Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
10/2006
10/31/2006US7128528 Bearings for CO2 refrigerant compressor use, compressor using the same, and applications of the same
10/31/2006US7128524 Ventilating structure and mounting structure for electronic apparatus
10/26/2006WO2006111520A1 Turbine rotor and turbine engine
10/26/2006US20060240273 Member coated with thermal barrier coating film and thermal spraying powder
10/26/2006US20060239852 Nickel alloy composition
10/26/2006US20060239822 Apparatus and method for anchoring a rotor blade in a rotor of a turbo machine
10/26/2006US20060239820 Member having internal cooling passage
10/26/2006US20060239819 Airfoil trailing edge cooling
10/26/2006DE10323132B4 Verstellbare Leitschaufel und Verfahren zur Herstellung derselben Adjustable vane and process for producing same
10/25/2006EP1715141A2 Device for the control of an air flow flowing in a rotor shaft of a turbine
10/25/2006EP1715139A2 Airfoil trailing edge cooling
10/25/2006EP1715081A1 Alloy coating for diffusion barrier, method for forming same, and high-temperature device member
10/25/2006EP1714008A1 Cambered vane for use in turbochargers
10/25/2006EP1714006A1 Damping arrangement for guide vanes
10/25/2006EP1350018B1 Combustor turbine successive dual cooling
10/25/2006CN2830646Y Secondary-final stage vane of large-scale top speed turbine
10/25/2006CN1851239A 翼型后缘冷却 Airfoil trailing edge cooling
10/24/2006US7125457 Method for removing oxide from cracks in turbine components
10/24/2006US7125227 Process for manufacturing or repairing a monobloc bladed disc
10/24/2006US7125225 Cooled rotor blade with vibration damping device
10/24/2006US7125220 Axial-flow type fan having an air outlet blade structure
10/24/2006CA2172070C Protective coating
10/19/2006WO2006110156A2 Counter-torque device for a helicopter
10/19/2006WO2006110125A2 Stacked annular components for turbine engines
10/19/2006WO2006108764A1 Convectively cooled gas turbine blade
10/19/2006WO2006108749A1 Component with film cooling holes
10/19/2006WO2006108746A1 Component of a steam turbine installation, steam turbine installation, use thereof and method for producing the same
10/19/2006WO2006108454A1 Guide vane support
10/19/2006US20060233647 Slotted bladeless turbine disc
10/19/2006US20060233646 Fan wheel
10/19/2006US20060233644 Stator turbine vane with improved cooling
10/19/2006US20060231123 Method for removing a layer area of a component
10/19/2006DE19547171B4 Ausgleichskupplung Flexible coupling
10/19/2006DE102004006775A1 Wirbelgleichrichter in Röhrenbauweise Vortex rectifier tube-type
10/19/2006CA2574108A1 Counter-torque device for a helicopter
10/18/2006EP1712745A1 Component of a steam turbine plant, steam turbine plant, use and production method of such a component.
10/18/2006EP1712741A2 Turbine nozzle retention key and turbine nozzle vane carrier
10/18/2006EP1712740A1 Blade for a turbo machine and turbo machine with a number of blades
10/18/2006EP1712739A1 Component with film cooling hole
10/18/2006EP1712738A2 Low solidity turbofan
10/18/2006EP1712737A1 Crescentic ramp turbine stage
10/18/2006EP1712736A2 Repaired spline and seal teeth on mated components
10/18/2006EP1712735A2 Method of repairing spline and seal teeth of a mated component
10/18/2006EP1712325A1 Overlay for repairing spline and seal teeth of a mated component comprising a tube and internal slines
10/18/2006EP1712324A1 Weld prep joint assembly with interference fit for electron beam or laser welding ; Method of welding such assembly
10/18/2006EP1711688A2 Mitigation of unsteady peak fan blade and disc stresses in turbofan engines through the use of flow control devices to stabilize boundary layer characteristics
10/18/2006EP1711339A2 Durable thermal barrier coating having low thermal conductivity
10/18/2006EP1711302A1 Method for connecting components
10/18/2006EP1711298A1 Process of brazing repairing of a part having a base material with oriented microstructure
10/18/2006CN2828322Y Final stage, penultimate vane of large full speed steam turbine
10/18/2006CN2828321Y Penultimate vane of large air-cooling steam turbine
10/18/2006CN2828320Y Steam turbine large enthalpy drop reaction moving vane
10/18/2006CN1849439A Cooled blade for a gas turbine
10/18/2006CN1847623A Crescentic ramp turbine stage
10/18/2006CN1847428A Protective part for the leading edge of a blade
10/17/2006US7121806 Welding method and an assembly formed thereby
10/17/2006US7121805 Electric fan with detachable blades
10/17/2006US7121803 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
10/17/2006US7121802 Selectively thinned turbine blade
10/17/2006US7121801 Cooled rotor blade with vibration damping device
10/17/2006US7121800 Turbine blade nested seal damper assembly
10/17/2006US7121798 Radial fan wheel for transporting cooling air for an electric machine
10/17/2006US7121797 Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine
10/17/2006US7121796 Nozzle-cooling insert assembly with cast-in rib sections
10/17/2006US7121792 Nozzle vane with two slopes
10/17/2006US7121787 Turbine nozzle trailing edge cooling configuration
10/17/2006CA2292380C Coating of a discrete selective surface of an article
10/17/2006CA2230291C Cooling structure to cool platform for drive blades of gas turbine
10/15/2006CA2543226A1 Protective part for the leading edge of a blade
10/14/2006CA2535205A1 Crescentic ramp turbine stage
10/13/2006CA2542057A1 Weld prep joint for electron beam or laser welding
10/12/2006WO2006106061A1 Method for repairing or renewing cooling holes of a coated component of a gas turbine
10/12/2006WO2006105891A1 Friction welding method and components produced from steel and metal aluminide using an intermediary from an ni alloy
10/12/2006US20060229759 Parametric production of drilled cooling holes
10/12/2006US20060228475 Oxidation resistant coatings for ultra high temperature transition metals and transition metal alloys
10/12/2006US20060228219 Repaired spline and seal teeth on mated components
10/12/2006US20060228217 Steam turbine rotors
10/12/2006US20060228216 Rotor for a compressor
10/12/2006US20060228210 Compressor rotor
10/12/2006US20060228208 Method and apparatus for distributing fluid into a turbomachine
10/12/2006DE102005016035A1 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
10/12/2006CA2602628A1 Method for repairing or renewing cooling holes of a coated component of a gas turbine
10/11/2006EP1710397A2 Bowed nozzle vane
10/11/2006EP1710395A2 Axial turbine
10/11/2006EP1709299A1 Gas turbine engine including airfoils having an improved airfoil film cooling configuration and method therefor
10/11/2006EP1709298A1 Cooled blade for a gas turbine
10/11/2006EP1709297A1 Disk of a disk rotor for a gas turbine
10/11/2006EP1708846A1 Method for repairing a component of a turbomachine
10/11/2006EP1636462B1 Blade and gas turbine
10/11/2006EP1561007B1 Variable nozzle for turbocharger
10/11/2006EP1386060B1 Turbine or compressor device and method for assembling the device
10/11/2006EP1373684B1 Environmental and thermal barrier coating for ceramic components
10/11/2006EP1322838B1 Moving blade for a turbo-machine and turbo-machine
10/11/2006EP1287234B1 Device for controlling the cooling flows of gas turbines
10/11/2006CN1846067A Turbocharger compressor wheel having a counterbore treated for enhanced endurance to stress-induced fatigue and configurable to provide a compact axial length
10/10/2006US7118636 Precipitation-strengthened nickel-iron-chromium alloy
10/10/2006US7118464 Apparatus for smoothing the surface of a gas turbine blade
10/10/2006US7118346 Compressor blade
10/10/2006US7118343 Trailing edge adjustable weight system for helicopter main rotor blades
10/10/2006US7118342 Fluted tip turbine blade