Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
09/2001
09/04/2001US6283713 Bladed ducting for turbomachinery
09/04/2001US6283712 Cooling air supply through bolted flange assembly
09/04/2001US6283708 Coolable vane or blade for a turbomachine
09/04/2001US6283707 Aerofoil blade damper
09/04/2001US6283356 Repair of a recess in an article surface
09/04/2001US6282786 Method of making injection formed hybrid airfoil
09/03/2001WO2001065086A1 Internal combustion rotary turbomotor
08/2001
08/30/2001WO2001063098A1 Moving turbine blade
08/30/2001WO2001063097A1 Rotor for a gas turbine
08/30/2001WO2001062419A1 Clean melt nucleated casting systems and methods with cooling of the casting
08/30/2001WO2001062414A1 Device and method for casting a workpiece and workpiece
08/30/2001WO2001045877A8 Multi-wall core and process
08/30/2001US20010018319 Process for treating the interior of a hollow component
08/30/2001US20010018024 Internal cooling circuit for gas turbine bucket
08/30/2001US20010018021 Turbine blade
08/30/2001US20010018020 Turbine guide blade
08/30/2001US20010018019 Pre-stressed/pre-compressed gas turbine nozzle
08/30/2001DE10008257A1 Verfahren zur Reparatur einer Gasturbinenkomponente A method of repairing a gas turbine component
08/29/2001EP1128024A2 Gas turbine moving blade
08/29/2001EP1128023A1 Turbine rotor blade
08/29/2001EP1128022A2 Rotor windage nut
08/29/2001EP1127959A1 Thermal barrier coating method and article
08/29/2001EP1127949A2 TiA1 based alloy, production process therefor, and rotor blade using same
08/29/2001EP1127651A1 Method and apparatus for increasing cladding or welding rates
08/29/2001EP1127648A2 Repairing method of gas turbine components
08/29/2001EP1127635A1 Apparatus and method for casting a workpiece and workpiece
08/28/2001US6280550 Fabrication of composite articles having an infiltrated matrix
08/28/2001US6280140 Method and apparatus for cooling an airfoil
08/28/2001US6279420 Balance weight for a rotary component in turbomachinery, methods of installation and installation tools
08/23/2001WO2001061152A1 Aerofoil for an axial flow turbomachine
08/23/2001US20010016163 Gas turbine moving blade
08/23/2001US20010016162 Cooled blade for a gas turbine
08/22/2001EP1126747A2 Heating device for metallic pieces
08/22/2001EP1126136A2 Turbine blade with air cooled tip shroud
08/22/2001EP1126135A2 Ceramic turbine airfoils with cooled trailing edge blocks
08/22/2001EP1126134A1 Air and steam-cooled gas turbine vane
08/22/2001EP1126133A2 Convex compressor casing
08/22/2001EP1126132A2 Fluted compressor flowpath
08/22/2001CN1309230A Three-D axial-flow turbine stage
08/21/2001US6276899 Impeller manufacturing process
08/21/2001US6276897 Cooling in gas turbines
08/21/2001US6276896 Apparatus and method for cooling Axi-Centrifugal impeller
08/21/2001US6276863 Friction- and form-grip connection of rotating components
08/21/2001US6276597 Tip cap hole brazing and oxidation resistant alloy therefor
08/21/2001US6276432 Directional solidification method and apparatus
08/21/2001US6276124 Bi-metallic tie-bolt for microturbine power generating system
08/21/2001CA2231668C Blade cooling air supplying system of gas turbine
08/21/2001CA2016007C Gamma titanium aluminum alloys modified by chromium and tantalum and method of preparation
08/16/2001WO2001059263A2 Turbine blade arrangement
08/16/2001WO2001059262A1 Improved cooling of turbine blades
08/16/2001WO2001059261A1 Three-dimensional axial-flow turbine stage
08/16/2001WO2001059168A1 Iron base high temperature alloy
08/16/2001US20010014403 Gas turbine engines
08/16/2001US20010014285 Rotor blade an axial-flow engine
08/16/2001US20010014284 Intake and exhaust damper with movable motor fan assembly
08/16/2001US20010014283 Debris trap in a turbine cooling system
08/16/2001US20010014282 Drilled cooling air openings in gas turbine components
08/16/2001EP1124038A1 Turbine blading
08/16/2001EP1123987A1 Repairable diffusion aluminide coatings
08/16/2001EP1123984A2 High and low pressure integrated type turbine rotor and process for producing the same
08/16/2001EP1123457A2 Gas turbine engine
08/16/2001EP1123455A1 Product with a heat insulating layer and method for the production of a heat insulating layer
08/16/2001DE10005874A1 Schweissverfahren zur Rissreparatur Welding method for crack repair
08/15/2001CN1308706A Turbine nozzle vane
08/15/2001CN1069737C Combined-cycle power generation plant
08/14/2001US6274215 Aerodynamic article with partial outer portion and method for making
08/14/2001US6274193 Repair of a discrete selective surface of an article
08/14/2001US6273683 Turbine blade platform seal
08/14/2001US6273682 Turbine blade with preferentially-cooled trailing edge pressure wall
08/14/2001US6273678 Modified diffusion aluminide coating for internal surfaces of gas turbine components
08/14/2001US6273676 Method and assembly for masking a flow directing assembly
08/14/2001US6273673 Ball turbine
08/14/2001US6273671 Blade clearance control for turbomachinery
08/14/2001US6272844 Gas turbine engine having a bladed disk
08/14/2001CA2232128C Cooled platform for a gas turbine moving blade
08/14/2001CA2231690C Cooled stationary blade for a gas turbine
08/14/2001CA2231495C Gas turbine rotating blade
08/14/2001CA2231035C Gas turbine blade
08/14/2001CA2014908C Gamma titanium aluminum alloys modified by carbon, chromium and niobium
08/09/2001WO2001057380A1 Variable cycle gas turbine engine
08/09/2001WO2001057365A1 Means for securing a bucket to a turbine wheel and methods of installation
08/09/2001WO2001057283A1 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting
08/09/2001US20010012568 Thermal barrier coating system utilizing localized bond coat and article having the same
08/09/2001US20010012484 Blade for gas turbines with choke cross section at the trailing edge
08/09/2001US20010011452 Cooling air ducting system in the high pressure turbine section of a gas turbine engine
08/08/2001EP1122443A2 Piggyback rotor blisk
08/08/2001EP1122407A2 Controllable guide vane apparatus for a gas turbine engine
08/08/2001EP1122406A2 Blade attachment configuration
08/08/2001EP1122405A2 Gas turbine bucket cooling circuit
08/08/2001EP1122329A1 A method of providing a protective coating on a metal substrate, and related articles
08/08/2001EP1122323A1 Method for recovering platinum from platinum-containing coatings on gas turbine engine components
08/08/2001EP0856095B1 Variable area compensation valve
08/07/2001US6270852 Providing superalloy substrate, superalloy material being capable of forming adherent alumina layer; applying bond coat; forming alumina layer; applying ceramic layer on alumina layer
08/07/2001US6270318 Article having corrosion resistant coating
08/07/2001US6270317 Turbine nozzle with sloped film cooling
08/07/2001US6270315 Highly loaded turbine blading
08/07/2001US6269540 Process for manufacturing or repairing turbine engine or compressor components
08/02/2001WO2001055627A1 Valve, in particular pressure reducing valve
08/02/2001WO2001055559A1 Porous turbine blades and turbine equipped with blades of this type
08/02/2001WO2001054857A1 Thermal processing apparatus and method