| 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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| 02/07/2008 | US20080031724 Turbo Machine With A Rotor Which Has At Least One Rotor Disk With A Bore |
| 02/07/2008 | US20080028726 Container and pallet for receiving blades of a fluid machine |
| 02/07/2008 | DE112006000603T5 Leitrad und Schaufel für eine Turbomaschinenanlage And stator blade for a turbo machinery |
| 02/07/2008 | DE102007035236A1 Turbinenschaufelspitzendeckband Turbine blade tip shroud |
| 02/07/2008 | CA2658275A1 Gas turbine component with a thermal barrier coating, thermal barrier coating for a gas turbine component and process for producing a thermal barrier coating on a gas turbine component |
| 02/06/2008 | EP1884879A1 Method of analysis of secondary air circuits in gas turbine plants |
| 02/06/2008 | EP1884628A2 Heat transfer system and method for turbine engine using heat pipes |
| 02/06/2008 | EP1884625A2 Heat transfer system and method for turbine engine using heat pipes |
| 02/06/2008 | EP1884624A2 Rotor assembly of a gas turbine and method of assembling a rotor |
| 02/06/2008 | EP1884623A2 Hollow CMC airfoil with internal stitch |
| 02/06/2008 | EP1884622A2 Airfoil with customized convective cooling |
| 02/06/2008 | EP1884621A2 Serpentine microciruit cooling with pressure side features |
| 02/06/2008 | EP1884312A1 A device for blocking a blade of a turbine and a method for blade machining using said blocking device |
| 02/06/2008 | EP1884306A1 Hybrid welding repair of gas turbine superalloy components |
| 02/06/2008 | EP1332016A4 Process for drilling holes in a metallic workpiece having a thermal barrier coating |
| 02/06/2008 | CN101120156A Component with film cooling holes |
| 02/06/2008 | CN101119826A Method for producing a hole and corresponding device |
| 02/06/2008 | CN101117898A Pre-coating burnishing of erosion coated parts |
| 02/06/2008 | CN101117897A 涡轮机叶片尖端罩 Turbine blade tip shroud |
| 02/06/2008 | CN101117896A 转子叶片及其制造方法 Rotor blade and its manufacturing method |
| 02/06/2008 | CN101117895A Variable-speed turbine final stage moving vane |
| 02/06/2008 | CN100366866C Turbine bucket damper pin |
| 02/06/2008 | CN100366865C Turbine propeller and turbine engine |
| 02/06/2008 | CN100366379C Surface processing method for matchable, conforming to fluid tech. |
| 02/05/2008 | US7327857 Non-contact measurement method and apparatus |
| 02/05/2008 | US7326873 Apparatus and methods for repairing tenons on turbine buckets |
| 02/05/2008 | US7326470 Adds the minimum weight while providing the maximum thermal insulation capability; for long life, stability, economy, gas turbines. coated part comprising a thermal barrier coating offering lower thermal conductivity but which exhibits suitable resistance to spallation |
| 02/05/2008 | US7326035 Device for attaching a moving blade to a turbine rotor disk in a turbomachine |
| 02/05/2008 | US7326033 Turbomachine blade |
| 02/03/2008 | CA2590496A1 Pre-coating burnishing of erosion coated parts |
| 02/01/2008 | CA2595773A1 Hybrid welding repair of gas turbine superalloy components |
| 01/31/2008 | WO2008013610A1 Turbine rotor blade groove entry slot lock structure |
| 01/31/2008 | WO2008012842A1 Highly corrosion-resistant movable blade assembly for a steam turbine, in particular a geothermal impulse turbine |
| 01/31/2008 | WO2008012530A2 Impulse turbine for use in bi-directional flows |
| 01/31/2008 | WO2005112603A3 Durable thermal barrier coating having low thermal conductivity |
| 01/31/2008 | US20080025844 Rotor for a Turbo Engine |
| 01/31/2008 | US20080025843 Mounting disc |
| 01/31/2008 | US20080025841 Rotor blade and method of fabricating same |
| 01/31/2008 | US20080025838 Ring seal for a turbine engine |
| 01/31/2008 | US20080022691 Method for Designing a Low-Pressure Turbine of an Aircraft Engine, and Low-Pressure Turbine |
| 01/31/2008 | DE102006034424A1 Gasturbine Gas turbine |
| 01/31/2008 | DE102006030235A1 Verfahren zum Schutz von Heißgaskorrosion von keramischen Oberflächen oder eines Körpers, hochtemperaturbeständiger Körper und deren Verwendung A method of protecting the hot gas corrosion of ceramic surfaces or a body of high temperature resistant body and their use |
| 01/31/2008 | CA2658914A1 Impulse turbine for use in bi-directional flows |
| 01/30/2008 | EP1882826A1 Ventilation system for an upstream cavity of a centrifugal compressor impeller |
| 01/30/2008 | EP1882825A1 System for cooling a centrifugal compressor impeller |
| 01/30/2008 | EP1882820A1 Microcircuit cooling and blade tip blowing |
| 01/30/2008 | EP1882819A1 Integrated platform, tip, and main body microcircuits for turbine blades |
| 01/30/2008 | EP1882818A1 Serpentine microcircuit vortex turbulators for blade cooling |
| 01/30/2008 | EP1882817A2 Dust hole dome blade |
| 01/30/2008 | EP1882816A2 Radially split serpentine cooling microcircuits |
| 01/30/2008 | EP1882815A1 Turbomachine comprising a system for cooling the downstream face of a centrifugal compressor impeller |
| 01/30/2008 | EP1882814A2 Turbine vanes with airfoil-proximate cooling seam |
| 01/30/2008 | EP1882813A2 A mounting disc for turbine or compressor blades |
| 01/30/2008 | EP1882085A2 BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (7FA+e, STAGE 2) |
| 01/30/2008 | EP1882084A2 Blade/disk dovetail backcut for blade/disk stress reduction (9fa+e, stage 2) |
| 01/30/2008 | EP1882083A1 Locking arrangement for radial entry turbine blades |
| 01/30/2008 | EP1337378B1 A method for manufacturing a vane to a gas turbine component and a method for manufacturing a gas turbine component |
| 01/30/2008 | EP1320661B1 Gas turbine blade |
| 01/30/2008 | CN101113676A Low stress turbins bucket |
| 01/30/2008 | CN100365257C Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 01/29/2008 | US7323247 A multilayer protective coating for silica-based turbine engine parts which includes a cation diffusion barrier of silicon nitride, a metallic silicate oxidation barrier, a water impervious environmental barrier, and a stabilized zirconia thermal barrier |
| 01/29/2008 | US7322797 Damper cooled turbine blade |
| 01/29/2008 | US7322796 Turbine vane construction |
| 01/29/2008 | US7322795 Firm cooling method and hole manufacture |
| 01/29/2008 | US7322101 Turbine engine disk spacers |
| 01/27/2008 | CA2594585A1 Turbine vanes with airfoil-proximate cooling seam |
| 01/24/2008 | WO2008009878A1 Method for characterising the profile of a surface |
| 01/24/2008 | WO2008009270A2 Method for repairing a guide blade segment for a jet engine |
| 01/24/2008 | WO2008009267A1 Method for repairing turbine blades |
| 01/24/2008 | US20080019841 Integrated platform, tip, and main body microcircuits for turbine blades |
| 01/24/2008 | US20080019840 Serpentine microcircuit vortex turbulatons for blade cooling |
| 01/24/2008 | US20080019839 Microcircuit cooling and tip blowing |
| 01/24/2008 | US20080019838 Blades |
| 01/24/2008 | US20080019837 Method for increasing the fatigue life of a blade root of a turbomachine blade |
| 01/24/2008 | US20080019836 Damping Arrangement for Guide Vanes |
| 01/24/2008 | US20080019835 Gas turbine blade shroud |
| 01/24/2008 | DE202004021411U1 Bauteil mit Druckeigenspannungen und Vorrichtung zur Erzeugung von Druckeigenspannungen Component having compressive residual stresses and apparatus for producing compressive residual stresses |
| 01/24/2008 | DE102006033799A1 Verfahren zur Reparatur von Turbinenschaufeln A method of repairing turbine blades |
| 01/24/2008 | DE102006033299A1 Verfahren zur Reparatur eines in BLISK-Bauweise ausgeführten Verdichterrotors Method for repairing a compressor rotor executed in BLISK construction |
| 01/24/2008 | DE102006033298A1 Manufacturing or repairing gas turbine compressors implemented using bladed-disc technology, welds blade extensions suitable for finishing to required dimensions, to oversized forged blank disc |
| 01/24/2008 | DE102006033297A1 Repair process for blades of gas turbine compressor involves heat treatment using laser beam in locally limited region influenced by welding heat |
| 01/24/2008 | DE102006026968A1 Strömungsarbeitsmaschine mit Rotoren hoher spezifischer Energieabgabe Turbomachine rotors with high specific power output |
| 01/24/2008 | DE102005056182B4 Verfahren und Anordnung zum Erzeugen von Energie an einer Antriebswelle (Tornadoturbine) Method and apparatus for generating power to a drive shaft (Tornado turbine) |
| 01/24/2008 | CA2656795A1 Flow deflection devices and methods for energy capture machines |
| 01/23/2008 | EP1881163A1 Highly slenderness rotor |
| 01/23/2008 | EP1881158A2 Blades |
| 01/23/2008 | EP1881157A1 Serpentine microcircuits for local heat removal |
| 01/23/2008 | EP1881156A2 Turbine vane with removable platform inserts |
| 01/23/2008 | EP1881155A1 Apparatus for designing turbines and turbine blades |
| 01/23/2008 | EP1881154A1 Repair process for coated articles |
| 01/23/2008 | EP1880793A2 High pressure single turbine blade tip repair with laser cladding |
| 01/23/2008 | EP1880789A1 Method of manufacturing a single-piece bladed disc and mould for implementing the method |
| 01/23/2008 | EP1880787A1 Process for repairing turbine engine components |
| 01/23/2008 | EP1759091B8 Turbine wheel in a waste gas turbine of a waste gas turbocharger |
| 01/23/2008 | CN101109292A Process for manufacturing a blisk and mold for implementing the process |
| 01/23/2008 | CN101109291A Machine components and methods of fabricating |
| 01/23/2008 | CN100363604C Methods and apparatus for cooling gas turbine engine blade tips |
| 01/23/2008 | CN100363594C Manufacturing method of small sized turbine |
| 01/23/2008 | CN100363593C 叶片和燃气轮机 And turbine blades |
| 01/22/2008 | US7320574 Turbomachine |