Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
11/2001
11/21/2001EP1155760A1 Method for producing a casting of high thermal load
11/21/2001EP1082216B1 Product with an anticorrosion protective layer and a method for producing an anticorrosion protective layer
11/21/2001CN1322892A Laser cladding process for crown damping surface of crowned gas turbine blade
11/20/2001US6318963 Gas turbine airfoil internal air system
11/20/2001US6318961 Axial turbine
11/20/2001US6318960 Gas turbine stationary blade
11/20/2001US6318346 Supercharger with new impeller and improved drive assembly
11/20/2001CA2077222C Single-cast, high-temperature, thin wall structures and methods of making the same
11/15/2001WO2001086130A1 A rotor unit and a method for its balancing
11/15/2001WO2001086121A1 Method for cooling a shaft in a high-pressure expansion section of a steam turbine
11/15/2001US20010041137 Steam turbine rotor shaft
11/15/2001US20010039984 Nickel alloy containing carbon, chromium, cobalt, molybdenum, titanium and aluminum is, after solution heat treatment, subjected to stabilizing treatment at a temperature 860-920 degree C. and aging at a temperature 680-760 degree C.
11/15/2001DE10022244A1 Schaufelanordnung mit Dämpfungselementen Blade arrangement with damping elements
11/14/2001EP1154126A2 Closed circuit steam cooled turbine shroud
11/14/2001EP1154125A2 Blading with damping elements
11/14/2001EP1154124A1 Impingement cooled airfoil
11/14/2001EP1154123A1 Method of cooling the shaft of a high pressure steam turbine
11/14/2001EP1153699A2 Blisk weld repair
11/14/2001EP1153157A1 Thermal barrier coating resistant to sintering
11/14/2001EP1152848A1 Method and apparatus for production of a cast component
11/13/2001US6316048 Modifying a surface roughness; ceramic matrix composite having ceramic fibers embedded in a ceramic matrix; applying the particulates onto a portion of a surface of the ceramic matrix composite to form a uniform layer; heating to bond
11/13/2001US6315518 Stationary blade of gas turbine
11/08/2001US20010038793 Blade arrangement with damping elements
11/08/2001US20010037570 Repair of coated turbine components
11/07/2001EP1152123A2 Hybrid blade with submerged ribs
11/07/2001EP1152122A2 Turbomachinery blade
11/06/2001US6312224 Relating to bladed structures for fluid flow propulsion engines
11/06/2001US6312221 End wall flow path of a compressor
11/06/2001US6312219 Narrow waist vane
11/06/2001US6311474 Combined cycle electric power plant
11/01/2001WO2001081731A1 Steam turbine comprising a blade support allocated to a rotor and/or a stator
11/01/2001US20010036407 Platelike projecting component portion of a gas turbine
11/01/2001US20010036401 Aerofoil for an axial flow turbomachine
10/2001
10/31/2001EP1149984A2 Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment
10/31/2001EP1149983A2 Film cooling for a closed loop cooled airfoil
10/31/2001EP1149982A2 A method of joining a vane cavity insert to a nozzle segment of a gas turbine
10/31/2001EP1149662A1 Method and Apparatus for disassembling a turbine blade
10/31/2001EP1148967A1 Laser welding superalloy articles
10/31/2001DE10020229A1 Verfahren und Vorrichtung zur Demontage einer Turbinenschaufel Method and apparatus for disassembling a turbine blade
10/30/2001US6310022 Hydroxylated wetting agent selected from polypropylene glycol, polyethylene glycol, glycerine, ethylene glycol, propylene glycol, chelating agent, emulsifier, crown ether
10/30/2001US6309175 Platform cooling in turbomachines
10/30/2001US6308511 Method and device for cooling guide vanes in a gas turbine plant
10/30/2001US6308407 Method of manufacturing a plurality of steam turbines for use in various applications
10/25/2001WO2001079705A1 An impeller for an axial flow fan and a method of mounting a blade on a hub for such fan
10/25/2001WO2001078920A1 Casting device, in particular for producing turbine blades
10/25/2001WO2001021847A3 Superalloys with improved weldability for high temperature applications
10/25/2001US20010033793 Turbine engine damper
10/25/2001US20010032389 Method and device for demounting a turbine blade
10/25/2001DE10019546A1 Steam turbine has imaginary extension of outer edge of cover plate facing bearer which intersects rounded section between foot point and end point
10/24/2001EP1147849A1 Method for repositioning or repairing holes
10/24/2001EP1147291A2 Compressor endwall bleed system
10/24/2001EP0906514B1 Rotor for a turbomachine with blades insertable into grooves and blades for a rotor
10/23/2001US6307175 Method of producing a noncircular cooling bore
10/23/2001US6305904 Coolable component
10/23/2001US6305903 Cooled vane for gas turbine
10/23/2001US6305157 Gas turbine engine
10/23/2001US6305155 System for compensating for a pressure loss in the cooling-air ducting in a gas turbine plant
10/23/2001US6305078 Method of making a turbine blade
10/23/2001US6305077 Repair of coated turbine components
10/18/2001US20010029668 Process for the manufacture of a blade/vane of a turbomachine
10/18/2001DE10017429A1 Verbundkeramiksubstrat mit gradierter thermochemischer Schutzschicht Composite ceramic substrate with graded thermochemical protective layer
10/17/2001EP1146203A2 Impingement cooling of an undercut region of a turbine nozzle segment
10/17/2001EP1146202A2 Side wall cooling of a turbine nozzle segment
10/17/2001EP1146201A2 A method of controlling the side wall thickness of a turbine nozzle segment for improved cooling
10/17/2001EP1146133A1 Manufacturing process of nickel-based alloy having improved hot sulfidation-corrosion resistance
10/17/2001EP1145784A1 Casting apparatus, especially for fabrication of turbine blades
10/17/2001EP1144727A1 Antiabrasion coating
10/17/2001EP1144163A2 Shim removing tool and method
10/17/2001EP1144141A1 Multipiece core assembly
10/17/2001EP0785837B1 Interactive laser welding at elevated temperatures of superalloy articles
10/16/2001US6303075 Allowing a nb--ti--al type alloy material to incorporate mg, and optionally providing a dense mgo surface coating
10/16/2001US6302651 Blade attachment configuration
10/16/2001US6302649 Superalloy weld composition and repaired turbine engine component
10/16/2001US6302625 Method and apparatus for refurbishing a gas turbine airfoil
10/16/2001CA2242650C Gas turbine moving blade steam cooling system
10/11/2001US20010028848 Turbine rotor disk fitted with blades having christmastree-shaped roots, and a method of mounting a blade on a disk
10/11/2001US20010027963 Method of machining the turbine rotor shaft of a supercharger
10/10/2001EP1143110A2 Side wall cooling for nozzle segments of a gas turbine
10/10/2001EP1143106A2 Method and detail for repairing a stator vane
10/10/2001EP1143030A1 Tip material for a turbine blade and method of manufacturing or repairing a tip of a turbine blade
10/10/2001EP1142852A2 Composite ceramic material having graded thermochemical protective coating
10/10/2001EP1142850A1 Thermal/environmental barrier coating for silicon-containing materials
10/10/2001EP1141543A1 Reduction in the noise produced by a rotor blade of a wind turbine
10/10/2001EP1141442A1 METHOD FOR PRODUCING A METAL ALLOY POWDER SUCH AS MCrALY AND COATINGS OBTAINED WITH SAME
10/10/2001EP1141441A1 METHOD FOR FORMING A METAL ALLOY COATING SUCH AS MCrAlY
10/10/2001EP1141437A1 Heat-insulating glass-metal/ceramic layers
10/10/2001EP1140417A1 Blade and rotor for a gas turbine and method for linking blade parts
10/09/2001US6299971 Ceramic coatings containing layered porosity
10/09/2001US6299935 Coating surface of substrate with a foam suspension containing a powder suspended in a foam to form a coating on surface, wherein coating has an activator; subjecting the substrate to diffusion treatment
10/09/2001US6299412 Bowed compressor airfoil
10/09/2001US6299411 Fastening of moving blades of a fluid-flow machine
10/09/2001US6299410 Method and apparatus for damping vibration in turbomachine components
10/09/2001US6298657 Combined cycle power plant generation plant with steam cooling
10/09/2001CA2262930C Seal structure between gas turbine discs
10/09/2001CA2245049C A power generation system
10/04/2001US20010026877 Used in gas turbines blades, jet engines, boilers; durability
10/04/2001US20010025476 Cooling supply system for stage 3 bucket of a gas turbine
10/04/2001US20010025418 Tip material for a turbine blade and method of manfacturing or repairing a tip of a turbine blade
10/04/2001US20010025417 Method for repairing a gas turbine component
10/04/2001EP1138879A1 Turbine blade rotor disc assembly with fir-tree turbine blade root and assembly method therefore