| 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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| 01/14/2009 | EP1625290B1 Turbocharger system for an internal combustion engine |
| 01/14/2009 | EP1472042B1 Hand held powder-fed laser fusion welding torch |
| 01/14/2009 | CN201180564Y Blade tip winglet of turbine or steamer movable blade |
| 01/14/2009 | CN101344015A Tinsel for turbomachine vane |
| 01/14/2009 | CN101344014A Airfoil for use in rotary machines and method for fabricating same |
| 01/14/2009 | CN101344013A Turbomachine rotor assembly |
| 01/13/2009 | US7476703 In-situ method and composition for repairing a thermal barrier coating |
| 01/13/2009 | US7476450 Fourth generation single crystal superalloy substrate having a bond coat containing Ni; Pt, Pd and/or Ir; Al, Co, Cr, Mo, Re, Ta and W and overcoated with a barrier coating, e.g., ZrO2 stabilized with Y2O3, Gd2O3, Ce2O3 or Sc2O3; turbine blades or vanes; low aluminum content (5-10%) |
| 01/13/2009 | US7476085 Blade/disk dovetail backcut for blade/disk stress reduction (6FA+E, stage2) |
| 01/13/2009 | US7476084 Blade/disk dovetail backcut for blade/disk stress reduction (6FA and 6FA+e, stage 1) |
| 01/13/2009 | US7476083 Blade/disk dovetail backcut for blade/disk stress reduction (7FA+e, stage 1) |
| 01/13/2009 | US7476080 Impeller for fluid transmitting device and method of manufacturing the same |
| 01/13/2009 | US7476078 Rotor with core surrounded by shielding rings |
| 01/13/2009 | CA2636924A1 Turbomachine rotor assembly |
| 01/13/2009 | CA2636922A1 Foil for turbomachine blade |
| 01/13/2009 | CA2448802C Turbine blade with sealing element |
| 01/13/2009 | CA2409382C Blade for turbine engine |
| 01/13/2009 | CA2404187C Improved flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine |
| 01/13/2009 | CA2398316C Method and apparatus for non-parallel turbine dovetail faces |
| 01/13/2009 | CA2359049C Device for fixing a turbine ferrule |
| 01/13/2009 | CA2350655C Method for making self-brazing components using powder metallurgy |
| 01/13/2009 | CA2349692C Hammer attachment blade locking device on a disk |
| 01/08/2009 | WO2009005721A1 Turbine vane restoration system |
| 01/08/2009 | WO2008140479A3 Impact resistant thermal barrier coating system |
| 01/08/2009 | US20090010765 Reinforced Airfoils |
| 01/08/2009 | US20090010762 Damper for turbomachine vanes |
| 01/08/2009 | DE102007031712A1 Vorrichtung und Verfahren zum Einspannen von beschaufelten Rotorscheiben eines Strahltriebwerkes Apparatus and method for clamping of the bladed rotor discs of a jet engine |
| 01/08/2009 | DE102007031711A1 Gehäusedeckbandsegment-Aufhängung Housing shroud segment suspension |
| 01/08/2009 | DE102007029728A1 Verfahren und Vorrichtung zur Reparatur von Blisks von Gasturbinen Method and apparatus for the repair of gas turbine blisks |
| 01/07/2009 | EP2012243A1 Aerodynamic design optimization using knowledge extraction from analyzing unstructured surface meshes |
| 01/07/2009 | EP2011969A1 Turbine assembly and method of fixing a mounting element |
| 01/07/2009 | EP2011968A2 Angled on-board injector |
| 01/07/2009 | EP2011967A1 Rotor shaft assembly and manufacturing method therefore |
| 01/07/2009 | EP2011966A2 Device for supplying ventilation air to the vanes of a low-pressure turbine of a gas turbine engine |
| 01/07/2009 | EP2011965A2 Method and device for clamping bladed rotor discs of a jet engine |
| 01/07/2009 | EP2011964A1 Corrosion protective coating through cold spray |
| 01/07/2009 | EP2011901A1 Component with a ceramic layer in which particles are dispersed, and method for producing same |
| 01/07/2009 | EP2011777A2 Articles for high temperature service and methods for their manufacture |
| 01/07/2009 | EP2011586A1 Investment casting cores and methods |
| 01/07/2009 | EP2010773A2 Blade for a turbine |
| 01/07/2009 | EP2010757A1 Turbine blade |
| 01/07/2009 | CN101341312A Diagonal flow turbine, or radial turbine |
| 01/07/2009 | CN101341001A Method of producing a welded rotor of a low-pressure steam turbine by means of build-up welding and stress-free annealing |
| 01/07/2009 | CN101337299A Welding manufacture method of hollow stationary blade of steam turbine |
| 01/07/2009 | CN100449023C Booster turbine and method of manufacturing the same |
| 01/06/2009 | US7473073 Turbine blade with cooled tip rail |
| 01/06/2009 | US7473072 Turbine blade tip and shroud clearance control coating system |
| 01/06/2009 | CA2636665A1 Device for supply of ventilation air to low pressure turbine blades of a gas turbine engine; segment for axial stoppage and ventilation of low pressure turbine blades |
| 01/02/2009 | DE102008002906A1 Gewölbte Spitzenkappe und zugehöriges Verfahren Curved tip cap and associated method |
| 01/02/2009 | DE102007029367A1 Schaufel mit Tangentialstrahlerzeugung am Profil Shovel with Tangentialstrahlerzeugung on profile |
| 01/02/2009 | DE102007028939A1 Gas turbine module, particularly compressor module or turbine module for gas turbine formed as aircraft engine, has guide vanes of guide vane ring or rotor blades of rotor blade ring is made of piezo static material |
| 01/01/2009 | US20090004023 Device for cooling the slots of a rotor disk in a turbomachine having two air feeds |
| 01/01/2009 | US20090004021 Movable impeller for a turbojet and turbojet comprising same |
| 01/01/2009 | US20090004020 Water Pump |
| 01/01/2009 | US20090004019 Axial Flow Fan |
| 01/01/2009 | US20090004018 Device for axially retaining blades mounted on a turbomachine rotor disk |
| 01/01/2009 | US20090004017 Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted |
| 01/01/2009 | US20090004013 Turbine blade nested seal and damper assembly |
| 01/01/2009 | US20090004011 Steam turbine, and intermediate support structure for holding row of long moving blades therein |
| 01/01/2009 | US20090004006 Device for cooling slots of a turbomachine rotor disk |
| 01/01/2009 | US20090003996 Labyrinth Seal in a Stationary Gas Turbine |
| 01/01/2009 | US20090003989 Blade with tangential jet generation on the profile |
| 01/01/2009 | US20090003987 Airfoil with improved cooling slot arrangement |
| 01/01/2009 | US20090000296 Turbocharger having divided housing with integral valve |
| 12/31/2008 | WO2009000728A1 Turbine arrangement and method of cooling a shroud located at the tip of a turbine blade |
| 12/31/2008 | EP2009248A1 Turbine arrangement and method of cooling a shroud located at the tip of a turbine blade |
| 12/31/2008 | EP2009247A2 Turbine blade seal and damper assembly |
| 12/31/2008 | EP2009246A2 A blade mounting |
| 12/31/2008 | EP2009245A1 Fan rotor |
| 12/31/2008 | EP2009244A1 Device for axial retention of vanes mounted on a turbomachine rotor disc |
| 12/31/2008 | EP2009243A2 Ceramic matrix composite turbine engine vane |
| 12/31/2008 | EP2009242A1 Turbomachine stator damper device |
| 12/31/2008 | EP2009241A2 Interconnected blades of a steam turbine |
| 12/31/2008 | EP2009240A2 Bimaterial turbine blade damper |
| 12/31/2008 | EP2009239A2 Blade with tangential jet production on the profile |
| 12/31/2008 | EP2009238A1 Rotor wheel for a jet engine, and jet engine comprising same |
| 12/31/2008 | EP2009237A1 Turbomachine shaft damper device |
| 12/31/2008 | EP2009236A2 A sideplate for a turbine rotor, corresponding turbine rotor and gas turbine engine |
| 12/31/2008 | EP2009235A1 Device for cooling the peripheral cavities of a turbomachine rotor disc with double air supply |
| 12/31/2008 | EP2009234A1 Device for cooling the cavities of a turbomachine rotor disc |
| 12/31/2008 | EP2009141A2 Thermal barrier system and bonding method |
| 12/31/2008 | EP2009123A1 Ni-BASED HEAT-RESISTANT ALLOY FOR GAS TURBINE COMBUSTOR |
| 12/31/2008 | EP2008758A1 Repaired gas turbine engine components and related methods |
| 12/31/2008 | EP2008756A1 Method and device for repairing BLISKs |
| 12/31/2008 | EP1907671B1 Gas-turbine blade ring |
| 12/31/2008 | EP1392957B1 Abradeable seal system |
| 12/31/2008 | EP1313932B1 Thermal barrier coating system |
| 12/31/2008 | EP1107867B1 Removal of thermal barrier coatings |
| 12/31/2008 | CN201173140Y Pneumatic motor |
| 12/31/2008 | CN101336335A Turbine rotor blade, turbine rotor and steam turbine comprising them |
| 12/31/2008 | CN101333995A Expansion machine rotor for highly pressurized liquid throttling |
| 12/31/2008 | CN101333942A Device for axial retention of vanes mounted on a turbomachine rotor disc |
| 12/31/2008 | CN101333941A 穹顶形的末梢帽及相关方法 Dome-shaped tip cap and related methods |
| 12/31/2008 | CN101333940A Rotor wheel for a jet engine, and jet engine comprising same |
| 12/31/2008 | CN101333939A Turbomachine shaft damper device |
| 12/31/2008 | CN101333938A Device for cooling the peripheral cavities of a turbomachine rotor disc with double air supply |
| 12/31/2008 | CN101333937A Device for cooling the cavities of a turbomachine rotor disc |
| 12/31/2008 | CN101333936A Steam turbine, and intermediate support structure for holding row of long moving blades therein |
| 12/31/2008 | CN100447387C Fatigue failure diagnostic method of turbocharger and fatigue failure diagnostic apparatus for turbocharger |
| 12/31/2008 | CN100447374C Turbine vane and casting assemble for mfg. same |