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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10/31/2006 | US7128528 Bearings for CO2 refrigerant compressor use, compressor using the same, and applications of the same |
10/31/2006 | US7128524 Ventilating structure and mounting structure for electronic apparatus |
10/26/2006 | WO2006111520A1 Turbine rotor and turbine engine |
10/26/2006 | US20060240273 Member coated with thermal barrier coating film and thermal spraying powder |
10/26/2006 | US20060239852 Nickel alloy composition |
10/26/2006 | US20060239822 Apparatus and method for anchoring a rotor blade in a rotor of a turbo machine |
10/26/2006 | US20060239820 Member having internal cooling passage |
10/26/2006 | US20060239819 Airfoil trailing edge cooling |
10/26/2006 | DE10323132B4 Verstellbare Leitschaufel und Verfahren zur Herstellung derselben Adjustable vane and process for producing same |
10/25/2006 | EP1715141A2 Device for the control of an air flow flowing in a rotor shaft of a turbine |
10/25/2006 | EP1715139A2 Airfoil trailing edge cooling |
10/25/2006 | EP1715081A1 Alloy coating for diffusion barrier, method for forming same, and high-temperature device member |
10/25/2006 | EP1714008A1 Cambered vane for use in turbochargers |
10/25/2006 | EP1714006A1 Damping arrangement for guide vanes |
10/25/2006 | EP1350018B1 Combustor turbine successive dual cooling |
10/25/2006 | CN2830646Y Secondary-final stage vane of large-scale top speed turbine |
10/25/2006 | CN1851239A 翼型后缘冷却 Airfoil trailing edge cooling |
10/24/2006 | US7125457 Method for removing oxide from cracks in turbine components |
10/24/2006 | US7125227 Process for manufacturing or repairing a monobloc bladed disc |
10/24/2006 | US7125225 Cooled rotor blade with vibration damping device |
10/24/2006 | US7125220 Axial-flow type fan having an air outlet blade structure |
10/24/2006 | CA2172070C Protective coating |
10/19/2006 | WO2006110156A2 Counter-torque device for a helicopter |
10/19/2006 | WO2006110125A2 Stacked annular components for turbine engines |
10/19/2006 | WO2006108764A1 Convectively cooled gas turbine blade |
10/19/2006 | WO2006108749A1 Component with film cooling holes |
10/19/2006 | WO2006108746A1 Component of a steam turbine installation, steam turbine installation, use thereof and method for producing the same |
10/19/2006 | WO2006108454A1 Guide vane support |
10/19/2006 | US20060233647 Slotted bladeless turbine disc |
10/19/2006 | US20060233646 Fan wheel |
10/19/2006 | US20060233644 Stator turbine vane with improved cooling |
10/19/2006 | US20060231123 Method for removing a layer area of a component |
10/19/2006 | DE19547171B4 Ausgleichskupplung Flexible coupling |
10/19/2006 | DE102004006775A1 Wirbelgleichrichter in Röhrenbauweise Vortex rectifier tube-type |
10/19/2006 | CA2574108A1 Counter-torque device for a helicopter |
10/18/2006 | EP1712745A1 Component of a steam turbine plant, steam turbine plant, use and production method of such a component. |
10/18/2006 | EP1712741A2 Turbine nozzle retention key and turbine nozzle vane carrier |
10/18/2006 | EP1712740A1 Blade for a turbo machine and turbo machine with a number of blades |
10/18/2006 | EP1712739A1 Component with film cooling hole |
10/18/2006 | EP1712738A2 Low solidity turbofan |
10/18/2006 | EP1712737A1 Crescentic ramp turbine stage |
10/18/2006 | EP1712736A2 Repaired spline and seal teeth on mated components |
10/18/2006 | EP1712735A2 Method of repairing spline and seal teeth of a mated component |
10/18/2006 | EP1712325A1 Overlay for repairing spline and seal teeth of a mated component comprising a tube and internal slines |
10/18/2006 | EP1712324A1 Weld prep joint assembly with interference fit for electron beam or laser welding ; Method of welding such assembly |
10/18/2006 | EP1711688A2 Mitigation of unsteady peak fan blade and disc stresses in turbofan engines through the use of flow control devices to stabilize boundary layer characteristics |
10/18/2006 | EP1711339A2 Durable thermal barrier coating having low thermal conductivity |
10/18/2006 | EP1711302A1 Method for connecting components |
10/18/2006 | EP1711298A1 Process of brazing repairing of a part having a base material with oriented microstructure |
10/18/2006 | CN2828322Y Final stage, penultimate vane of large full speed steam turbine |
10/18/2006 | CN2828321Y Penultimate vane of large air-cooling steam turbine |
10/18/2006 | CN2828320Y Steam turbine large enthalpy drop reaction moving vane |
10/18/2006 | CN1849439A Cooled blade for a gas turbine |
10/18/2006 | CN1847623A Crescentic ramp turbine stage |
10/18/2006 | CN1847428A Protective part for the leading edge of a blade |
10/17/2006 | US7121806 Welding method and an assembly formed thereby |
10/17/2006 | US7121805 Electric fan with detachable blades |
10/17/2006 | US7121803 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge |
10/17/2006 | US7121802 Selectively thinned turbine blade |
10/17/2006 | US7121801 Cooled rotor blade with vibration damping device |
10/17/2006 | US7121800 Turbine blade nested seal damper assembly |
10/17/2006 | US7121798 Radial fan wheel for transporting cooling air for an electric machine |
10/17/2006 | US7121797 Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine |
10/17/2006 | US7121796 Nozzle-cooling insert assembly with cast-in rib sections |
10/17/2006 | US7121792 Nozzle vane with two slopes |
10/17/2006 | US7121787 Turbine nozzle trailing edge cooling configuration |
10/17/2006 | CA2292380C Coating of a discrete selective surface of an article |
10/17/2006 | CA2230291C Cooling structure to cool platform for drive blades of gas turbine |
10/15/2006 | CA2543226A1 Protective part for the leading edge of a blade |
10/14/2006 | CA2535205A1 Crescentic ramp turbine stage |
10/13/2006 | CA2542057A1 Weld prep joint for electron beam or laser welding |
10/12/2006 | WO2006106061A1 Method for repairing or renewing cooling holes of a coated component of a gas turbine |
10/12/2006 | WO2006105891A1 Friction welding method and components produced from steel and metal aluminide using an intermediary from an ni alloy |
10/12/2006 | US20060229759 Parametric production of drilled cooling holes |
10/12/2006 | US20060228475 Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys |
10/12/2006 | US20060228219 Repaired spline and seal teeth on mated components |
10/12/2006 | US20060228217 Steam turbine rotors |
10/12/2006 | US20060228216 Rotor for a compressor |
10/12/2006 | US20060228210 Compressor rotor |
10/12/2006 | US20060228208 Method and apparatus for distributing fluid into a turbomachine |
10/12/2006 | DE102005016035A1 Turbinenrad für ein gasbetriebenes medizinisches Handstück und medizinisches Handstück mit einem Turbinenrad sowie Verfahren zum Fräsen einer Schaufel des Turbinenrads Turbine for a gas-driven medical handpiece and medical handpiece with a turbine and method for milling a blade of the turbine wheel |
10/12/2006 | CA2602628A1 Method for repairing or renewing cooling holes of a coated component of a gas turbine |
10/11/2006 | EP1710397A2 Bowed nozzle vane |
10/11/2006 | EP1710395A2 Axial turbine |
10/11/2006 | EP1709299A1 Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor |
10/11/2006 | EP1709298A1 Cooled blade for a gas turbine |
10/11/2006 | EP1709297A1 Disk of a disk rotor for a gas turbine |
10/11/2006 | EP1708846A1 Method for repairing a component of a turbomachine |
10/11/2006 | EP1636462B1 Blade and gas turbine |
10/11/2006 | EP1561007B1 Variable nozzle for turbocharger |
10/11/2006 | EP1386060B1 Turbine or compressor device and method for assembling the device |
10/11/2006 | EP1373684B1 Environmental and thermal barrier coating for ceramic components |
10/11/2006 | EP1322838B1 Moving blade for a turbo-machine and turbo-machine |
10/11/2006 | EP1287234B1 Device for controlling the cooling flows of gas turbines |
10/11/2006 | CN1846067A Turbocharger compressor wheel having a counterbore treated for enhanced endurance to stress-induced fatigue and configurable to provide a compact axial length |
10/10/2006 | US7118636 Precipitation-strengthened nickel-iron-chromium alloy |
10/10/2006 | US7118464 Apparatus for smoothing the surface of a gas turbine blade |
10/10/2006 | US7118346 Compressor blade |
10/10/2006 | US7118343 Trailing edge adjustable weight system for helicopter main rotor blades |
10/10/2006 | US7118342 Fluted tip turbine blade |