| 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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| 04/06/2011 | CN101624945B Jet pressing burning splitting ring curled turbine engine |
| 04/06/2011 | CN101473171B Armor-plated machine components and gas turbines |
| 04/06/2011 | CN101233298B Cooled turbine blade for a gas turbine and use of such a turbine blade |
| 04/06/2011 | CN101158291B 汽轮机动叶片 Turbine rotor blades |
| 04/05/2011 | US7919187 Environmental barrier coating for silicon-containing substrates and process therefor |
| 04/05/2011 | US7918653 Rotor blade trailing edge assemby and method of use |
| 04/05/2011 | US7918652 Dovetail structure of fan |
| 04/05/2011 | US7918651 Fan and impeller thereof |
| 04/05/2011 | US7918647 Turbine airfoil with flow blocking insert |
| 04/05/2011 | US7918646 High efficiency turbine with variable attack angle foils |
| 04/05/2011 | US7918645 Torque converter with brazed turbine |
| 04/05/2011 | US7917988 Apparatus and a method of applying a dry film lubricant to a rotor slot |
| 04/05/2011 | CA2458550C Double flow compressor |
| 04/01/2011 | CA2715954A1 Gas turbine engine sheet metal vane |
| 04/01/2011 | CA2715605A1 Fabricated gas turbine vane ring |
| 04/01/2011 | CA2715604A1 Method for centering engine structures |
| 04/01/2011 | CA2715596A1 Fabricated static vane ring |
| 04/01/2011 | CA2715594A1 Interturbine vane with multiple air chambers |
| 04/01/2011 | CA2715271A1 Gas turbine engine balancing |
| 04/01/2011 | CA2715228A1 Cooling air system for mid turbine frame |
| 04/01/2011 | CA2714740A1 Radial balancing clip weight for rotor assembly |
| 03/31/2011 | WO2011036380A1 Method and mold for producing a turbine engine blade made from composite material |
| 03/31/2011 | WO2011036045A1 Blade for use in two-phase flows and method for producing such a blade |
| 03/31/2011 | WO2011035773A1 Method for repairing a component of a turbomachine |
| 03/31/2011 | WO2011035772A1 Method for repairing an integral rotor and integral rotor |
| 03/31/2011 | WO2010136707A3 Low-pressure turbine |
| 03/31/2011 | US20110076155 Guide blade for a gas turbine |
| 03/31/2011 | US20110076153 Steam turbine rotor and steam turbine using the same |
| 03/31/2011 | US20110076151 Method and system for focused energy brazing |
| 03/31/2011 | US20110076150 Airfoil shape |
| 03/31/2011 | US20110076148 Fan |
| 03/31/2011 | DE102010037688A1 Fastback-Turbulatorstruktur und ein dieselbe enthaltender Turbinenleitapparat FastBack Turbulatorstruktur and a same-containing turbine nozzle |
| 03/31/2011 | DE102009048665A1 Turbinenschaufel und Verfahren zu deren Herstellung Turbine blade and methods for their preparation |
| 03/31/2011 | DE102009043136A1 Verfahren zum Reparieren eines Bauteils einer Strömungsmaschine A method of repairing a component of a turbomachine |
| 03/31/2011 | DE102009043097A1 Laufschaufel zur Verwendung in Zweiphasenströmungen sowie Verfahren zum Herstellen einer solchen Laufschaufel Blade for use in two-phase flows as well as methods for making such a blade |
| 03/30/2011 | EP2302173A1 Gas turbine |
| 03/30/2011 | EP2302172A1 Machine comprising an electromagnetic woven rotor and manufacturing method |
| 03/30/2011 | EP2302171A1 Turbomachine comprising several impellers and method of operation |
| 03/30/2011 | EP2302170A1 Turbomachine system and method of operation |
| 03/30/2011 | EP2302169A2 Rotary machine tip clearance control mechanism |
| 03/30/2011 | EP2302168A1 Turbine blade |
| 03/30/2011 | EP2302167A2 A gas turbine sealing component |
| 03/30/2011 | EP2302166A2 A metal-composite hybrid component |
| 03/30/2011 | EP2302165A2 Steam turbine having rotor with cavities |
| 03/30/2011 | EP2302089A1 Steam turbine rotor and alloy therefor |
| 03/30/2011 | EP2301841A2 Variable shape rotor blade |
| 03/30/2011 | EP2301730A1 Hole drilling with close proximity backwall |
| 03/30/2011 | EP2301707A1 Method and device for producing a hole |
| 03/30/2011 | EP2300728A1 Method for increasing the coefficient of adhesion between two parts rotating as one with a rotor |
| 03/30/2011 | EP2300685A1 Turbomachine fan rotor |
| 03/30/2011 | EP2300178A1 Blade for a gas turbine and method for producing such a blade by a casting process |
| 03/30/2011 | EP2270312A9 Aero- or hydrodynamic construction |
| 03/30/2011 | EP1740738B1 Method for application of a protective coating to a thermally-stressed component |
| 03/30/2011 | CN1903494B Method for repairing a blade of a one-piece bladed disc of aturbine engine and a test piece for implementing the method |
| 03/30/2011 | CN101994526A Locking spacer assembly for circumferential dovetail rotor blade attachment system |
| 03/30/2011 | CN101994525A End wall cooling arrangement for turbine |
| 03/30/2011 | CN101994524A System and method for modifying rotor thrust |
| 03/30/2011 | CN101992356A Joined turbine rotor components and method thereof |
| 03/29/2011 | US7914257 Turbine rotor blade with spiral and serpentine flow cooling circuit |
| 03/29/2011 | US7913495 Gas turbine and manufacturing process of gas turbine |
| 03/29/2011 | CA2473335C Improved device for attaching a motor shaft to a bearing support |
| 03/29/2011 | CA2425409C Process of formation of a ceramic coating on a substrate by electron-beam physical vapor deposition |
| 03/24/2011 | WO2011033206A1 Part comprising structure and shape memory alloy element |
| 03/24/2011 | WO2011033063A1 Blade fastening having safety device for turbine blades |
| 03/24/2011 | WO2011032548A1 Rotor of a turbomachine |
| 03/24/2011 | WO2010043209A3 Component for a gas turbine and method for producing the component |
| 03/24/2011 | US20110070368 Apparatus and a method of applying a dry film lubricant to a rotor slot |
| 03/24/2011 | US20110070097 Gas turbine engine component cooling scheme |
| 03/24/2011 | US20110070096 Curved electrode and electrochemical machining method and assembly employing the same |
| 03/24/2011 | US20110070095 Aerofoil structure |
| 03/24/2011 | US20110070093 Coating of metallic articles to restrict ice accumulation |
| 03/24/2011 | US20110070089 Guide vane for a gas turbine |
| 03/24/2011 | US20110070088 Steam turbine rotor and alloy therefor |
| 03/24/2011 | US20110070085 Internally damped blade |
| 03/24/2011 | US20110070084 Electric fan capable to modify angle of air supply |
| 03/24/2011 | US20110070069 Steam turbine having rotor with cavities |
| 03/24/2011 | US20110070064 System and Method for Accommodating Changing Resource Conditions for a Steam Turbine |
| 03/24/2011 | DE102009042029A1 Blade ring for flow machine, particularly for gas turbine, has hardened reinforcement on inner shroud, where reinforcement is closed in circumferential direction |
| 03/24/2011 | DE102009029587A1 Rotor einer Turbomaschine Rotor of a turbomachine |
| 03/23/2011 | EP2299124A1 Rotor blade for an axial compressor |
| 03/23/2011 | EP2299123A2 Composite airfoil with locally reinforced tip region |
| 03/23/2011 | EP2299060A1 Blade fixation with locking device for turbine blades |
| 03/23/2011 | EP2299059A2 An aerofoil blade assembly |
| 03/23/2011 | EP2299058A2 Cooled blade or vane and corresponding fluid flow conduit |
| 03/23/2011 | EP2299057A1 Gas Turbine |
| 03/23/2011 | EP2299056A1 Cooling of a gas turbine component shaped as a rotor disc or as a blade |
| 03/23/2011 | EP2298946A2 High-strength Ni-based wrought superalloy and manufacturing method of same |
| 03/23/2011 | EP2298489A1 Superalloy composition and method of forming a turbine engine component |
| 03/23/2011 | EP2297430A1 Axial turbine for a gas turbine with limited play between blades and housing |
| 03/23/2011 | CN101988394A Thermoplastic last-stage blade |
| 03/23/2011 | CN101988393A Extra block-free structure of blade forging |
| 03/23/2011 | CN101988392A Rotor blades for turbine engines |
| 03/23/2011 | CN101987412A Process of closing an opening in a component |
| 03/22/2011 | US7909581 Layer system, use and process for producing a layer system |
| 03/22/2011 | US7909580 Vanes for exposure to vibratory loading |
| 03/22/2011 | US7909565 Turbomachine, in particular a gas turbine |
| 03/22/2011 | CA2653836C Annular flow duct for a turbomachine through which a main flow can flow in the axial direction |
| 03/22/2011 | CA2528668C Rotor assembly with cooling air deflectors and method |
| 03/17/2011 | WO2011029420A1 Deflecting device for a leakage flow in a gas turbine, and gas turbine |
| 03/17/2011 | WO2011009430A9 Method for coating turbine blades |