Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2002
04/02/2002US6364634 Turbocharger rotor with alignment couplings
04/02/2002US6364616 Submerged rib hybrid blade
04/02/2002US6364613 Hollow finger dovetail pin and method of bucket attachment using the same
04/02/2002US6364608 Partially coated airfoil and method for making
04/02/2002US6363712 Gas-driven microturbine
04/02/2002US6363612 Method of reducing burr formation during turbine bucket cover machining
04/02/2002CA2247491C Steam cooled gas turbine rotor
03/2002
03/28/2002WO2002025066A1 Steam-type gas turbine subassembly and method for enhancing turbine performance
03/28/2002WO2002025065A1 Seal system
03/28/2002WO2002024411A1 Transverse ultrasound peening of blades on a rotor
03/28/2002US20020037220 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby
03/28/2002US20020037219 Gas turbine engine rotor blades
03/28/2002US20020037217 Cooling circuit for steam and air-cooled turbine nozzle stage
03/28/2002US20020037216 Shaft structure and bearing structure for tail end of rotor of gas turbine
03/27/2002EP1191191A2 Turbine bearing
03/27/2002EP1191189A1 Gas turbine blades
03/27/2002EP1191188A2 Shaft structure for a steam cooled gas turbine
03/27/2002EP1191125A1 Method for making a thermal barrier coating
03/27/2002EP1191118A1 Manufacturing process of nickel-based alloy having improved high temperature sulfidation-corrosion resistance
03/26/2002US6361277 Methods and apparatus for directing airflow to a compressor bore
03/21/2002WO2002023014A1 A lead-in structure and a fixing flange for a turbo generator
03/21/2002WO2002022291A1 Device and method for producing a blade for a turbine and blade produced according to this method
03/21/2002WO2001098561A3 Graded platinum diffusion aluminide coating
03/21/2002DE10113609C1 Turbine rotor for wind turbine has intermediate plate between each rotor blade and outer ring of rotor hub
03/21/2002DE10029807C1 Exhaust gas turbocharger for IC engine has turbine wheel provided with hollow space between hub base and hub envelope
03/20/2002EP1188903A1 Machined turbomachine shroud
03/20/2002EP1188902A1 Impingement cooled wall
03/20/2002EP1188901A2 Bypass holes for rotor cooling
03/20/2002EP1188900A2 Balancing method for a blisk
03/20/2002EP1188500A1 Apparatus and method for producing a turbine blade and turbine blade
03/20/2002EP1188497A2 A method of manufacturing an article by diffusion bonding
03/20/2002EP1042542A4 Method for electrophoretic deposition of brazing material
03/20/2002CN1341192A Internal combustion rotary turbomotor
03/20/2002CN1340576A Anti-oxidation coat, its correlated product and method
03/20/2002CN1081289C Stationary blade for gas turbine
03/19/2002US6358013 Turbine blade and manufacture thereof
03/19/2002US6358012 High efficiency turbomachinery blade
03/19/2002US6358010 Enhanced fan and fan drive assembly
03/19/2002US6358004 Steam turbine power-generation plant and steam turbine
03/19/2002US6358003 Rotor blade an axial-flow engine
03/19/2002US6357999 Gas turbine engine internal air system
03/19/2002US6357217 Endothermic cooling of guide vanes and/or moving blades in a gas turbine
03/19/2002CA2041633C Turbomachine blade fastening
03/18/2002CA2357176A1 Turbine engine with improved outward flow
03/14/2002WO2002020949A1 Turbo-machine and turbine blade
03/14/2002WO2002020948A1 Moving blade for a turbo-machine and turbo-machine
03/14/2002US20020031429 Gas turbine engine system
03/14/2002US20020031427 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor
03/14/2002US20020029653 Balance weight for a rotary component in turbomachinery, methods of installation and installation tools
03/14/2002DE10140419A1 Flüssigkristallines Medium mit niedriger Doppelbrechung Liquid-crystalline medium having low birefringence
03/14/2002DE10043906A1 Vordralldüsenträger Vordralldüsenträger
03/13/2002EP1186749A1 Turbomachine and turbine blade
03/13/2002EP1186748A1 Rotor blade for a turbomachine and turbomachine
03/13/2002EP1186747A2 An automized blade shape designing method
03/13/2002EP1186746A2 Swirl nozzle
03/13/2002EP1186680A2 Process for applying and aluminum-containing coating using an inorganic slurry mix
03/13/2002EP1185764A1 Device for controlling air flow in a turbine blade
03/13/2002EP1135540B1 Method and device for cleaning a product
03/13/2002CN1340129A Shim removing tool and method
03/12/2002US6355356 Coating system for providing environmental protection to a metal substrate, and related processes
03/12/2002US6355116 Method for renewing diffusion coatings on superalloy substrates
03/12/2002US6355086 Method and apparatus for making components by direct laser processing
03/12/2002US6354803 Blade damper and method for making same
03/12/2002US6354799 Superalloy weld composition and repaired turbine engine component
03/12/2002US6354798 Blade for a fluid-flow machine, and steam turbine
03/12/2002US6354780 Eccentric balanced blisk
03/07/2002WO2002018674A2 Thermal barrier coating system for turbine components
03/07/2002US20020028142 Centrifugal impeller assembly
03/07/2002US20020028141 Apparatus and methods for balancing turbine rotors
03/07/2002US20020028140 Cooling circuit for and method of cooling a gas turbine bucket
03/07/2002US20020028139 Stator vane assembly for a turbine and method for forming the assembly
03/07/2002US20020028136 Pre-swirl nozzle carrier
03/07/2002US20020028135 Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment
03/07/2002US20020028134 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment
03/07/2002US20020028133 Vane assembly
03/07/2002DE10039642A1 Turbine blade air wing for axial flow turbine, has bent surface portion provided to outside arc at wing section corresponding to flat surface portion provided to air wing inside arc
03/06/2002EP1184656A1 Method for structural development of monocrystalline superalloys
03/06/2002EP1184479A1 Method of forming a reactive-element containing aluminide on a metallic substrate
03/06/2002EP1184475A2 Oxidation-resistant coatings, and related articles and processes
03/06/2002EP1183442A1 Cast on-board injection nozzle with adjustable flow area
03/05/2002US6352790 Substrate containing silicon and a barrier layer which functions as a protective/thermal barrier coating
03/05/2002US6352788 Impact resistance
03/05/2002US6352406 Method for assessing quality of a coating process and assembly therefor
03/05/2002US6352385 Mechanical coupling for cooperating rotatable members
03/05/2002US6351938 Turbine or system with internal evaporative blade cooling
03/05/2002US6351937 Gas turbine plant
03/05/2002CA2264282C Gas turbine air separator
02/2002
02/28/2002WO2002016775A2 A turbine
02/28/2002US20020025250 Connector tube for a turbine rotor cooling circuit
02/28/2002US20020025248 Method for enhancing heat transfer inside a turbulated cooling passage
02/28/2002US20020023846 Chemical macrographic etching and a subsequent step of electrochemical etching by means of a bath containing phosphoric acid and at least one weak acid for revealing structure for a component made of a single-crystal superalloy
02/28/2002US20020023696 Formation of an aluminide coating, incorporating a reactive element, on a metal substrate
02/28/2002DE10037053A1 Verfahren und Vorrichtung zum Plasmaimpulsverfestigen eines metallischen Bauteils Method and apparatus for pulsed plasma solidifying a metallic component
02/27/2002EP1182339A2 Clocked turbine airfoil cooling
02/27/2002EP1182329A2 Blade attachment using hollow pins
02/27/2002EP1182328A2 Method for reducing circumferential rim stress in rotors
02/27/2002EP1181437A1 Component and method for producing a protective coating on a component
02/27/2002CN2479214Y Final blade of large steam turbine
02/26/2002USRE37562 Turbine system having more failure resistant rotors and repair welding of low alloy ferrous turbine components by controlled weld build-up
02/26/2002US6350325 Turbine shaft and method for producing a turbine shaft