| 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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| 04/07/2009 | US7513738 Methods and apparatus for cooling gas turbine rotor blades |
| 04/07/2009 | US7513737 Gas turbine blade cooling circuit having a cavity with a high aspect ratio |
| 04/07/2009 | US7513114 Exhaust gas turbocharger for a reciprocating internal combustion engine and corresponding reciprocating internal combustion engine |
| 04/07/2009 | CA2422000C A lead-in structure and a fixing flange for a turbo generator |
| 04/07/2009 | CA2395211C Viscous drag impeller components incorporated into pumps, turbines and transmissions |
| 04/07/2009 | CA2378101C Cooled airfoil |
| 04/02/2009 | WO2009042157A2 Integral single crystal/columnar grained component and method of casting the same |
| 04/02/2009 | WO2009039835A1 Flow structure for a turbocompressor |
| 04/02/2009 | WO2008076724A3 Method of forming yttrium-modified platinum aluminide diffusion coating |
| 04/02/2009 | US20090087572 Gas turbines; intermetallics comprised of aluminum, nickel, and platinum; vapor deposition; heat treatment; electrodeposition |
| 04/02/2009 | US20090087316 Rotor blade, method for producing a rotor blade, and compressor with a rotor blade |
| 04/02/2009 | US20090087313 Aircraft turbomachine fan comprising a balancing flange concealed by the inlet cone |
| 04/02/2009 | US20090087312 Turbine Airfoil Concave Cooling Passage Using Dual-Swirl Flow Mechanism and Method |
| 04/02/2009 | DE102008044501A1 Verbundschaufelblatt Composite airfoil |
| 04/02/2009 | DE102008044500A1 Verfahren zur Herstellung eines Verbundschaufelblattes A method for producing a composite airfoil |
| 04/02/2009 | DE102008037391A1 Turbine blade for gas turbine engine, has set of cooling channels extending between foot section and tip section of blade leaf, where channels are positioned in curve line pattern and each channel passes to tip section |
| 04/02/2009 | DE102008037384A1 Konkaver Turbinenschaufel-Kühlkanal unter Verwendung eines Doppelwirbelströmungsmechanismus und Verfahren dafür Concave turbine blade cooling channel using a double vortex flow mechanism and method therefor |
| 04/02/2009 | DE102007043791A1 Verfahren zur Herstellung einer Wärmedämmschicht und Wärmedämmschicht A process for producing a thermal barrier coating and thermal barrier coating |
| 04/01/2009 | EP2042689A1 Shim for a blade of a turbomachine |
| 04/01/2009 | EP2042618A1 Method for recovering turbine engine components |
| 04/01/2009 | EP2041400A1 Turbocharger having a catalytic coating |
| 04/01/2009 | EP2041398A2 Rotor for a compressor |
| 04/01/2009 | EP2041397A1 Reduction of flexural vibration amplitudes of turbine rotors |
| 04/01/2009 | EP2040876A1 Method for repairing turbine blades |
| 04/01/2009 | EP1444418B1 Internal cooled gas turbine vane or blade |
| 04/01/2009 | CN101397918A Shim for a blade of a turbomachine |
| 04/01/2009 | CN101397917A Air-cooled bland for turbine |
| 04/01/2009 | CN101397916A Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method |
| 04/01/2009 | CN100473806C Turbomachine having compact rolling bearing assembly |
| 04/01/2009 | CA2640028A1 Rotor blade, method for producing a rotor blade, and also compressor with such a rotor blade |
| 03/31/2009 | US7510779 Low-sulfur article having a platinum aluminide protective layer and its preparation |
| 03/31/2009 | US7510778 Part for protecting the leading edge of a blade |
| 03/31/2009 | US7510380 Non-parallel spacer for improved rotor group balance |
| 03/31/2009 | US7510378 Airfoil shape for a compressor |
| 03/31/2009 | US7510376 Skewed tip hole turbine blade |
| 03/31/2009 | US7510375 Method of coating and a shield for a component |
| 03/31/2009 | US7510372 Wedge repair of mechanically retained vanes |
| 03/31/2009 | US7510370 Turbine blade tip and shroud clearance control coating system |
| 03/31/2009 | US7509736 Process for repairing metallic pieces especially turbine blades of a gas turbine motor |
| 03/31/2009 | US7509735 In-frame repairing system of gas turbine components |
| 03/31/2009 | US7509734 Repairing turbine element |
| 03/31/2009 | CA2340932C Turbine rotor modernization and repair method |
| 03/26/2009 | WO2009038749A1 Imparting functional characteristics to engine portions |
| 03/26/2009 | WO2009038743A1 Bimetallic bond layer for thermal barrier coating on superalloy |
| 03/26/2009 | WO2009012747A3 Method of repair |
| 03/26/2009 | WO2009006871A3 Turbomachine blade with weaar-resistant layer |
| 03/26/2009 | US20090081048 Turbine Blade for a Turbine |
| 03/26/2009 | US20090081046 Shim for a turbomachine blade |
| 03/26/2009 | US20090081044 Polygon rotor attachment device |
| 03/26/2009 | US20090081032 Composite airfoil |
| 03/26/2009 | US20090081024 Turbine blade |
| 03/26/2009 | US20090078390 Integral Single Crystal/Columnar Grained Component and Method of Casting the Same |
| 03/26/2009 | CA2639960A1 Method of recuperating turbine elements |
| 03/25/2009 | EP2039884A1 Ceramic matrix composite turbine engine vane |
| 03/25/2009 | EP2039883A2 Methods for repairing gas turbine engine components |
| 03/25/2009 | EP2039882A2 Methods for performing gas turbine engine casing repairs and repaired cases |
| 03/25/2009 | EP2039459A1 Method for joining metallic compounds and device for executing an inductive low or high frequency welding procedure |
| 03/25/2009 | EP2038605A1 Measurement of aerofoil blades |
| 03/25/2009 | CN201212404Y Impeller wheel of steam turbine |
| 03/25/2009 | CN101392661A Method for making a composite airfoil |
| 03/25/2009 | CN101392660A Composite airfoil |
| 03/25/2009 | CN100472055C Methods and apparatus for assembling gas turbine engines |
| 03/25/2009 | CN100472033C A rotor blade for a gas turbine engine |
| 03/25/2009 | CA2640003A1 Foil for turbomachine blade |
| 03/24/2009 | US7507306 An Fe Ni Cr alloy formulated to contain a strengthening phase that is able to maintain a fine grain structure during forging and high temperature processing of the alloy. The alloy contains a sufficient amount of titanium, zirconium, carbon and nitrogen so that fine titanium and zirconium carbonitride |
| 03/24/2009 | US7507075 Mistake proof identification feature for turbine blades |
| 03/24/2009 | US7507073 Methods and apparatus for assembling a steam turbine bucket |
| 03/24/2009 | US7507072 Turbine module for a gas-turbine engine with rotor that includes a monoblock body |
| 03/24/2009 | US7507071 Cooling arrangement |
| 03/24/2009 | US7507070 Gas turbine engine and a rotor for a gas turbine engine |
| 03/24/2009 | CA2639724A1 Method for forming raised areas to disrupt boundary layer |
| 03/19/2009 | WO2009035380A1 A method of producing a rotor component or a stator component |
| 03/19/2009 | WO2008010200A3 Flow deflection devices and method for energy capture machines |
| 03/19/2009 | US20090074589 Cooling Circuit for Enhancing Turbine Performance |
| 03/19/2009 | US20090074588 Airfoil with cooling hole having a flared section |
| 03/19/2009 | US20090074586 Damping device for composite blade |
| 03/19/2009 | US20090074585 Wind turbine blades with trailing edge serrations |
| 03/19/2009 | US20090074582 Method for joining metal components and device for execution of an inductive low or high-frequency pressure welding method |
| 03/19/2009 | US20090074580 Radial turbine wheel structure |
| 03/19/2009 | US20090074579 Turbine ring |
| 03/19/2009 | US20090074578 Turbine and compressor employing tubercle leading edge rotor design |
| 03/19/2009 | US20090074576 Turbine blade with cooling breakout passages |
| 03/19/2009 | US20090074575 Cooling circuit flow path for a turbine section airfoil |
| 03/19/2009 | US20090072010 Joining method and resultant article |
| 03/19/2009 | CA2686702A1 Method and system for turbine blade characterization |
| 03/19/2009 | CA2639589A1 Control device for the tangential dimples of a rotor disk |
| 03/18/2009 | EP2037126A1 Tubofan engine |
| 03/18/2009 | EP2037083A2 Seal for gas turbine engine component |
| 03/18/2009 | EP2037082A1 Damping device for a composite blade |
| 03/18/2009 | EP2037081A1 Platform cooling structure of gas turbine rotor blade |
| 03/18/2009 | EP2036657A2 Method of repairing a turbine engine component |
| 03/18/2009 | EP2036646A1 Method of repairing a turbine engine component |
| 03/18/2009 | EP2035692A1 Sealing means between rotor and housing in a water turbine |
| 03/18/2009 | EP2035669A1 Secondary ventilation system for turbocharger turbine |
| 03/18/2009 | EP2035658A2 Guide vane arrangement for a driving mechanism |
| 03/18/2009 | EP2035179A1 Friction welding of a single crystal component to a second component with minimisation of in plane friction and forge forces |
| 03/18/2009 | EP1902160B1 Ceramic heat insulating layer |
| 03/18/2009 | EP1825105B1 A wheel for a rotating flow machine |
| 03/18/2009 | EP1625291B1 Turbo compressor system for an internal combustion engine comprising a compressor of radial type and provides with an impeller with backswept blades |
| 03/18/2009 | CN201209463Y Frequency non-modulation moving blade suitable for blast furnace gas energy recovery and turbining |