Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2001
05/23/2001EP1101899A1 Method and apparatus for cooling an airfoil
05/23/2001EP1101898A2 Gas turbine blade
05/23/2001EP1101897A2 Methods for disassembling, replacing and assembling parts of a steam cooling system for a gas turbine
05/23/2001EP1101833A1 Repair of coated turbine components
05/23/2001EP1101563A2 Modification and repair of film cooling holes in gas turbine engine components
05/23/2001EP1101552A2 Clean melt nucleated cast metal article
05/23/2001DE10009655C1 Air cooling system for the paddles of a high pressure gas turbine has flow chambers at each paddle for the leading and trailing edges and the center profile with a heat exchanger to cool the air flow to the paddle edges
05/23/2001CN1295900A Turbine inlet guiding section and repairing method thereof
05/22/2001US6235370 High temperature erosion resistant, abradable thermal barrier composite coating
05/22/2001US6234912 High-stiffness composite shaft
05/22/2001US6234756 Segmented ring blade retainer
05/22/2001US6234755 Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture
05/22/2001US6234754 Coolable airfoil structure
05/22/2001US6234753 Turbine airfoil with internal cooling
05/22/2001US6234752 Method and tool for electrochemical machining
05/22/2001US6234746 Apparatus and methods for cooling rotary components in a turbine
05/22/2001US6233823 Method of making plastically formed hybrid airfoil
05/17/2001WO2001034946A1 Device for fixing a turbine ferrule
05/16/2001EP1099826A1 Positioning device for a turbine liner
05/16/2001EP1099825A1 Turbine blade and production method therefor
05/16/2001EP1099508A2 Turbine nozzle segment and method of repairing same
05/16/2001EP0839286B1 Fan blade with curved planform and high-lift airfoil having bulbous leading edge
05/16/2001CN1295650A Runner for a turbo-machine, especially for water turbine
05/16/2001CN1295184A Gas turbine, gas turbomachine and coolant collecting method for blades of the same
05/15/2001US6231998 Thermal barrier coating
05/15/2001US6231991 Ceramic on superalloy turbine
05/15/2001US6231307 Impingement cooled airfoil tip
05/15/2001US6231303 Gas turbine having a turbine stage with cooling-air distribution
05/15/2001US6231287 Rotor windage nut
05/15/2001US6230483 Steam cooled type gas turbine
05/10/2001WO2001005579A3 One-step noble metal-aluminide coatings
05/10/2001US20010000831 Shim removing method
05/09/2001EP1098092A2 Stator blade
05/09/2001EP1098069A2 A particle vibration damper
05/09/2001EP1098068A2 Striated cooling hole
05/09/2001EP1098067A2 Cooling structure for gas turbine rotor blades
05/09/2001CN1294246A Fixed blades of steam turbine
05/08/2001US6227804 Gas turbine blade
05/08/2001US6227801 Turbine engine having improved high pressure turbine cooling
05/08/2001US6227799 Turbine shaft of a steam turbine having internal cooling, and also a method of cooling a turbine shaft
05/08/2001US6227798 Turbine nozzle segment band cooling
05/08/2001US6226978 Heat, oxidation, and corrosion resistant under- and overcoating alloy of chromium, yttrium, aluminum, nickel, and base metal
05/03/2001WO2001031181A1 Gas turbine cooling system
05/03/2001WO2001031171A1 Cast airfoil structure with openings which do not require plugging
05/03/2001WO2001031170A1 Heat transfer promotion structure for internally convectively cooled airfoils
05/02/2001EP1096108A2 Stationary flowpath components for gas turbine engines
05/02/2001EP1096107A2 Locking devices
05/02/2001EP1095213A1 Integrated fan/low pressure compressor rotor for gas turbine engine
05/02/2001EP1095208A1 Blade retention apparatus for gas turbine rotor
05/02/2001EP1095207A2 High temperature airfoil
05/02/2001EP1095172A1 Method of stripping a coating from a rotary seal of an aircraft engine
05/02/2001CN1293736A Turbine wheel and pelton turbine equipped with same
05/01/2001US6224361 Tool for disposing laser blocking material in an airfoil
05/01/2001US6224341 Damping systems for vibrating members
05/01/2001US6224339 High temperature airfoil
05/01/2001US6224337 Thermal barrier coated squealer tip cavity
05/01/2001US6224336 Triple tip-rib airfoil
05/01/2001US6224334 Steam turbine, rotor shaft thereof, and heat resisting steel
05/01/2001US6224328 Turbomachine with cooled rotor shaft
05/01/2001US6224327 Steam-cooling type gas turbine
05/01/2001US6224321 Impeller containment system
05/01/2001US6223524 Shrouds for gas turbine engines and methods for making the same
04/2001
04/26/2001DE19950417A1 Component for gas turbine, with base body and protective covering made of ceramic material
04/25/2001EP1094200A1 Gas turbine cooled moving blade
04/25/2001EP1094199A1 Rotor for a gas turbine
04/25/2001EP1093879A2 Tip cap hole brazimg and oxidation resistant alloy therefor
04/25/2001EP1093872A1 Controlling grain spacing in directional solidified castings
04/24/2001US6221512 Metallic article having a thermal barrier coating and a method of application thereof
04/24/2001US6220817 AFT flowing multi-tier airfoil cooling circuit
04/24/2001US6220031 Exhaust gas turbocharger for an internal-combustion engine and method of operating same
04/24/2001US6220012 Booster recirculation passageway and methods for recirculating air
04/24/2001US6219916 Method for linear friction welding and product made by such method
04/24/2001CA2230341C Cooling steam system for steam cooled gas turbine
04/24/2001CA2045415C Turbomachine blade fastening
04/22/2001CA2287577A1 Gas turbine cooled moving blade
04/19/2001WO2001027443A1 Turbine rotor vane
04/19/2001DE19950109A1 Rotor für eine Gasturbine A rotor for a gas turbine
04/18/2001EP1092081A1 Rotor for a turbomachine
04/17/2001US6217286 Unidirectionally solidified cast article and method of making
04/17/2001US6217283 Composite fan platform
04/17/2001US6217280 Turbine inter-disk cavity cooling air compressor
04/12/2001WO2000071764A3 Cobalt-base composition and method for diffusion braze repair of superalloy articles
04/11/2001EP1091092A2 Method and apparatus for cooling a wall within a gas turbine engine
04/11/2001EP1091091A2 Method and apparatus for cooling a wall within a gas turbine engine
04/11/2001EP1091090A2 A method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture
04/11/2001EP1091089A2 Cooling air supply through bolted flange assembly
04/11/2001EP1091013A1 Method for forming a coating by use of an activated foam technique
04/11/2001EP1090711A1 Superalloy weld composition and repaired turbine engine component
04/11/2001EP1090710A1 Superalloy weld composition and repaired turbine engine component
04/11/2001CN1291260A Method for producing a wear-endangered component of a turbo-machine
04/10/2001US6215097 On the fly laser shock peening
04/10/2001US6214475 Thermal insulating layer for a metallic component and its process of manufacture
04/10/2001US6214248 Method of forming hollow channels within a component
04/10/2001US6213720 High strength composite reinforced turbomachinery disk
04/10/2001US6213719 Bar wedge preload apparatus for a propeller blade
04/10/2001US6213714 Cooled airfoil
04/10/2001US6213711 Steam turbine and blade or vane for a steam turbine
04/05/2001DE10040431A1 Steam turbine bucket for power generating plant, has fin with large thickness in one side and small thickness in other side being formed in periphery of snubber cover
04/04/2001EP1088976A2 An arrangement for sealing a steam-cooled gas turbine
04/04/2001EP1088964A2 Slotted impingement cooling of airfoil leading edge