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)
08/2003
08/07/2003US20030148140 High temperature corrosion resistant alloy, thermal barrier coating material, and gas turbine using high temperature corrosion resistant alloy
08/07/2003US20030147750 Cooled turbine blade
08/07/2003US20030147748 Split blade frictional damper
08/07/2003US20030145916 12Cr Alloy steel for a turbine rotor
08/06/2003EP1333181A1 Low noise fan stationary blade
08/06/2003EP1333155A1 Cooled trailing edge for a high pressure turbine rotor blade
08/06/2003EP1333154A2 Cooled turbine blade
08/06/2003EP1332824A2 Method for manufacturing turbine blade and manufactured turbine blade
08/06/2003EP1332016A1 Process for drilling holes in a metallic workpiece having a thermal barrier coating
08/06/2003CN1434894A Axial flow turbine type rotor mechanical device for elastic fluid
08/05/2003US6602814 Thermal insulating material and method of producing same
08/05/2003US6602553 Process for producing a ceramic thermal barrier layer for gas turbine engine component
08/05/2003US6602548 Ceramic turbine blade attachment having high temperature, high stress compliant layers and method of fabrication thereof
08/05/2003US6602542 Device for cleaning an article
08/05/2003US6602053 Cooling structure and method of manufacturing the same
08/05/2003US6602052 Airfoil tip squealer cooling construction
08/05/2003US6602049 Compressor stator having a constant clearance
08/05/2003US6602047 Methods and apparatus for cooling gas turbine nozzles
08/05/2003CA2263576C Stationary blade of gas turbine
07/2003
07/31/2003WO2003062637A1 Rotor blade for a wind power installation with a damping device
07/31/2003WO2003062607A1 Cooled component for a gas turbine
07/31/2003WO2003062606A1 Method for changing the frequency of blades for thermal turbo-machines
07/31/2003WO2003062605A1 Method and apparatus for increasing welding rates for high aspect ratio welds
07/31/2003US20030143079 Gas turbine engine
07/31/2003US20030143078 Rotor or rotor element for a turbocompressor
07/31/2003US20030143077 Fastening of the blades of a compression machine
07/31/2003US20030143075 Turbulated cooling holes
07/31/2003US20030143074 Method for manufacturing turbine blade and manufactured turbine blade
07/31/2003US20030143068 Three-dimensional axial-flow turbine stage
07/31/2003US20030143065 Turbine rotor
07/31/2003US20030143064 Nozzle-vane band for a gas turbine engine
07/31/2003US20030140632 Air impingement cooling system
07/31/2003US20030140493 Pneumatic press vane lift installation tool
07/31/2003DE10227426C1 Bladed rotor for compact flow machines has compression and induction side each with own blade set, differing from each other in geometry and number of blades
07/30/2003EP1331362A2 Geothermal steam turbine
07/30/2003EP1331361A1 Turbine blade and casting device for producing a turbine blade
07/30/2003EP1331360A2 Arrangement of vane and blade aerofoils in a turbine exhaust section
07/30/2003EP1115963B1 Gas turbine engine
07/30/2003EP1092081B1 Rotor for a turbomachine
07/30/2003CN1432721A Booster
07/30/2003CN1116512C Nozzle for gas turbine
07/29/2003US6599568 Method for cooling engine components using multi-layer barrier coating
07/29/2003US6599092 Methods and apparatus for cooling gas turbine nozzles
07/29/2003US6599088 Dynamically sealing ring fan shroud assembly
07/29/2003US6598781 Article having turbulation and method of providing turbulation on an article
07/29/2003CA2263521C Structure and method for inserting inserts in stationary blade of gas turbine
07/24/2003WO2003060292A1 Turbine comprising at least four stages and use of a turbine blade with a reduced mass
07/24/2003WO2003060194A1 High-temperature protective coating
07/24/2003US20030138641 Silicon nitride, a silicon carbide and Sialon, and a surface protection layer of group 3a stabilizer zirconia with total amount of aluminum and silicon is suppressed to </= 1%
07/24/2003US20030138322 Moving blade for a high pressure turbine, the blade having a trailing edge of improved thermal behavior
07/24/2003US20030138320 Gas turbine cooling system
07/24/2003US20030136001 Method of producing rotary vane member and rotary vane member
07/23/2003EP1329639A1 Centripetal air bleed device
07/23/2003EP1329593A1 Turbine-blade
07/23/2003EP1329592A1 Turbine with at least four stages and utilisation of a turbine blade with reduced mass
07/23/2003EP1329591A1 Axial compressor disc for a turbomachine with a centripetal air-bleed system
07/23/2003EP1329590A2 Coolant recirculation type gas turbine
07/23/2003EP1329589A1 Rotor configuration for a turbomachine
07/23/2003EP1135348B1 Method for joining ceramic to metal
07/23/2003CA2418241A1 Moving blade of a high-pressure turbine equipped with a trailing edge with improved thermal properties
07/22/2003US6596523 Sialyltransferase for use in the diagnosis and treatment of inflammation and cancer
07/22/2003US6595755 Configuration for axial retention of blades in a disc
07/22/2003US6595751 Composite rotor having recessed radial splines for high torque applications
07/22/2003US6595750 Component of a flow machine
07/22/2003US6595749 Turbine airfoil and method for manufacture and repair thereof
07/22/2003US6595748 Trichannel airfoil leading edge cooling
07/22/2003US6595741 Pre-swirl nozzle carrier
07/22/2003US6595401 Blade maintenance tool, and its application to friction welding of blades
07/17/2003WO2003058038A1 Vane wheel for radial turbine
07/17/2003US20030133803 Turbomachine rotor arrangement
07/17/2003US20030133802 Turbine blande/vane
07/17/2003US20030133799 Closed loop steam cooled airfoil
07/17/2003US20030133798 Gas turbine engine aerofoil
07/17/2003US20030133797 Gas turbine engine aerofoil
07/17/2003US20030133795 Crossover cooled airfoil trailing edge
07/17/2003US20030133788 Axial compressor disk for a turbomachine with centripetal air bleed
07/17/2003US20030133787 Device for straightening the flow of air fed to a centripetal bleed in a compressor
07/17/2003US20030133786 Gas turbine and turbine rotor for a gas turbine
07/17/2003US20030132119 Turbine and manufacturing method therefor
07/16/2003EP1327747A2 Crossover cooled airfoil trailing edge
07/16/2003EP1327704A1 Thermal barrier coating and process therefor
07/16/2003EP1327698A2 Thermally-stabilized thermal barrier coating and process therefor
07/16/2003EP1327056A1 Fan blade compliant shim
07/16/2003EP1327006A1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
07/16/2003CN1429968A Method and device for cooling gas turbine nozzle
07/15/2003US6594533 System and method for performing electronic triage of a turbine part
07/15/2003US6593540 Hand held powder-fed laser fusion welding torch
07/15/2003US6592330 Method and apparatus for non-parallel turbine dovetail-faces
07/15/2003US6591873 Turbo fan aspirator
07/10/2003WO2003056139A1 A single or multiple bladed rotor
07/10/2003WO2003055672A1 Foam wall combustor construction
07/10/2003WO2003055634A1 Method for making a blade ring
07/10/2003US20030129378 Thermally-stabilized thermal barrier coating and process therefor
07/10/2003US20030129338 Integral surface features for cmc components and method therefor
07/10/2003US20030129316 A thermal-insulating material contains yttria-stabilized zirconia (YSZ) alloyed atleast a third oxide (to increase the lattice energy of thermal barrier coating), and also contain carbon, oxycarbides, carbides and/or a carbon-containing gas
07/10/2003US20030129061 Multi-component hybrid turbine blade
07/10/2003US20030129060 Indentor arrangement
07/10/2003US20030129056 Stator vane arrangement for rotating machinery
07/10/2003US20030129055 Step-down turbine platform
07/10/2003US20030129054 Methods and apparatus for cooling gas turbine nozzles
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