| 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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| 10/13/2011 | US20110250057 Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine |
| 10/13/2011 | DE102010014556A1 Leitschaufel einer Strömungsmaschine Vane of a turbomachine |
| 10/13/2011 | DE102010014094A1 Motor vehicle pump device, particularly for forming motor vehicle coolant pump, has pump wheel drive shaft that forms operating fluid channel, where operating fluid channel is provided for cooling motor vehicle pump device component |
| 10/12/2011 | EP2374999A2 Composite turbine bucket assembly |
| 10/12/2011 | EP2374998A2 Turbine bucket having a radial cooling hole |
| 10/12/2011 | EP2374997A2 Cooling circuit of a gas turbine engine |
| 10/12/2011 | EP2374996A2 Airfoil cooling arrangement, corresponding casting core mold insert and cooling method |
| 10/12/2011 | EP2374995A2 Rear hub cooling for high pressure compressor |
| 10/12/2011 | EP2374994A2 Attachment assemblies between turbine rotor discs and methods of attaching turbine rotor discs |
| 10/12/2011 | EP2374913A1 Deposition apparatus with preheating chamber having thermal hood |
| 10/12/2011 | EP2374911A2 A method of manufacturing a rotor disc |
| 10/12/2011 | EP2374777A2 Composite article having a solid solution protective layer |
| 10/12/2011 | EP2374572A1 Solder containing germanium, component with a solder and a soldering method |
| 10/12/2011 | EP2373872A2 Turbine wheel provided with an axial retention device that locks blades in relation to a disk |
| 10/12/2011 | EP2373824A1 Method for coating a component with film cooling holes, and component |
| 10/12/2011 | EP1839800B1 Method for local application of diffusion aluminide coating |
| 10/12/2011 | EP1828567B1 Diffuser aspiration for a tip turbine engine |
| 10/12/2011 | CN102216567A Gas turbine with securing plate between blade base and disk |
| 10/12/2011 | CN102216566A Anti-erosion layer for aerodynamic components and structures and method for the production thereof |
| 10/12/2011 | CN102213176A Same-diameter impeller group working by using fluid power |
| 10/12/2011 | CN102213115A Device and method for monitoring and controlling security risk of turbine movable blade on line |
| 10/12/2011 | CN102213109A Turbine bucket having a radial cooling hole |
| 10/12/2011 | CN102213108A Composite turbine bucket assembly |
| 10/11/2011 | US8033794 Wind turbine |
| 10/11/2011 | US8033790 Multiple piece turbine engine airfoil with a structural spar |
| 10/11/2011 | US8033789 Apparatus for preventing ice accretion |
| 10/11/2011 | US8033787 Canopy cover for a ceiling fan |
| 10/11/2011 | US8033784 Compressor rotor |
| 10/11/2011 | CA2548712C Coverplate deflectors for redirecting a fluid flow |
| 10/11/2011 | CA2528076C Shroud leading edge cooling |
| 10/11/2011 | CA2493094C Improvements to turbine blade cooling air exhaust slots |
| 10/06/2011 | WO2011123432A1 Multilayer cmas-resistant barrier coating |
| 10/06/2011 | WO2011122342A1 Ni-based alloy, and gas turbine rotor blade and stator blade each using same |
| 10/06/2011 | US20110243756 Method for producing a blade by casting and blade for a gas turbine |
| 10/06/2011 | US20110243755 Cooled blade for a gas turbine, method for producing such a blade, and gas turbine having such a blade |
| 10/06/2011 | US20110243753 Wind turbine blade having a flow guiding device with optimised height |
| 10/06/2011 | US20110243752 Method for manufacturing a rectifier |
| 10/06/2011 | US20110243749 Gas turbine engine with non-axisymmetric surface contoured rotor blade platform |
| 10/06/2011 | US20110243748 High pressure turbine blade airfoil profile |
| 10/06/2011 | US20110243747 High pressure turbine vane airfoil profile |
| 10/06/2011 | US20110243746 Composite turbine bucket assembly |
| 10/06/2011 | US20110243744 Seal for a platform in the rotor of a turbine engine |
| 10/06/2011 | US20110243743 Attachment assemblies between turbine rotor discs and methods of attaching turbine rotor discs |
| 10/06/2011 | US20110243742 Stator stage for turbomachine compressor |
| 10/06/2011 | US20110243714 Sealing structure on a shroud of a turbine blade |
| 10/06/2011 | US20110243711 Interior cooling channels |
| 10/06/2011 | US20110243709 Non-integral platform and damper for an airfoil |
| 10/06/2011 | DE102010003594A1 Turbine blades for fluid flow machine in e.g. power generation field, has vibration damping element coupled with surrounding area such that heat transferred to shape memory element is changed based on vibration state of blade |
| 10/05/2011 | EP2372165A1 Turbine blade and gas turbine |
| 10/05/2011 | EP2372099A2 Turbine sealing system |
| 10/05/2011 | EP2372096A2 Composite fan blade dovetail root |
| 10/05/2011 | EP2372095A1 Method and device for fixing a blade to a rotor using a memory shape element |
| 10/05/2011 | EP2372094A2 Non-Integral Platform and Damper for a gas turbine engine blade |
| 10/05/2011 | EP2372093A1 Seal design on a shroud of a turbine blade |
| 10/05/2011 | EP2372092A2 Internal cooling channels for industrial machines |
| 10/05/2011 | EP2372091A2 Airfoil having a cooling channel with a flag-shaped region |
| 10/05/2011 | EP2372090A2 Apparatus for cooling a bucket assembly |
| 10/05/2011 | EP2372089A2 Apparatus for cooling an airfoil |
| 10/05/2011 | EP2372088A2 Turbofan flow path trenches |
| 10/05/2011 | EP2372087A1 Components with an external wall which can be exposed to a hot gas of a gas turbine and method for producing such a component |
| 10/05/2011 | EP2372086A2 Cooling circuit for a turbine rotor blade and corresponding cooling method |
| 10/05/2011 | EP2372085A2 Internal reaction steam turbine cooling arrangement |
| 10/05/2011 | EP2372084A2 Turbomachine Rotor Cooling |
| 10/05/2011 | EP2371987A2 Thermal barrier coating member, method for producing the same, thermal barrier coating material, gas turbine, and sintered body |
| 10/05/2011 | EP2371986A1 Metallic coating for non-line of sight areas |
| 10/05/2011 | EP2371521A1 Method of manufacturing a rectifier |
| 10/05/2011 | EP2371476A1 Method for welding workpieces made from extremely heat-proof superalloys |
| 10/05/2011 | EP2371459A2 Masking apparatus |
| 10/05/2011 | EP1529123B1 Intermetallic material and use of said material |
| 10/05/2011 | CN202001066U Rotor of steam turbine for driving boiler water feeding pump of below 300MW |
| 10/05/2011 | CN1766290B Turbine airfoil with stepped coolant outlet slots |
| 10/05/2011 | CN102209837A Annular flange for fastening a rotor or a stator element in a turbine engine |
| 10/05/2011 | CN102207007A Interior cooling channels |
| 10/05/2011 | CN101484663B Guide-vane arrangement for an engine |
| 10/05/2011 | CN101105150B An engine core stand arrangement and method of removal and transportation of an engine core |
| 10/05/2011 | CN101078355B Airfoil and method for moisture removal and steam injection |
| 10/04/2011 | US8029240 Rotor blade adjustable weight retention system |
| 09/30/2011 | CA2734857A1 High pressure turbine vane airfoil profile |
| 09/30/2011 | CA2734842A1 High pressure turbine blade airfoil profile |
| 09/29/2011 | WO2011119147A1 Metallic bondcoat with a high gamma/gamma' transition temperature and a component |
| 09/29/2011 | WO2011119145A1 METALLIC BONDCOAT OR ALLOY WITH A HIGH γ/γ' TRANSITION TEMPERATURE AND A COMPONENT |
| 09/29/2011 | WO2011118131A1 Double-jet film cooling structure |
| 09/29/2011 | WO2011117395A1 Component having an outer wall which can be exposed to a hot gas of a gas turbine and method for producing such a component |
| 09/29/2011 | WO2011039352A3 Rotor of a turbomachine compressor, with an optimised inner end wall |
| 09/29/2011 | US20110236223 Blade for a gas turbine |
| 09/29/2011 | US20110236222 Blade for a gas turbine and casting technique method for producing same |
| 09/29/2011 | US20110236221 Four-Wall Turbine Airfoil with Thermal Strain Control for Reduced Cycle Fatigue |
| 09/29/2011 | US20110236220 Airfoil cooling hole flag region |
| 09/29/2011 | US20110236215 Wind turbine control surface hinge |
| 09/29/2011 | US20110236214 High pressure turbine blade airfoil profile |
| 09/29/2011 | US20110236213 Guide blade carrier |
| 09/29/2011 | US20110236192 Compressor housing resistant to titanium fire, high-pressure compressor including such a housing and aircraft engine fitted with such a compressor |
| 09/29/2011 | US20110236190 Turbine rotor wheel |
| 09/29/2011 | US20110236178 Branched airfoil core cooling arrangement |
| 09/29/2011 | US20110233057 Homogeneous titanium tungsten alloys produced by powder metal technology |
| 09/29/2011 | DE102010012940A1 Producing firmly bonded connection between two components of a fluid-flow machine such as a steam turbine, which reaches in an operation of an operating temperature, comprises providing a solder connection of the firmly bonded compound |
| 09/29/2011 | DE102010012779B3 Method for manufacturing and/or repairing of e.g. blisk for aircraft engine, involves producing joint connection between hub element and rotor blade, where connection comprises joining zone with smaller cross-section thickness |
| 09/29/2011 | DE102010012583A1 Verfahren zum Betrieb einer Dampfturbine mit einem Impulsrotor sowie Dampfturbine zur Durchführung des Verfahrens Method for operating a steam turbine rotor, as well as with an impulse steam turbine for carrying out the method |
| 09/28/2011 | EP2369137A1 One-stage stator vane cooling structure and gas turbine |
| 09/28/2011 | EP2369136A1 Weight-reduced single-piece multi-stage drum of an axial flow compressor |