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)
12/1996
12/18/1996EP0748667A1 Removal of inserts from the interior of turbine airfoils
12/17/1996US5585163 Ceramic-metal composite assembly
12/17/1996US5584663 Formed of nickel-based alloy containing specified amounts of chromium, aluminum, cobalt, tantalum, rhenium, hafnium, zirconium, carbon, silicon, boron
12/17/1996US5584662 Laser shock peening for gas turbine engine vane repair
12/17/1996US5584660 Increased impact resistance in hollow airfoils
12/17/1996US5584659 Device for fixing turbine blades and for eliminating rotor balance errors in axially flow-through compressors or turbines of gas turbine drives
12/17/1996US5584658 Turbocompressor disk provided with an asymmetrical circular groove
12/12/1996DE19603515C1 Spraying material used to form corrosive-resistant coating
12/11/1996EP0747573A1 Gas turbine rotor with remote support rings
12/11/1996EP0747151A1 Method and apparatus for removing cores from castings
12/10/1996US5582657 Heat-resistant, ferritic cast steel having high castability and exhaust equipment member made thereof
12/10/1996US5582077 System for balancing and damping a turbojet engine disk
12/10/1996US5581996 Method and apparatus for turbine cooling
12/10/1996US5581994 Method for cooling a component and appliance for carrying out the method
12/05/1996WO1996038639A1 A damped element
12/04/1996EP0745756A1 Fixture and method for the assembly of runner blades
12/04/1996EP0745755A1 Flow directing element for a turbine engine
12/03/1996US5580219 Disc assembly
12/03/1996US5580218 Of an axial-flow turbomachine
12/03/1996US5580183 Gas turbine engine spline arrangement
12/03/1996US5579644 Turbo-jet equipped with inclined balancing disks within the rotor of the high pressure compressor and process for producing such disks
12/03/1996CA2174367A1 Turbine cooling cycle
11/1996
11/27/1996EP0744529A1 Methods for coating and securing multi-vane nozzle segments
11/26/1996US5577889 Gas turbine cooling blade
11/26/1996US5577884 Structure for a stationary cooled turbine vane
11/20/1996EP0533677B1 A process for producing a thermal barrier coating for substrates.
11/19/1996US5576079 Braided fibers impregnated with resin, reverse thrust device for gas turbine engines
11/19/1996US5575623 Drum rotor for an axial-flow turbomachine
11/19/1996US5575620 Turbine blade assembly
11/19/1996US5575617 Apparatus for cooling an axial-flow gas turbine
11/19/1996US5575616 Turbine cooling flow modulation apparatus
11/14/1996WO1996035878A1 Multi-stage rotary fluid handling apparatus
11/14/1996WO1996035826A1 Porous thermal barrier coating
11/14/1996DE19516834A1 Internal stress rolling device for interior surface of work piece
11/14/1996DE19516829A1 Fossil fuel gas turbine for power plant
11/13/1996EP0742634A2 Compound shaft
11/13/1996EP0742347A2 Turbine blade cooling
11/12/1996US5573862 Single crystal oxide turbine blades
11/12/1996US5573604 Remelting, alloying blade edge; erosion resistance
11/12/1996US5573377 Assembly of a composite blade root and a rotor
11/12/1996US5573375 Turbine engine rotor blade platform sealing and vibration damping device
11/06/1996EP0740977A1 Containerless method of producing crack free metallic articles
11/06/1996EP0740976A1 Method of repairing single crystal metallic articles
11/06/1996CN1135014A Guide blade for steam turbines
10/1996
10/31/1996WO1996034181A1 Increased impact resistance in hollow airfoils
10/31/1996WO1996034130A1 Metal component with a high-temperature protection coating system and a method of coating the component
10/30/1996EP0739443A1 Cooling of turbine blade
10/29/1996US5569338 Consists of specific ratios of carbon, silicon, nickel, chromium, molybdenum, manganese, vanadium and balance iron and impurities; toughness
10/29/1996US5569018 Technique to prevent or divert cracks
10/23/1996EP0738369A1 Gas turbine airfoil
10/23/1996EP0738368A1 An improved airfoil structure
10/23/1996CN1133936A 燃气轮机 Gas turbine
10/22/1996US5567116 Arrangement for clipping stress peaks in a turbine blade root
10/17/1996DE19513517A1 Method of manufacturing blades for pump or turbine wheels of fluid coupling
10/16/1996EP0737120A1 Method for making gas turbine engine blade attachment slots
10/15/1996US5564902 Gas turbine rotor blade tip cooling device
10/15/1996US5564896 Method and apparatus for shaft sealing and for cooling on the exhaust-gas side of an axial-flow gas turbine
10/10/1996WO1996031687A1 Method and composite for protection of thermal barrier coating with an impermeable barrier coating
10/10/1996WO1996031636A1 Erosion/corrosion protective coating for high-temperature components
10/10/1996WO1996031293A1 Method and composite for protection of thermal barrier coating by a sacrificial surface coating
10/09/1996EP0736668A1 Ceramic blade attachment system
10/08/1996US5562419 Shrouded fan blisk
10/08/1996US5562409 Air cooled gas turbine aerofoil
10/08/1996US5562404 Vaned passage hub treatment for cantilever stator vanes
10/08/1996CA2070188C Wheel lock, centering and drive means and turbocharger impeller combination
10/02/1996EP0735255A1 Compressor rotor cooling system for a gas turbine
10/02/1996EP0735243A2 Inner turbine shell with bucket tip clearance control
10/02/1996EP0735241A1 Method for reducing internal hot corrosion in gas turbine engine components
10/02/1996EP0735240A1 Gas turbine bucket
10/02/1996EP0735239A1 Adapting basic gas turbine construction to drive generators operating at different frequencies
10/02/1996EP0735238A1 Closed or open circuit cooling of turbine rotor components
10/02/1996DE19515464C1 Radial compressor for exhaust gas turbocharger
10/02/1996DE19512138A1 Axial-flow working or power machine
09/1996
09/26/1996WO1996029586A1 Method of balancing a bladed rotor
09/24/1996US5558500 Elastomeric seal for axial dovetail rotor blades
09/24/1996US5558497 Airfoil vibration damping device
09/24/1996US5558496 Removing particles from gas turbine coolant
09/18/1996EP0732481A1 Turbine rotor
09/18/1996EP0731874A1 Hollow fan blade dovetail
09/18/1996EP0731873A1 Airfoil having coolable leading edge region
09/18/1996EP0731744A1 Turbine blade repair
09/17/1996US5556257 Integrally bladed disks or drums
09/12/1996WO1996027684A1 A technique to prevent or divert cracks
09/11/1996EP0731184A1 Laser shock peened gas turbine engine compressor airfoil edges
09/11/1996EP0730704A1 Cooled turbine airfoil
09/11/1996CN1130713A Bladed rotor
09/10/1996US5554837 Interactive laser welding at elevated temperatures of superalloy articles
09/10/1996US5554005 Bladed rotor of a turbo-machine
09/10/1996US5554000 Blade profile for axial flow compressor
09/10/1996US5553370 Method for repair of steam turbine blades
09/04/1996EP0729544A1 Coolable rotor assembly
09/03/1996US5551840 Gas turbine engine blade
09/03/1996US5551623 Process for welding two blade parts
09/03/1996CA2045654C Thermal barrier coating for substrates and process for producing it
08/1996
08/29/1996DE19601819A1 Turbinenschaufel-Anordnung mit einem gekühlten Deckband Turbine blade assembly with a cooled shroud
08/29/1996DE19601818A1 Turbinenschaufel-Anordnung mit einem Deckband Turbine blade assembly with a shroud
08/27/1996US5549767 Heat treatment and repair of cobalt base superalloy articles
08/22/1996DE4445296C1 Radial compressor wheel impeller having low noise level
08/21/1996EP0727564A1 Vibration damping for turbine blades
08/21/1996EP0727563A2 Turbine engine rotor blade vibration damping device
1 ... 279 280 281 282 283 284 285 286 287 288 289 290 291 292 293 294 295 296 297 298 299 ... 330