| 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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| 05/14/2008 | EP1921007A2 A turbine engine mounting arrangement |
| 05/14/2008 | EP1920871A1 Integrally bladed rotor having an MMC ring component and an airfoil component having monolithic airfoils |
| 05/14/2008 | EP1920870A1 Integrally bladed rotor having an mmc ring component and a unitary airfoil component |
| 05/14/2008 | EP1920869A1 Integrally bladed rotor having an MMC ring component and an airfoil component having MMC airfoils |
| 05/14/2008 | EP1919846A2 Refractory component with ceramic matrix composite skeleton |
| 05/14/2008 | EP1756406B1 Gas turbine compression system and compressor structure |
| 05/14/2008 | CN101178015A Integrally bladed rotor having an mmc ring component and an airfoil component having monolithic airfoils |
| 05/14/2008 | CN101178014A Dual interstage cooled engine |
| 05/14/2008 | CN101178013A 复合式喷嘴冷却的发动机 Composite nozzle cooled engine |
| 05/14/2008 | CN101178012A Turbomachine arrow blade |
| 05/14/2008 | CN101178011A Impeller structure of centripetal turbine |
| 05/13/2008 | US7371426 lower growth environmental bond coating of an aluminum alloy applied to the remaining base metal substrate so that upon subsequent repair of the component, less of the remaining base metal substrate is removed because of less environmental coating growth into the substrate than prior bond coat |
| 05/13/2008 | US7371050 Device for axially retaining blades on a turbomachine rotor disk |
| 05/13/2008 | US7371049 Manufacturable and inspectable microcircuit cooling for blades |
| 05/13/2008 | US7371048 Turbine blade trailing edge construction |
| 05/13/2008 | US7370787 Compressor rotor and method for making |
| 05/13/2008 | US7370467 Turbofan case and method of making |
| 05/10/2008 | CA2607878A1 Compound nozzle cooled engine |
| 05/10/2008 | CA2607654A1 Interstage cooled turbine engine |
| 05/08/2008 | WO2008053635A1 Transonic airfoil and axial flow rotary machine |
| 05/08/2008 | WO2008052846A1 Turbine blade |
| 05/08/2008 | WO2008031413A3 Maintenance planning method for turbomachines |
| 05/08/2008 | WO2007107388A3 Thermal insulation layer system |
| 05/08/2008 | US20080107541 Refractory metal core main body trench |
| 05/08/2008 | US20080107540 Damping element for a wind turbine rotor blade |
| 05/08/2008 | US20080107539 Impeller manufacturing method and impeller |
| 05/08/2008 | US20080107538 swept turbomachine blade |
| 05/08/2008 | US20080107537 Airfoil shape for a compressor |
| 05/08/2008 | US20080107536 Airfoil shape for a compressor |
| 05/08/2008 | US20080107535 Airfoil shape for a compressor |
| 05/08/2008 | US20080107534 Airfoil shape for a compressor |
| 05/08/2008 | US20080107533 System for manufacturing a rotor having an mmc ring component and a unitary airfoil component |
| 05/08/2008 | US20080107532 System for manufacturing a rotor having an mmc ring component and an airfoil component having mmc airfoils |
| 05/08/2008 | US20080107531 System for manufacturing a rotor having an mmc ring component and an airfoil component having monolithic airfoils |
| 05/08/2008 | US20080107530 Coupling device for a turbine upstream guide vane, a turbine comprising same, and aircraft engine fitted therewith |
| 05/08/2008 | US20080107529 Fan blade connector component with skeleton and method of manufacturing such |
| 05/08/2008 | US20080107519 Turbine blade for a gas turbine |
| 05/08/2008 | DE102007049498A1 Feingussverfahren und -vorrichtung zur Erzielung einer besseren Kornstruktur in einer gerichtet erstarrten Turbinenlaufschaufel mit Deckband Precision casting method and apparatus for achieving a better grain structure oriented in a solidified turbine blade with shroud |
| 05/08/2008 | DE102006051813A1 Schaufel für einen Verdichter oder eine Turbine eines Flugtriebwerks, Flugtriebwerk mit einer solchen Schaufel sowie Verfahren zum Beschichten einer Schaufel eines Flugtriebwerks Bucket for a compressor or turbine aircraft engine, aircraft engine with such a blade and method for coating a blade of an aircraft engine |
| 05/08/2008 | CA2610278A1 Turbojet arrow blade |
| 05/07/2008 | EP1918590A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918547A2 Gas turbine production process |
| 05/07/2008 | EP1918525A2 Gas turbine engine seal and corresponding passive sealing clearance control system |
| 05/07/2008 | EP1918523A2 Turbine and rotor blade with brush seal |
| 05/07/2008 | EP1918522A2 Turbine component |
| 05/07/2008 | EP1918521A2 Compressor stator vane with variable pitch having an extended fillet |
| 05/07/2008 | EP1918520A2 Plasma lifted boundary layer on a gas turbine engine vane |
| 05/07/2008 | EP1918519A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918518A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918517A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918516A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918515A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918514A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918513A2 Airfoil shape for a compressor |
| 05/07/2008 | EP1918512A2 Balancing system for a turbomachine rotor |
| 05/07/2008 | EP1918511A2 Balancing system for a turbomachine rotor |
| 05/07/2008 | EP1918093A1 Surface treatment for a thin titanium foil |
| 05/07/2008 | EP1917419A2 Guide vane arrangement of a turbo-machine |
| 05/07/2008 | EP1704260B1 Component with internal compressive stress, method for producing said component and device for generating internal compressive stress |
| 05/07/2008 | EP1200217B1 Directional solidification method and apparatus |
| 05/07/2008 | CN101173611A Blade/disk dovetail backcut for blade/disk stress reduction (9FA, stage 1) |
| 05/07/2008 | CN101173610A Heated wall surface cooling structure and gas turbine impeller vane with the same |
| 05/07/2008 | CN101173349A Method for forming anti-corrosion and anti-oxidation coating layer on high-temperature components of gas turbine fuel additive |
| 05/07/2008 | CN100386503C Method for testing a component in a non-destructive manner and for producing a gas turbine blade |
| 05/07/2008 | CN100386502C Steam/gas turbine with improved housing or sealing member |
| 05/06/2008 | US7368177 Highly oxidation resistant component |
| 05/06/2008 | US7367779 LP turbine vane airfoil profile |
| 05/06/2008 | US7367778 Rotor end piece |
| 05/06/2008 | US7367775 Apparatus and method for optimizing vibration of a gas turbine |
| 05/06/2008 | US7367774 System for protecting a main shaft of an engine having a fusible bearing |
| 05/02/2008 | WO2008051751A2 Impeller for centrifugal pump |
| 05/02/2008 | WO2008049677A1 Turbine blade assembly |
| 05/02/2008 | WO2008049465A1 Method for production of turbine blades by centrifugal casting |
| 05/02/2008 | WO2008049460A1 Method for adjusting the surface roughness in a low temperature coating method, and component |
| 05/02/2008 | WO2008049456A1 Coating optimization process using a coupon and component comprising a coupon |
| 05/02/2008 | WO2008049442A1 Method for production of precision castings by centrifugal casting |
| 05/01/2008 | US20080101961 Turbine airfoil cooling system with spanwise equalizer rib |
| 05/01/2008 | US20080101939 Blade/disk dovetail backcut for blade/disk stress reduction (7FA, stage 2) |
| 05/01/2008 | US20080101938 Blade/disk dovetail backcut for blade/disk stress reduction (7FA, stage 1) |
| 05/01/2008 | US20080101937 Blade/disk dovetail backcut for blade/disk stress reduction (9FA, stage 1) |
| 05/01/2008 | US20080101933 Airflow generating apparatus |
| 05/01/2008 | US20080101921 Impeller for centrifugal pump |
| 04/30/2008 | EP1916389A1 Turbine blade assembly |
| 04/30/2008 | EP1916388A2 Vane with enhanced heat transfer |
| 04/30/2008 | EP1916387A2 Airfoil shape for a compressor |
| 04/30/2008 | EP1916386A2 Airfoil shape for a compressor |
| 04/30/2008 | EP1916385A1 Sponson of fan platform |
| 04/30/2008 | EP1916384A2 Airfoil shape for a compressor |
| 04/30/2008 | EP1916383A2 Airfoil shape for a compressor |
| 04/30/2008 | EP1916382A1 Device and method for securing a sealing element on a rotor |
| 04/30/2008 | EP1916051A1 Method of repairing an aperture and defect in a part with welding using an insert with top and runoff plates and backing |
| 04/30/2008 | EP1915514A1 Wind turbine blade |
| 04/30/2008 | DE102007051417A1 Gas turbine engine arrangement, particularly turbine blade for rotating blade, has uncoated profile that is corresponding to cartesian coordinate values of X, Y and Z according to description in certain table |
| 04/30/2008 | DE102007051413A1 Guiding device for turbine i.e. gas turbine, has turbine blade including nominal profile based on Cartesian coordinate values X, Y and Z, where profiles flowing in z-distances are connected with one another to form turbine blade shape |
| 04/30/2008 | DE102007051096A1 Stress reducing method for gas turbine engine's disk and blade, involves optimizing start point and cut angle based on blade and disk geometry, and positioning datum line at fixed distance from face of dovetail along centerline of axis |
| 04/30/2008 | DE102007050918A1 Turbine components have erosion-resistant coating applied using electron beam physical vapor deposition or ion plasma arc coating |
| 04/30/2008 | DE102007050917A1 Voltage reduction method either on turbine disk or on turbine blade or on both, involves fixing number of turbine blade, and determining initial point for dovetail making location in relation to reference line |
| 04/30/2008 | DE102006050440A1 Lightweight structure-turbine blade manufacturing method, involves casting blade unit with blade wall and hollow space surrounding blade wall, where blade unit extends radially from floor area to head area |
| 04/30/2008 | DE102006049616A1 Aerodynamic component has slits at the trailing edge, running between the upper and lower main surfaces, to reduce air turbulence noise emissions |
| 04/30/2008 | DE102006049219A1 Hochdruckturbinen-Schaufel und Verfahren zur Reparatur von Hochdruckturbinen-Schaufeln High-pressure turbine blade and method of repairing high pressure turbine blades |