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)
10/2000
10/03/2000US6126400 Thermal barrier coating wrap for turbine airfoil
10/03/2000US6126397 Trailing edge cooling apparatus for a gas turbine airfoil
10/03/2000US6126396 AFT flowing serpentine airfoil cooling circuit with side wall impingement cooling chambers
10/03/2000US6126394 Turbine nozzle and moving blade of axial-flow turbine
10/03/2000US6126357 Friction- and form-grip connection of rotating components
10/03/2000US6125626 Active rotor stage vibration control
09/2000
09/28/2000WO2000057032A1 Guide blade and guide blade rim for a fluid-flow machine and component for delimiting a flow channel
09/28/2000WO2000057031A1 Gas turbine rotor with internally-cooled gas turbine blade
09/28/2000WO2000057030A1 Turbomachine blade
09/28/2000WO2000057029A1 Turbine blade
09/28/2000DE19913269A1 Turbinenschaufel Turbine blade
09/28/2000DE19913265A1 Turbomaschinenschaufel Turbomachine blade
09/27/2000EP1039096A2 Turbine nozzle
09/27/2000EP1038092A1 Cover plate for gas turbine rotor
09/27/2000CN1056909C Axial-flow gas turbine
09/26/2000US6123898 Low heat expansion alloy
09/26/2000US6123504 Steam-turbine power plant and steam turbine
09/26/2000US6123145 Synthetic jet actuators for cooling heated bodies and environments
09/19/2000US6120249 Gas turbine blade platform cooling concept
09/19/2000US6120245 Cooling structure around L shaped vertical type gas turbine output shaft
09/19/2000US6120244 Structure and method for inserting inserts in stationary blade of gas turbine
09/14/2000WO2000053909A1 Gas turbine engine
09/14/2000WO2000053897A1 Gas turbine engine
09/14/2000WO2000053896A1 Turbine blade and method for producing a turbine blade
09/14/2000WO2000053895A1 Turbine rotor disk
09/14/2000CA2366842A1 Turbine blade and method for producing a turbine blade
09/13/2000EP1035302A2 Multiple impingement airfoil cooling
09/12/2000US6118098 Turbine rotor modernization and repair method
09/12/2000US6117560 A ceramic surface coatings has a cubic pyrochlore structure
09/12/2000US6116854 Gas turbine moving blade
09/12/2000US6115917 Single position turbine rotor repair method
09/12/2000CA2214826C Gas turbine stationary blade
09/08/2000WO2000052307A1 High temperature erosion resistant, abradable thermal barrier composite coating
09/08/2000WO2000051761A1 Method and apparatus for production of a cast component
09/08/2000CA2714871A1 Method and apparatus for production of a cast component
09/08/2000CA2663076A1 Method and apparatus for production of a cast component
09/07/2000DE19909899A1 Fan blade with variable profile geometry, in which profile geometry can be altered by elastic deformation in at least one part region over blade height
09/06/2000EP1033476A2 Heat exchange flow circuit for a turbine rotor
09/06/2000EP1032749A1 Rotor with integrated blading
09/06/2000EP0811752B1 Centrifugal gas turbine
09/06/2000EP0724658B1 Protective coating
09/06/2000CN1056212C 燃气轮机 Gas turbine
09/05/2000US6115307 Method and structure for rapid enablement
08/2000
08/31/2000WO2000050779A1 Centrifugal air flow control
08/30/2000EP1031751A1 Enhanced fan and fan drive assembly
08/29/2000US6110604 Metallic article having a thermal barrier coating and a method of application thereof
08/29/2000US6110555 Heat resistant oxide, oxygen-free component and refractory metal each in form of curved tapes joined with each other forming multilayer curved band-like chips randomly interlaced in a compact three dimensioned pattern; heat, crack resistant
08/29/2000US6109877 Turbine blade-to-disk retention device
08/29/2000US6109873 Shield for masking a flow directing assembly
08/29/2000US6109869 Steam turbine nozzle trailing edge modification for improved stage performance
08/29/2000US6109867 Cooled turbine-nozzle vane
08/29/2000US6109843 Shield assembly for masking a stator of a rotary machine
08/29/2000US6109022 Turbofan with frangible rotor support
08/29/2000US6109019 Steam cooled gas turbine system
08/29/2000CA2051133C Gas turbine, gas turbine blade used therefor and manufacturing method for gas turbine blade
08/24/2000WO2000022287A3 Gas turbine engine
08/23/2000EP1029153A1 Turbine engine vane segment
08/23/2000EP1029115A1 Product,especially a gas turbine component, with a ceramic heat insulating layer
08/23/2000EP1029101A1 Product, especially a gas turbine component, with a ceramic heat insulating layer
08/22/2000US6106766 Material for gas turbine disk
08/22/2000US6106234 Rotary assembly
08/22/2000US6106233 Method for linear friction welding and product made by such method
08/22/2000US6106231 Partially coated airfoil and method for making
08/22/2000US6106188 Joint between two joint partners, and its use
08/22/2000US6105359 Efficiency enhanced turbine engine
08/17/2000WO2000047792A1 Method for producing fibre reinforced metallic components
08/16/2000EP1028232A1 Fastening of turbomachine rotor blades
08/16/2000EP1028231A1 Fastening of turbomachine rotor blades
08/16/2000EP1028230A1 Cooled gas turbine component with adjustable cooling
08/16/2000EP1028229A1 Turbomachine blade
08/16/2000EP1028228A1 Cooling device for a turbine rotor blade platform
08/16/2000CN1263204A Fixing component of rotating blade of fluid flow machine
08/15/2000US6103993 Hollow rotor blade of columnar structure having a single crystal column in which a series of holes are laser drilled
08/15/2000US6103402 The power density is reduced and the interaction time is increased, which allows for a significant increase in temperature of the substrate immediately adjacent the molten pool at the time that solidifiction occurs, reduces cracking
08/15/2000US6103386 A thermal barrier coating for a superalloy substrate includes an aluminide or chromium-alulminum-yttrium and a metal selected from iron, cobalt, nickel, a ceramic layer has a columnar grain microstructure and alumina bond inhibitor film
08/15/2000US6102664 Blading system and method for controlling structural vibrations
08/15/2000US6102658 Trailing edge cooling apparatus for a gas turbine airfoil
08/15/2000US6102656 Segmented abradable ceramic coating
08/15/2000US6102655 Shroud band for an axial-flow turbine
08/15/2000US6102654 Turbomachine and method for cooling a turbomachine
08/15/2000CA2042350C Shroud band for a rotor wheel
08/10/2000WO2000046420A1 Thermal barrier coating resistant to sintering
08/10/2000DE19904229A1 Cooled turbine blade has shroud formed by sealing rib with integrated cooling channels connected to coolant channel in blade
08/10/2000DE10005250A1 Fiber-reinforced metal component of complicated shape, e.g. a turbine blade, is produced by plastic shaping and then diffusion welding of an assembly of loose metal-coated silicon carbide fibers between metal pieces
08/09/2000EP1026367A1 Turbomachine rotor blade tip sealing
08/09/2000EP1026366A1 Vibration damping coating
08/08/2000US6099655 Wet chemical process for removing an abrasive alumina seal tooth coating
08/08/2000US6099257 Plastically formed hybrid airfoil
08/08/2000US6099253 Gas turbine rotor blade
08/08/2000US6099252 Axial serpentine cooled airfoil
08/08/2000US6099251 Coolable airfoil for a gas turbine engine
08/08/2000US6099249 Structure of output section of jet propulsion engine or gas turbine
08/08/2000US6099248 Output stage for an axial-flow turbine
08/08/2000US6099245 Tandem airfoils
08/08/2000US6099244 Cooled stationary blade for a gas turbine
08/08/2000US6098395 Closed-loop air cooling system for a turbine engine
08/03/2000WO2000020740B1 Gas turbine engine
08/03/2000DE19903880A1 Device for generating energy, transporting gases, fluids, light fractions whilst meeting small space or low drive energy requirement has rotor profile formed on imaginary rotation ellipsoid
08/03/2000DE10003516A1 Steam turbine has high, medium and low pressure sections with two or more sections combined with each other, and rotor subjected to thermal conditioning with different thermal operating temperatures in respective pressure sections
08/02/2000EP1024251A2 Cooled turbine shroud
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