| 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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| 08/15/2013 | US20130209270 Method for reconditioning a blade of a gas turbine and also a reconditioned blade |
| 08/15/2013 | US20130209269 Gas turbine engine component with multi-lobed cooling hole |
| 08/15/2013 | US20130209268 Gas turbine blade |
| 08/15/2013 | US20130209267 Rotor |
| 08/15/2013 | US20130209266 Superalloy Compositions, Articles, and Methods of Manufacture |
| 08/15/2013 | US20130209265 Superalloy Compositions, Articles, and Methods of Manufacture |
| 08/15/2013 | US20130209264 Wind turbine rotor blade assembly with root extension panel and method of assembly |
| 08/15/2013 | US20130209263 Blade for a Wind Turbine |
| 08/15/2013 | US20130209261 Assembly of a Blade and a Composite Carrier, Obtained by Sealing |
| 08/15/2013 | US20130209259 Blade group arrangement as well as turbomachine |
| 08/15/2013 | US20130209258 Tip shrouded blade |
| 08/15/2013 | US20130209257 Blade for a Wind Turbine |
| 08/15/2013 | US20130209253 Turbine assembly |
| 08/15/2013 | US20130209240 Adjustable blade outer air seal apparatus |
| 08/15/2013 | US20130209236 Gas turbine engine component with compound cusp cooling configuration |
| 08/15/2013 | US20130209235 Gas turbine engine component with cusped, lobed cooling hole |
| 08/15/2013 | US20130209234 Multiple diffusing cooling hole |
| 08/15/2013 | US20130209233 Cooling hole with enhanced flow attachment |
| 08/15/2013 | US20130209232 Multi-lobed cooling holes in gas turbine engine components having thermal barrier coatings |
| 08/15/2013 | US20130209229 Gas turbine engine component with converging/diverging cooling passage |
| 08/15/2013 | US20130209228 Gas turbine engine component with cusped cooling hole |
| 08/15/2013 | US20130209227 Gas turbine engine component with diffusive cooling hole |
| 08/15/2013 | US20130205792 Cooling hole with asymmetric diffuser |
| 08/15/2013 | US20130205791 Cooling hole with curved metering section |
| 08/15/2013 | US20130205790 Multi-lobed cooling hole and method of manufacture |
| 08/15/2013 | US20130205787 Tri-lobed cooling hole and method of manufacture |
| 08/15/2013 | US20130205786 Cooling hole with thermo-mechanical fatigue resistance |
| 08/14/2013 | EP2626518A1 Seal assemby for turbine coolant passageways |
| 08/14/2013 | EP2626517A2 Rotating assembly for a turbine assembly |
| 08/14/2013 | EP2626516A1 Turbine assembly and corresponding method of altering a fundamental requency |
| 08/14/2013 | EP2626515A1 Tandem blade group assembly |
| 08/14/2013 | EP2626514A1 Flow engine |
| 08/14/2013 | EP2626513A1 Tandem blade assembly |
| 08/14/2013 | EP2626512A1 Flow engine |
| 08/14/2013 | EP2626169A2 Methods and tooling assemblies for the manufacture of metallurgically-consolidated turbine engine components |
| 08/14/2013 | EP2626167A1 Method for reconditioning a blade of a gas turbine and also a reconditioned blade |
| 08/14/2013 | EP2625413A1 Aircraft propulsion assembly |
| 08/14/2013 | EP2625389A1 Impingement cooling of gas turbine blades or vanes |
| 08/14/2013 | EP2625388A1 Thrust reverser |
| 08/14/2013 | EP2624996A1 Method for manufacturing a metal part |
| 08/14/2013 | CN203130243U Pressurizer |
| 08/14/2013 | CN203130242U Turbocharger |
| 08/14/2013 | CN103249917A Turbine rotor blade |
| 08/14/2013 | CN103249916A Fluid flow machine especially gas turbine penetrated axially by a hot gas stream |
| 08/14/2013 | CN103244198A Turbine assembly |
| 08/14/2013 | CN103244197A Turbine blade partition rib parametric modeling method |
| 08/14/2013 | CN103244196A Discrete air film cooling hole shape |
| 08/14/2013 | CN103244195A Precision forging blade thickness plastic deformation compensation method |
| 08/14/2013 | CN103244194A Threaded interference fitting method and threaded interference fitting structure for turbine impeller and rotary shaft |
| 08/14/2013 | CN101182785B Integrally bladed rotor having MMC ring component and airfoil component having MMC airfoils |
| 08/13/2013 | US8508062 Turbomachinery electric generator arrangement |
| 08/13/2013 | US8506257 Adjustable camber aerofoil |
| 08/13/2013 | US8506253 Balancing apparatus for rotor assembly |
| 08/13/2013 | US8506252 Turbine blade with multiple impingement cooling |
| 08/13/2013 | US8506251 Gas turbine blade, manufacturing method therefor, and gas turbine using turbine blade |
| 08/13/2013 | US8506250 Wind turbine rotor blade with trailing edge extension and method of attachment |
| 08/13/2013 | US8506241 Turbine blade with cooling and tip sealing |
| 08/13/2013 | US8506239 Turbine with at least one rotor which comprises rotor disks and a tie-bolt |
| 08/13/2013 | US8506236 Counter rotation inducer housing |
| 08/13/2013 | CA2680645C Gas turbine engine rotor and balance weight therefor |
| 08/13/2013 | CA2558028C Locking device for an axial retention ringon a blade, associated disk rotor and retention ring and rotor and aircraft engine containing same |
| 08/09/2013 | CA2803367A1 Gas turbine engine rotor balancing |
| 08/08/2013 | WO2013116500A1 Gas turbine rotary blade with tip insert |
| 08/08/2013 | WO2013115984A1 Compressor disk bleed air scallops |
| 08/08/2013 | WO2013115949A2 Aluminum airfoil |
| 08/08/2013 | WO2013115873A2 Fluid driven turbine blade and turbine using same |
| 08/08/2013 | WO2013113324A1 Gas turbine with rotating casing |
| 08/08/2013 | WO2013060977A3 Method for manufacturing a turbine nozzle guide vanes sector or a compressor guide vanes sector from composite material for a turbomachine |
| 08/08/2013 | WO2012066262A3 Blade for a turbine engine propeller |
| 08/08/2013 | US20130202912 Process for producing thermal barrier coating, turbine member provided with thermal barrier coating, and gas turbine |
| 08/08/2013 | US20130202451 Safety propeller |
| 08/08/2013 | US20130202449 Axisymmetric part for an aviation turbine engine rotor |
| 08/08/2013 | US20130202445 Turbine blade having improved flutter capability and increased turbine stage output |
| 08/08/2013 | US20130202444 Blade cascade and turbomachine |
| 08/08/2013 | US20130202443 Axial flow device |
| 08/08/2013 | US20130202442 Fan and boost joint |
| 08/08/2013 | US20130202439 Rotating assembly for a turbine assembly |
| 08/08/2013 | US20130202403 Low noise turbine for geared turbofan engine |
| 08/08/2013 | US20130202401 Method and Device for variable motion and applications using Interchangeable Heads |
| 08/08/2013 | US20130199198 Method of automatically regulating an aircraft power plant, a device, and an aircraft |
| 08/08/2013 | DE102012002285A1 Verfahren zum Herstellen eines Turbinenrotors A method of manufacturing a turbine rotor |
| 08/08/2013 | DE102012002284A1 Verfahren zum Herstellen eines Turbinenrotors eines Abgasturboladers sowie Verwendung eines Turbinenrotors A method of manufacturing a turbine rotor of a turbocharger, as well as use of a turbine rotor |
| 08/08/2013 | DE102012002275A1 Vorrichtung und Verfahren zur Bearbeitung von Hochdruckturbinenschaufeln einer Gasturbine Apparatus and method for processing high-pressure turbine blades of a gas turbine |
| 08/08/2013 | CA2855493A1 Fluid driven turbine blade and turbine using same |
| 08/07/2013 | EP2623793A1 Blade row and flow machine |
| 08/07/2013 | EP2623729A2 Gas turbine engine with a fan and booster joint and corresponding method |
| 08/07/2013 | EP2623722A1 Turbine |
| 08/07/2013 | EP2623716A1 Design method for a rotor blade |
| 08/07/2013 | EP2623715A2 Exhaust strut with leading edge formed of shape memory alloy |
| 08/07/2013 | EP2623714A2 Turbine cooling system |
| 08/07/2013 | EP2623713A1 A rotor, a steam turbine and a method for producing a rotor |
| 08/07/2013 | EP2623252A1 Method of forming a strong connection between two components using forms for manipulating the components |
| 08/07/2013 | EP2622110A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH y/y' TRANSITION TEMPERATURE AND A COMPONENT |
| 08/07/2013 | CN203114427U Gas turbine engine |
| 08/07/2013 | CN203114353U Circular-arc feather joint structure |
| 08/07/2013 | CN203114352U 300MW machine set low pressure cylinder double-backpressure double-rotor exchange device |
| 08/07/2013 | CN103237958A Blade body and rotary machine |
| 08/07/2013 | CN102076885B Component for rotary machine |
| 08/07/2013 | CN101429875B turbine blade with end shield of Z-notch shape |
| 08/06/2013 | US8504646 Data transfer between motors |