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