Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
07/2003
07/10/2003US20030127438 Method for producing an opening in a metallic structural part
07/10/2003US20030126800 Mixed powder deposition of components for wear, erosion and abrasion resistant applications
07/09/2003EP1326007A2 Cooling of a structure for use as a turbine blade
07/09/2003EP1326006A2 Methods and apparatus for cooling gas turbine nozzles
07/09/2003EP1326005A2 Step-down turbine platform
07/08/2003US6589677 Thermal barrier additive which reduces the rate of weight loss and recession of the substrate comprises Ta oxide and an oxide selected from MgO, CaO, SrO, BaO, Al2O3, Y2O3, La2O3, Re2O3 (where Re is a rare earth element)
07/08/2003US6589668 Graded platinum diffusion aluminide coating
07/08/2003US6589600 Turbine engine component having enhanced heat transfer characteristics and method for forming same
07/08/2003US6589011 Device for cooling a shroud of a gas turbine blade
07/08/2003US6589010 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
07/08/2003US6588103 Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade
07/08/2003CA2262854C Microturbomachinery
07/08/2003CA2262050C Steam-cooling type gas turbine
07/03/2003WO2003054357A2 Air- and steam-cooled turbine blade and method for cooling a turbine blade
07/03/2003WO2003054356A1 Thermally loaded component
07/03/2003WO2003054355A1 Gas turbine with a multiple fixing disk
07/03/2003WO2003053622A1 Workpiece with a recess which is closed from the exterior by means of a solder film and method for closing a recess by means of a solder film
07/03/2003US20030124342 Oxidation resistant coatings for niobium-based silicide composites
07/03/2003US20030123986 Device for immobilizing blades in a slot of a disk
07/03/2003US20030123977 Exhaust-gas turbine
07/03/2003US20030121507 Supercharger
07/03/2003US20030121270 Engine core rotor shaft structure for gas turbine engine
07/02/2003EP1323909A2 Supercharger
07/02/2003EP1323691A2 Silicon based substrate with environmental/thermal barrier layer
07/02/2003EP1323690A2 Barrier layer for silicon containing substrate
07/02/2003EP1323689A2 Silicon based substrate with a CTE compatible layer on the substrate
07/02/2003EP1323490A2 Apparatus and method for friction welding
07/02/2003EP1322838A1 Moving blade for a turbo-machine and turbo-machine
07/02/2003CN1427085A High-temp corrosion-resisting alloy, heat barrier coating material, turbine structural member and gas turbine
07/02/2003CN1113153C Cooling system of front edge area of hollow vane of gas turbine
07/01/2003US6586118 Bonded niobium silicide and molybdenum silicide composite articles using semi-solid brazes
07/01/2003US6586115 Yttria-stabilized zirconia with reduced thermal conductivity
06/2003
06/27/2003WO2003059569A2 Method of forming turbine blade root
06/27/2003CA2431889A1 Method of forming turbine blade root
06/27/2003CA2414744A1 Supercharger
06/27/2003CA2366325A1 Method of forming turbine blade root
06/26/2003WO2003052240A2 Gas turbine system
06/26/2003US20030118874 Evaporation electron beam vapor deposition; protective coating for nickel, cobalt alloy
06/26/2003US20030118873 Stabilized zirconia thermal barrier coating with hafnia
06/26/2003US20030118447 Bladed member, in particular for an axial turbine of an aircraft engine
06/26/2003US20030118445 Foil formed structure for turbine airfoil
06/26/2003US20030118444 Foil formed structure for turbine airfoil tip
06/26/2003US20030116549 Rotor and method for welding an element of a rotor
06/26/2003US20030116542 Laser consolidation apparatus for manufacturing precise structures
06/26/2003US20030116278 Gas distributor for vapor coating method and container
06/26/2003US20030116240 High and low pressure integrated type turbine rotor and process for producing the same
06/26/2003US20030116237 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature
06/26/2003US20030115922 Transverse utrasound peening of blades on a rotor
06/26/2003US20030115882 Foil formed cooling area enhancement
06/26/2003US20030115881 Ventilated thermal barrier coating
06/25/2003EP1321712A1 Integral surface features for CMC components and method therefor
06/25/2003EP1321630A2 System for connecting and locking rotor blades of an axial compressor
06/25/2003EP1321629A2 Ventilated thermal barrier coating
06/25/2003EP1321628A2 Airfoil for a turbine nozzle of a gas turbine engine and method of making same
06/25/2003EP1321627A1 Air and steam-cooled turbine blade and method for cooling a turbine blade
06/25/2003EP1321626A1 Gasturbine rotor
06/25/2003EP1321625A1 Method for removing a metallic layer
06/25/2003EP1321542A1 Thermal barrier coating systems and materials
06/25/2003EP1321538A2 Gas distributor for vapor coating method and apparatus
06/25/2003EP1321536A2 Process for rejuvenating a diffusion aluminide coating
06/25/2003EP1321214A1 Workpiece comprising a cavity covered by a soldering foil and method for covering a cavity using a soldering foil
06/25/2003EP1320685A1 Multi-stage impeller
06/25/2003EP1320662A1 Seal system
06/25/2003EP1320661A1 Gas turbine blade
06/25/2003EP1060284B1 Protecting layer
06/25/2003EP1040253B1 Cooling arrangement for turbine rotor
06/25/2003EP0805263B1 Vane for gas turbine
06/24/2003US6582834 Overcoating interior passageway with protective coating; gas turbine engines
06/24/2003US6582812 Article made of a ceramic foam joined to a metallic nonfoam, and its preparation
06/24/2003US6582779 Silicon nitride components with protective coating
06/24/2003US6582772 Heating and diffusing aluminum, silicon, and hafnium into platinum layer to form protective coating for aircraft gas turbine blades; aluminiding
06/24/2003US6582585 Chemical macrographic etching and a subsequent step of electrochemical etching by means of a bath containing phosphoric acid and at least one weak acid for revealing structure for a component made of a single-crystal superalloy
06/24/2003US6582584 Method for enhancing heat transfer inside a turbulated cooling passage
06/24/2003US6582197 Method of investment casting with casting identification
06/24/2003US6582195 Compressor rotor blade spacer apparatus
06/24/2003US6582194 Gas-turbine blade and method of manufacturing a gas-turbine blade
06/24/2003US6582189 Turbo machines
06/24/2003US6582187 Methods and apparatus for isolating gas turbine engine bearings
06/24/2003US6582186 Vane assembly
06/24/2003US6581978 Connector tube for a turbine rotor cooling circuit
06/21/2003CA2412455A1 Stabilized zirconia thermal barrier coating with hafnia
06/19/2003US20030114081 Fixture for clamping a gas turbine component and its use in shaping the gas turbine component
06/19/2003US20030113559 Barrier layer for silicon containing substrate
06/19/2003US20030113553 Silicon based substrate with a CTE compatible layer on the substrate
06/19/2003US20030113552 Silicon based substrate with environmental/thermal barrier layer
06/19/2003US20030113206 Selective step turbine nozzle
06/19/2003US20030113201 Methods and apparatus for cooling gas turbine nozzles
06/18/2003EP1319842A1 Rotor or rotating element for turbocompressor
06/18/2003EP1319805A1 Rotor or rotor element for turbocompressors
06/18/2003EP1319804A1 Stator blade platform for a gas turbine engine
06/18/2003EP1319803A2 Coolable rotor blade for an industrial gas turbine engine
06/18/2003EP1319802A2 Turbine nozzle segment and method of repairing same
06/18/2003EP1319730A1 High temperature corrosion resistant alloy, thermal barrier coating material with metal bonding layer, and gas turbine using high temperature corrosion resistant alloy
06/18/2003EP1319729A1 High temperature resistant part, made of single-crystal or polycrystalline nickel-base superalloy
06/18/2003EP1319473A1 Fixture for clamping a gas turbine component and its use in shaping the gas turbine component
06/18/2003EP1163426B1 Turbomachine blade
06/18/2003EP1112440B1 Turbine guide blade
06/18/2003CN1424490A Cooling rotor blade for industrial gas turbine engine
06/17/2003US6579066 Turbine bucket
06/17/2003US6579061 Selective step turbine nozzle
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