| 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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| 06/27/2013 | WO2013067341A3 Ni-ti-cr near ternary eutectic alloy for gas turbine component repair |
| 06/27/2013 | US20130164488 Airfoils for wake desensitization and method for fabricating same |
| 06/27/2013 | US20130164145 Method for manufacturing a hollow vane |
| 06/27/2013 | US20130164143 Laminated abutment, a rotor provided with such an abutment, and an aircraft |
| 06/27/2013 | US20130164142 Propeller blade with reinforcing spars and boxes, and propeller comprising at least one such blade |
| 06/27/2013 | US20130164141 Blade with semi-rigid trailing edge |
| 06/27/2013 | US20130164140 Airfoils including compliant tip |
| 06/27/2013 | US20130164139 Fan with replacable vanes |
| 06/27/2013 | US20130164138 Turbine rotor insert and related method of installation |
| 06/27/2013 | US20130164137 Turbofan flow path trenches |
| 06/27/2013 | US20130164132 Dual frequency hub mounted vibration suppressor system |
| 06/27/2013 | US20130164130 Stirling engine with flapping wing for an emission-free aircraft |
| 06/27/2013 | US20130161444 High efficiency hub for pressure jet helicopters |
| 06/27/2013 | DE102012112536A1 Turbinenrotoreinsatz und zugehöriges Installationsverfahren Turbine rotor insert and associated installation procedures |
| 06/27/2013 | DE102012002363A1 Metallic base material component e.g. fan blade of aircraft gas turbine engine, has geometric support structure that is formed with undercut starting from base material layers which are joined undetachably with molded lining of insert |
| 06/27/2013 | DE102011089701A1 Vorrichtung zum Rekonturieren einer Gasturbinenschaufel Apparatus for recontouring a gas turbine blade |
| 06/27/2013 | DE102011089699A1 Vorrichtung zum Rekonturieren einer Gasturbinenschaufel Apparatus for recontouring a gas turbine blade |
| 06/26/2013 | EP2607633A2 Engine assembly and waste heat recovery system |
| 06/26/2013 | EP2607629A1 Shrouded turbine blade with cooling air outlet port on the blade tip and corresponding manufacturing method |
| 06/26/2013 | EP2607628A2 Airfoils including compliant tip |
| 06/26/2013 | EP2607627A1 Fan blade with composite core and wavy wall trailing edge cladding |
| 06/26/2013 | EP2607626A1 Turbomachine and stage of a turbomachine |
| 06/26/2013 | EP2607625A1 Turbomachine and stage of turbomachine |
| 06/26/2013 | EP2607624A1 Vane for a turbomachine |
| 06/26/2013 | EP2606203A1 Transonic gas turbine stage and method |
| 06/26/2013 | CN203022824U Damping girdle structure of high-load short blade for industrial steam turbine |
| 06/26/2013 | CN103180617A Transonic blade |
| 06/26/2013 | CN103180550A Self-centring clamping device and measuring device for blade |
| 06/26/2013 | CN103174467A 连接器 Connector |
| 06/26/2013 | CN103174466A Airfoils including compliant tip |
| 06/26/2013 | CN103174465A Airfoils including tip profile for noise reduction and method for fabricating same |
| 06/26/2013 | CN103174464A Steam turbine rotor cooling system with middle steam admission bidirectional flow structure |
| 06/26/2013 | CN103174463A Turbine rotor insert and related method of installation |
| 06/25/2013 | US8470460 Multilayer thermal barrier coatings |
| 06/25/2013 | US8469670 Fan assembly |
| 06/25/2013 | US8469669 Cover disk for a closed impeller |
| 06/25/2013 | US8469667 Distributed-mass device for reducing vibration generated by a rotorcraft lift rotor, and a rotor hub fitted with such a device |
| 06/25/2013 | US8469666 Turbine blade tip portion with trenched cooling holes |
| 06/25/2013 | CA2502810C Turbine shroud cooling system |
| 06/23/2013 | CA2798754A1 Airfoils including compliant tip |
| 06/20/2013 | WO2013090742A1 Energy absorbent fan blade spacer |
| 06/20/2013 | WO2013089913A1 Film cooled turbine component |
| 06/20/2013 | WO2013089255A1 Turbine blade |
| 06/20/2013 | WO2013089251A1 Turbine blade |
| 06/20/2013 | WO2013089250A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013089218A1 Heat-resistant nickel-based superalloy |
| 06/20/2013 | WO2013089173A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013089139A1 Turbine |
| 06/20/2013 | WO2013087496A1 Rotary machine including a machine rotor with a composite impeller portion and a metal shaft portion |
| 06/20/2013 | WO2012071166A3 Integrated variable geometry flow restrictor and heat exchanger |
| 06/20/2013 | US20130156966 Method for reprocessing a turbine blade having at least one platform |
| 06/20/2013 | US20130156602 Film cooled turbine component |
| 06/20/2013 | US20130156601 Gas turbine engine airfoil cooling circuit |
| 06/20/2013 | US20130156600 Components with microchannel cooling |
| 06/20/2013 | US20130156595 Riblet structure on a flow surface and method |
| 06/20/2013 | US20130156594 Composite rotor and vane assemblies with integral airfoils |
| 06/20/2013 | US20130156592 Fan blade with composite core and wavy wall trailing edge cladding |
| 06/20/2013 | US20130156591 Energy absorbent fan blade spacer |
| 06/20/2013 | US20130156590 Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping |
| 06/20/2013 | US20130156589 Turbine rotor retaining system |
| 06/20/2013 | US20130156588 Electrical grounding for fan blades |
| 06/20/2013 | US20130156587 Retrofitting methods and devices for large steam turbines |
| 06/20/2013 | US20130156586 Method for connecting a turbine blade or vane to a turbine disc or a turbine ring |
| 06/20/2013 | US20130156584 Compressor rotor with internal stiffening ring of distinct material |
| 06/20/2013 | US20130156583 Airfoils including tip profile for noise reduction and method for fabricating same |
| 06/20/2013 | US20130156579 Ambient air cooling arrangement having a pre-swirler for gas turbine engine blade cooling |
| 06/20/2013 | US20130156541 Active turbine tip clearance control system |
| 06/20/2013 | DE102010015211B4 Dämpfungselement zur Dämpfung von Laufschaufelschwingungen, Laufschaufel sowie Rotor Damping element for damping blade vibrations, blade and rotor |
| 06/20/2013 | DE102007037208B4 Turbinenschaufel mit zumindest einer Einsatzhülse zum Kühlen der Turbinenschaufel Turbine blade with at least one insert sleeve for cooling the turbine blade |
| 06/20/2013 | CA2858320A1 Fiber structure woven into a single part by means of 3d weaving, and use in the manufacture of a composite material part |
| 06/20/2013 | CA2858020A1 Turbine blade |
| 06/20/2013 | CA2798821A1 Fan blade with composite core and wavy wall trailing edge cladding |
| 06/20/2013 | CA2798211A1 Airfoils including tip profile for noise reduction and method for fabricating same |
| 06/19/2013 | EP2604866A1 Method and system for reducing flow losses and fluid flow engine |
| 06/19/2013 | EP2604806A2 Gas turbine engine with controller for cooling and blade tip clearance control of the turbine and coresponding method for operating a gas turbine engine |
| 06/19/2013 | EP2604800A2 Nozzle vane for a gas turbine engine |
| 06/19/2013 | EP2604799A1 Rotor of a turbomachine |
| 06/19/2013 | EP2604798A1 Turbine engine component and corresponding manufacturing method |
| 06/19/2013 | EP2604797A1 Rotor blade with a rib assembly with an abrasive coating |
| 06/19/2013 | EP2604796A2 Gas turbine components with microchannel cooling |
| 06/19/2013 | EP2604795A2 Aerofoil blade or vane |
| 06/19/2013 | EP2604794A1 Electrical Grounding for Fan Blades |
| 06/19/2013 | EP2604793A2 Rotor with Internal Stiffening Ring |
| 06/19/2013 | EP2604792A1 Method for repairing a component of a gas turbine engine and associated repaired component |
| 06/19/2013 | EP2604588A2 Method for stabilizing a refractory carbide hot gas path component |
| 06/19/2013 | EP2604377A1 Method for laser processing a laminated piece with ceramic coating |
| 06/19/2013 | EP2603670A1 Device for locking a root of a rotor blade |
| 06/19/2013 | EP2603669A1 Blade arrangement and associated gas turbine |
| 06/19/2013 | EP2603668A1 Blade ring segment, turbomachine and method for producing same |
| 06/19/2013 | CN103168149A Assembly of a blade and a composite carrier, obtained by sealing |
| 06/19/2013 | CN103161526A Gas-steam combined cycle power generation system |
| 06/19/2013 | CN103160711A Nickel-cobalt-based alloy and bond coat and bond coated articles incorporating the same |
| 06/19/2013 | CN101749181B Turbine blade and method of fabricating same |
| 06/19/2013 | CN101688313B Anti-wear coating and component comprising an anti-wear coating |
| 06/19/2013 | CN101508063B Methods and apparatus to repair a rotor disk for a gas turbine |
| 06/19/2013 | CN101333939B Turbomachine shaft damper device |
| 06/19/2013 | CN101333938B Device for cooling the peripheral cavities of a turbomachine rotor disc with double air supply |
| 06/19/2013 | CN101315032B Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes |
| 06/18/2013 | US8465258 Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine blade |
| 06/18/2013 | US8465256 Wind turbine rotor |