Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2010
05/18/2010US7717679 Structure of balancing fan
05/18/2010US7717676 High aspect ratio blade main core modifications for peripheral serpentine microcircuits
05/18/2010US7717675 Turbine airfoil with a near wall mini serpentine cooling circuit
05/18/2010US7717671 Passive air seal clearance control
05/18/2010CA2485179C Split flow turbine nozzle
05/18/2010CA2462318C Method of applying environmental and bond coatings to turbine flowpath parts
05/18/2010CA2454922C Process of removing a ceramic coating deposit in a surface hole of a component
05/14/2010WO2010053775A1 Multi-part modular airfoil section and method of attachment between parts
05/14/2010WO2010053023A1 Method for manufacturing a steam turbine rotor, and steam turbine rotor
05/14/2010WO2010052784A1 Turbine blade
05/14/2010WO2010052379A1 Annular flange for fastening a rotor or a stator element in a turbine engine
05/14/2010WO2010052053A1 Gas turbine with securing plate between blade base and disk
05/14/2010WO2010052052A1 Rotor for a turbomachine
05/14/2010WO2010052051A1 Process for removing a coating from surfaces of components using only hydrochloric acid
05/14/2010WO2010051803A1 Anti-erosion layer for aerodynamic components and structures and method for the production thereof
05/14/2010WO2010051799A2 Repair method
05/14/2010CA2743226A1 Anti-erosion layer for aerodynamic components and structures and method for the production thereof
05/14/2010CA2742045A1 Annular flange for fastening a rotor or a stator element in a turbine engine
05/14/2010CA2737390A1 Multi-part modular airfoil section and method of attachment between parts
05/13/2010US20100119718 Dense protective coatings, methods for their preparation and coated articles
05/13/2010US20100119377 Cooling arrangement
05/13/2010US20100119375 Pre-Coating Burnishing of Erosion Coated Parts
05/13/2010US20100119373 Wind Turbine Rotor Blade
05/13/2010US20100119371 Shiplap arrangement
05/13/2010US20100115967 Eccentric chamfer at inlet of branches in a flow channel
05/12/2010EP2184444A2 Blade attachment apparatus for a turbine
05/12/2010EP2184443A1 Gas turbine with locking plate between blade foot and disk
05/12/2010EP2184442A1 Airfoil fillet
05/12/2010EP2184441A2 Shaft of a gas turbine
05/12/2010EP2184440A2 Shaft of a gas turbine
05/12/2010EP2184439A2 Method of manufacturing a shaft of a power unit
05/12/2010EP2184379A1 Method of removing the surfaces of components using hydrochloric acid
05/12/2010EP2184128A2 Methods for repairing gas turbine engine components
05/12/2010EP2183467A1 Rotor arrangement of a turbine
05/12/2010EP2183466A2 Seal coating between rotor blade and rotor disk slot in gas turbine engine
05/12/2010EP1896216B1 Component and method for joining metal elements
05/12/2010DE10334827B4 Schaufeldämpfer für einen Bläsernabenhohlraum unter der Schaufel Blade damper for a fan hub cavity under the blade
05/12/2010DE102009044408A1 System und Verfahren zum Verringern von Schaufelspitzenverlusten System and method for reducing blade tip losses
05/12/2010DE102008056741A1 Verschleissschutzschicht für Tial Wear protection for Tial
05/12/2010CN201460991U Disc-closed type turbine of turbocharger
05/12/2010CN201460990U Moving blade of steam turbine
05/12/2010CN201460988U turbine generator
05/12/2010CN1851246B Internal-combustion engine
05/11/2010US7713029 Turbine blade with spar and shell construction
05/11/2010US7713027 Turbine blade with split impingement rib
05/11/2010US7713026 Turbine bladed with tip cooling
05/11/2010US7712311 Turbocharger assembly with catalyst coating
05/11/2010CA2593267C Turbine blade for turbo-engines and method for manufacturing same
05/11/2010CA2464414C High pressure turbine blade cooling scoop
05/11/2010CA2460662C Methods and apparatus for assembling gas turbine engines
05/06/2010WO2010051453A2 Turbine blade including a seal pocket
05/06/2010WO2010050261A1 Turbine moving blade having tip thinning
05/06/2010WO2010050248A1 Method for manufacturing turbine wheel
05/06/2010WO2010049271A1 Cooled blade for a gas turbine, method for producing such a blade, and gas turbine having such a blade
05/06/2010WO2010049196A1 Gas turbine having sealing plates on the turbine disc
05/06/2010WO2010049195A1 Gas turbine having cooling insert
05/06/2010WO2010028641A3 Replacement part for a gas turbine blade of a gas turbine, gas turbine blade and method for repairing a gas turbine blade
05/06/2010US20100111704 Turbine blade having squealer
05/06/2010US20100111701 Turbine rotor blade and fixation structure thereof
05/06/2010US20100111700 Turbine blade including a seal pocket
05/06/2010US20100111699 Spacers and turbines
05/06/2010US20100111673 Turbine with interrupted purge flow
05/06/2010US20100111672 Hesting Power Turbine Device
05/06/2010US20100111671 Methods and apparatus involving shroud cooling
05/06/2010DE102009043866A1 Turbinenschaufel für eine Turbomaschine und Verfahren zur Reduktion von Bugwelleneffekten an einer Turbinenschaufel Turbine blade for a turbo machine and method for reducing Bugwelleneffekten on a turbine blade
05/06/2010DE102008056018A1 Triebwerkswelle für ein Gasturbinentriebwerk Engine shaft for a gas turbine engine
05/06/2010DE102008056017A1 Verfahren zur Herstellung einer Triebwerkswelle A process for producing an engine shaft
05/06/2010DE102008056002A1 Triebwerkswelle aus einem Faserverbundkunststoffrohr mit metallischen Antriebs-und Abtriebszapfen Engine shaft of a fiber composite plastic pipe with metallic drive and output pins
05/06/2010DE102008055706A1 Device for fastening wheel on shaft, has shaft and wheel arranged at shaft, where wheel is provided between fastening element and counter bearing
05/06/2010DE102008055676A1 Rotor disk for rotor of compressor or turbine, particularly for compressor or turbine of aero engine or stationary gas turbine, has hub and disk body, where disk body is fully or partially formed from multiple spoke-type elements
05/06/2010DE102006044706B4 Schichtstruktur, deren Anwendung und Verfahren zur Herstellung einer Schichtstruktur Layer structure, their application and method for preparing a layered structure
05/05/2010EP2182174A2 Steam turbine with pressure activated sealing device
05/05/2010EP2182173A2 Steam turbine with thermally activated sealing device
05/05/2010EP2182172A1 Compressing turbomachine with fluid injection
05/05/2010EP2182170A1 Gas turbine with seal plates on the turbine disk
05/05/2010EP2182169A1 Blade cooling structure of gas turbine
05/05/2010EP2182168A1 Fabricated hybrid turbine blade
05/05/2010EP2182092A2 A method of repairing an aluminide coating on an article
05/05/2010CN201448124U Turbine moving blade
05/05/2010CN201448123U Material-saving sampling analysis impeller
05/04/2010US7708528 Platform mate face contours for turbine airfoils
05/04/2010US7708525 Industrial gas turbine blade assembly
05/04/2010US7708519 Vortex spoiler for delivery of cooling airflow in a turbine engine
05/04/2010CA2422842C Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes
05/04/2010CA2398659C Cooling circuits for gas turbine blade
04/2010
04/29/2010WO2010046584A1 Turbine blade equipped with means of adjusting its cooling fluid flow rate
04/29/2010WO2010046553A1 Ventilation of a high-pressure turbine in a turbomachine
04/29/2010WO2010046299A2 Airfoil and blade for a turbine, and method for directly determining the progress of erosion of a turbine blade airfoil
04/29/2010WO2010046283A1 Blade for a gas turbine
04/29/2010US20100104461 Multi-Part Modular Airfoil Section and Method of Attachment Between Parts
04/29/2010US20100104446 Fabricated hybrid turbine blade
04/29/2010US20100104445 Fan Blade Modifications
04/29/2010US20100104440 Coating material and method of manufacturing same, coating method, and moving blade with shroud
04/29/2010US20100104436 Active curcilation control of aerodynamic structures
04/29/2010US20100104430 Component with a Protective Layer
04/29/2010US20100104419 Turbine airfoil with near wall inflow chambers
04/29/2010US20100104418 Gas turbine
04/29/2010DE10344843B4 Integrierte Rotations-Messerkanten-Injektionsanordnung Integrated rotary knife-edge injection assembly
04/29/2010DE102008052947A1 Verfahren zur Herstellung von Laufschaufeln und einer Radscheibe für eine Turbomaschine sowie Vorrichtung, aufweisend Laufschaufeln und eine Radscheibe für eine Turbomaschine A process for the production of rotor blades, and a wheel disc for a turbo machine and apparatus comprising blades and a wheel disc for a turbomachine
04/29/2010CA2740512A1 Turbine blade equipped with means of adjusting its cooling fluid flow rate