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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02/27/2008 | EP1892377A1 Turbomachine blade |
02/27/2008 | EP1892376A1 Cooled steam turbine rotor with inner tube |
02/27/2008 | EP1892375A1 Turbine engine rotor disc with cooling passage |
02/27/2008 | EP1892374A2 Method of repairing shrouded turbine blades with cracks in the vicinity of the outer shroud notch |
02/27/2008 | EP1892091A1 Turbine blade with protective coating and buttering layer |
02/27/2008 | EP1891300A1 Trailing edge attachment for composite airfoil |
02/27/2008 | EP1891249A1 Layer system for a component comprising a thermally insulating layer and a metallic anti-erosion layer, method for the production and method for the operation of a steam turbine |
02/27/2008 | EP1654089B1 Method for producing integrated blade rotors for a gas turbine mounted by capacitor discharge welding |
02/27/2008 | CN201027697Y Compressor machine wheel |
02/27/2008 | CN101133188A Layered matrix and system |
02/27/2008 | CN101131099A Coated turbine blade |
02/27/2008 | CN101131098A 相反尖端挡板翼片 Instead bezel edge flap |
02/27/2008 | CN101131097A 叶片顶部级联挡板翼型 Top blade airfoil cascade baffle |
02/27/2008 | CN101131096A Flared tip turbine blade |
02/27/2008 | CN101131095A 共形叶尖隔板翼型 Conformal tip airfoil baffle |
02/27/2008 | CN101131094A 尖端斜面涡轮机叶片 Beveled tip turbine blades |
02/27/2008 | CN101131093A Blade root platform damping structure of blast furnace gas turbine blade |
02/27/2008 | CN101131092A Methods and apparatus for fabricating a rotor for a steam turbine |
02/27/2008 | CN101130291A Component with a coating system |
02/27/2008 | CN100371126C Repairing method of turbine inlet guiding section |
02/26/2008 | US7335616 Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating |
02/26/2008 | US7334999 Turbomachine rotor including at least one disk reinforced by a composite ring |
02/26/2008 | US7334998 Low-noise fan exit guide vanes |
02/26/2008 | US7334997 Hybrid blisk |
02/26/2008 | US7334996 Device for the positioning of a blade and bladed disk comprising such a device |
02/26/2008 | US7334995 Turbine blade assembly and method of manufacture |
02/26/2008 | US7334993 Gas turbine rotor blade, gas turbine using the rotor blade, and power plant using the gas turbine |
02/26/2008 | US7334992 Turbine blade cooling system |
02/26/2008 | US7334991 Turbine blade tip cooling system |
02/26/2008 | US7334412 Cooling air and injected liquid system for gas turbine blades |
02/26/2008 | US7334333 Method for making a hollow fan blade with machined internal cavities |
02/26/2008 | US7334332 Method of manufacturing a hollow blade for a turbine engine |
02/26/2008 | US7334331 Methods and apparatus for machining components |
02/26/2008 | US7334330 Thermally insulating layer incorporating a distinguishing agent and method for inspecting the same |
02/26/2008 | CA2549313C Blade of a gas turbine |
02/25/2008 | CA2598532A1 Turbomachine rotor blade |
02/25/2008 | CA2597443A1 Vane assembly with improved vane roots |
02/25/2008 | CA2597268A1 Vane assembly with outer grommets |
02/24/2008 | CA2595849A1 Disc firtree slot with truncation for blade attachment |
02/21/2008 | WO2008000014A3 Guide vane arrangement for a driving mechanism |
02/21/2008 | WO2006110156A3 Counter-torque device for a helicopter |
02/21/2008 | US20080044287 Lp turbine blade airfoil profile |
02/21/2008 | US20080044286 Rotor blade of a first phase of a vapor turbine with a fork foot and covering belt |
02/21/2008 | US20080044282 Heat transferring cooling features for an airfoil |
02/21/2008 | DE19857653C5 Laufschaufel einer mehrstufigen Dampfturbine Rotor blade of a multi-stage steam turbine |
02/21/2008 | DE102006038060A1 Blade for turbo machine, comprises current stumbling element, where current is applied along prospective detachment position transversely to required number of current stumbling elements |
02/21/2008 | CA2597654A1 Tip ramp turbine blade |
02/21/2008 | CA2596782A1 Counter tip baffle airfoil |
02/21/2008 | CA2596777A1 Conformal tip baffle airfoil |
02/21/2008 | CA2596764A1 Cascade tip baffle airfoil |
02/20/2008 | EP1890054A1 Ring gear mounting arrangement with oil scavenge scheme |
02/20/2008 | EP1890008A2 Rotor blade |
02/20/2008 | EP1890007A2 High lift transonic turbine blade |
02/20/2008 | EP1890006A1 Rotor with a vibrational damper for a turbomachine |
02/20/2008 | EP1890005A2 Preswirl pollution air handling with tangential on-board injector for turbine rotor cooling |
02/20/2008 | EP1890004A1 Method for the production of a deposited layer from recycled layer material |
02/20/2008 | EP1890002A1 Method for manufacturing a turbomachine and turbomachine |
02/20/2008 | EP1889680A1 Process of welding of turbine components using a ceramic core introduced in an hollow part of the turbine component |
02/20/2008 | EP1888403A2 Rotor hub fairing system for a counter-rotating, coaxial rotor system |
02/20/2008 | CN101128649A Component comprising an embedded channel, in particular a hot gas component of a turbomachine |
02/20/2008 | CN101126327A Turbine blade tail micro-channel inner-cooling structure |
02/20/2008 | CN101126326A Combined cooling structure for turbine blade middle-part round-corner transition impact aerating film |
02/20/2008 | CN101126325A Combined cooling structure for turbine blade middle-part porous impact aerating film |
02/20/2008 | CN101126324A Combined cooling structure for turbine blade middle-part inclined impact aerating film |
02/20/2008 | CN101126323A Rotor for a turbomachine |
02/20/2008 | CN101125753A Dysprosia stabilized zirconia abradable |
02/20/2008 | CN100370113C Steam turbine moving vane shroud structure |
02/19/2008 | US7332123 Method for manufacturing composite articles and the articles obtained therefrom |
02/19/2008 | US7331757 Turbine shaft and production of a turbine shaft |
02/19/2008 | US7331755 Method for coating gas turbine engine components |
02/14/2008 | WO2008017559A1 Method for producing a wear layer |
02/14/2008 | US20080038578 Atomic layer deposition for turbine components |
02/14/2008 | US20080038116 Turbine Blade Tip Shroud |
02/14/2008 | US20080038108 Axial Flow Turbine with Overspeed Preventing Device |
02/14/2008 | DE102006037575A1 Abgasturbolader für eine Brennkraftmaschine und Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine and internal combustion engine |
02/14/2008 | CA2660319A1 Method for producing a useful layer |
02/13/2008 | EP1887187A2 Rotor blade |
02/13/2008 | EP1887186A2 Leading edge cooling with microcircuit anti-coriolis device |
02/13/2008 | EP1886015A1 Water turbine with bi-symmetric airfoil |
02/13/2008 | EP1886000A1 Detection of gas turbine airfoil failure |
02/13/2008 | EP1885999A1 An air intake for a turbocharger for an internal combustion engine |
02/13/2008 | EP1455982B1 Workpiece with a recess which is closed from the exterior by means of a solder film and method for closing a recess by means of a solder film |
02/13/2008 | EP1441874A4 Method for removing coating material from a cooling hole of a gas turbine engine component |
02/13/2008 | CN100368657C Labyrinth seal in a stationary gas turbine |
02/12/2008 | US7329832 Automated adaptive machining of obstructed passages |
02/12/2008 | US7329102 Blade |
02/12/2008 | US7329101 Ceramic composite with integrated compliance/wear layer |
02/12/2008 | US7328580 Chevron film cooled wall |
02/12/2008 | US7328496 Apparatus for rebuilding gas turbine engine blades |
02/12/2008 | CA2373192C Device for controlling air flow in a turbine blade |
02/12/2008 | CA2218692C Turbomachinery and method of manufacturing the same |
02/10/2008 | CA2581033A1 Turbine shroud thermal distortion control |
02/10/2008 | CA2578648A1 Ceramic shroud assembly |
02/07/2008 | WO2008015145A1 Method of analysis of secondary-air circuits in gas-turbine plants |
02/07/2008 | WO2008014776A2 Microporous thermal barrier coating for a gas turbine component |
02/07/2008 | WO2008014568A1 Steam turbine |
02/07/2008 | WO2007147177A3 A blade |
02/07/2008 | WO2007089466A3 Dry running flexible impeller pump and method of manufacture |
02/07/2008 | US20080031739 Airfoil with customized convective cooling |
02/07/2008 | US20080031738 Bell-shaped fan cooling holes for turbine airfoil |