine Egine Comprising Turbine Clusters And Radial Attachment Lock Arrangement Therefor
05/29/2008US20080124211 Diffuser Aspiration For A Tip Turbine Engine
05/29/2008DE102007055572A1 Schweißen einer Statorausgleichsplatte Welding a Statorausgleichsplatte
05/29/2008DE102006055869A1 Rotor and guide blades designing method for turbo-machine i.e. gas turbine engine, involves running skeleton curve in profile section in sectional line angle distribution area lying between upper and lower limit curves
05/28/2008EP1925782A1 Non wetable surface coating of steam turbine parts which work in wet steam
05/28/2008EP1925781A1 Blade arrangement
05/28/2008EP1925780A1 Blade for an axial-flow turbine
05/28/2008EP1925779A1 Flow guiding component and method of production therefore
05/28/2008EP1925391A1 Laser fillet welding
05/28/2008EP1924757A1 Cover strip comprising a detachable anchoring for a row of blades of a turbomachine
05/28/2008EP1924391A1 Method of producing holes
05/28/2008EP1649145B1 Turbofan casing, turbofan engine and corresponding method
05/28/2008CN101187312A System for manufacturing a rotor having an MMC ring component and a unitary airfoil component
05/28/2008CN100390378C Manufacturing method for obtaining high-temperature components for gas turbines and components thus obtained
05/28/2008CN100390377C Method for making turbine blade
05/28/2008CA2612038A1 Cmc articles having small complex features
05/28/2008CA2611359A1 Lp turbine vane airfoil profile
05/28/2008CA2611112A1 Lp turbine blade airfoil profile
05/28/2008CA2610627A1 Hp turbine blade airfoil profile
05/28/2008CA2610173A1 Hp turbine vane airfoil profile
05/27/2008US7377749 Device for balancing a rotating part, in particular a turbojet rotor
05/27/2008US7377748 Fanned trailing edge teardrop array
05/27/2008US7377747 Turbine airfoil with integrated impingement and serpentine cooling circuit
05/27/2008US7377743 Countercooled turbine nozzle
05/27/2008US7377417 Repair process
05/27/2008US7377115 Approach to extending life of gas turbine engine
05/27/2008US7377037 Fillet machining method without adaptive probing
05/27/2008US7377036 Methods for tuning fuel injection assemblies for a gas turbine fuel nozzle
05/27/2008CA2434920C Superalloy for single crystal turbine vanes
05/27/2008CA2363276C Ultrasonic shot-peening process and system for rotor blade attachment ring sockets
05/27/2008CA2282010C Film-cooling hole and method of producing it
05/22/2008WO2008059620A1 Film cooling structure
05/22/2008WO2008058827A1 Liner in a cooling channel of a turbine blade
05/22/2008US20080118367 Cooling of turbine blade suction tip rail
05/22/2008US20080118366 Bifeed serpentine cooled blade
05/22/2008US20080118364 Hp turbine blade airfoil profile
05/22/2008US20080118363 Triforial tip cavity airfoil
05/22/2008US20080118362 Transonic compressor rotors with non-monotonic meanline angle distributions
05/22/2008US20080118361 Hp turbine vane airfoil profile
05/22/2008US20080118360 Lp turbine vane airfoil profile
05/22/2008US20080118359 Turbine exhaust strut airfoil profile
05/22/2008US20080118358 Lp turbine blade airfoil profile
05/22/2008US20080118355 Turbine Vane for Turbo-Machines and Method for Fabricating
05/22/2008US20080118350 Turbine seal guards
05/22/2008CA2610625A1 Lp turbine blade airfoil profile
05/22/2008CA2610539A1 Hp turbine vane airfoil profile
05/22/2008CA2610538A1 Hp turbine blade airfoil profile
05/22/2008CA2610528A1 Lp turbine vane airfoil profile
05/21/2008EP1923574A1 Compressor, turbine and method for supplying heating gas
05/21/2008EP1923537A2 Double feeding for the serpentine of a cooled blade
05/21/2008EP1923536A1 Liner in a cooling channel of a turbine blade
05/21/2008EP1922482A2 Wind fin: articulated, oscillating wind power generator
05/21/2008EP1922471A1 Arrangement for axially securing rotating blades in a rotor and use
05/21/2008EP1922431A1 Method for coating or decoating a component
05/21/2008DE102007055410A1 Schaufelblatt mit Dreifachbogen-Spitzenhohlraum Blade with triple bow-tip cavity
05/21/2008DE102007054912A1 Vorrichtung und Verfahren zum Kappen von Verdichterschaufelspitzen in-situ Apparatus and method for caps of compressor blade tips in-situ
05/21/2008DE102006054154A1 Supercharger for internal combustion engine, has turbine and rotor body with groove, which is encased in circumferential direction at side, and groove is cut through recesses serving for accommodation of rotating blades
05/21/2008CN101182785A Integrally bladed rotor having an MMC ring component and an airfoil component having mmc airfoils
05/21/2008CN101182784A Ultrasound profile applied to aerial engine fan/compressor rotor and design method thereof
05/20/2008US7374821 Low thermoconductivity and high high-temperature strength; for turbines; zirconia-based ceramic stabilized with trivalent oxide and oxygen vacancies reduced by pentavalent oxides, such as zirconia with yttria and niobium oxide
05/20/2008US7374402 Fastening arrangement for an impeller on a shaft
05/20/2008US7374401 Bell-shaped fan cooling holes for turbine airfoil
05/20/2008US7374400 Turbine blade arrangement
05/20/2008US7374398 Automotive compressor
05/20/2008US7373773 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation
05/20/2008CA2610090A1 Triforial tip cavity airfoil
05/20/2008CA2450723C Method of repairing a ni-based alloy part
05/15/2008WO2008055764A1 Turbine blade
05/15/2008WO2008055737A1 Turbine blade
05/15/2008US20080112816 Air-cooled component
05/15/2008US20080112814 Method for the heat treatment of nickel-based superalloys
05/15/2008US20080112812 Propeller blades propelling for all
05/15/2008US20080112811 Hoop seal with partial slot geometry
05/15/2008US20080112809 Highly slenderness rotor
05/15/2008US20080112803 Mechanical support of a ceramic gas turbine vane ring
05/15/2008US20080112795 Dual interstage cooled engine
05/15/2008US20080112793 Interstage cooled turbine engine
05/15/2008DE102007000516A1 Heat shield e.g. stator-sided heat shield, for turbo machine i.e. gas turbine, has discharge opening provided with cross-section at flow direction of turbo machine at opposite or same sided edge area of shield
05/15/2008CA2652708A1 Flow-control technique to vector bulk flow leaving a vane
05/14/2008EP1921324A1 Turbomachine arrow blade
05/14/2008EP1921272A2 Air-cooled aerofoil for a gas turbine engine
05/14/2008EP1921271A2 Titanium foil as a structural heater element
05/14/2008EP1921270A2 Compound nozzle cooled engine
05/14/2008EP1921269A1 Turbine blade
05/14/2008EP1921268A1 Turbine blade
05/14/2008EP1921267A2 Airfoil shape for a compressor
05/14/2008EP1921266A2 Airfoil shape for a compressor
05/14/2008EP1921265A2 Airfoil shape for a compressor
05/14/2008EP1921264A2 Airfoil shape for a compressor
05/14/2008EP1921263A2 Airfoil for a compressor
05/14/2008EP1921262A2 Airfoil shape for a compressor
05/14/2008EP1921261A2 Airfoil shape for a compressor
05/14/2008EP1921260A2 Airfoil shape for a compressor
05/14/2008EP1921259A2 Airfoil shape for a compressor
05/14/2008EP1921258A2 Airfoil shape for a compressor
05/14/2008EP1921257A2 Airfoil shape for a compressor
05/14/2008EP1921256A2 Dual interstage cooled engine
05/14/2008EP1921255A2 Interstage cooled turbine engine
05/14/2008EP1921254A2 Hoop seal with partial slot geometry