Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
07/2010
07/01/2010US20100166551 Hybrid turbomachinery component for a gas turbine engine
07/01/2010US20100166548 Steam turbine blade and method for manufacturing the same
07/01/2010US20100162703 Process for reducing carbon dioxide emission in a power plant
07/01/2010DE102009059319A1 Turbinenschaufelfußkonfigurationen Turbinenschaufelfußkonfigurationen
07/01/2010DE102009059225A1 Turbinenrotorschaufelspitzen, die eine Querströmung behindern Turbine rotor blade tips that hinder cross-flow
07/01/2010CA2747983A1 Device for attaching hammer clamp blades, associated compressor hub, compressor, and turbine engine
07/01/2010CA2746415A1 Curved platform turbine blade
06/2010
06/30/2010EP2202385A1 Treatment of the compressor housing of a turbomachine consisting of a circular groove describing a ripple intended to control vane head vortices
06/30/2010EP2202212A2 Components Comprising CMAS mitigation compositions
06/30/2010EP2201220A1 A method of producing a rotor component or a stator component
06/30/2010EP2126285B1 Turbine seal plate locking system
06/30/2010CN101765702A Rotor of rotary machine and method for manufacturing same
06/30/2010CN101761368A Low-grade heat flow prime motor, power generating system and method thereof
06/30/2010CN101761364A Method for generating electricity by using low-pressure saturated steam
06/30/2010CN101761361A Turbomachine, especially steam turbine
06/30/2010CA2689179A1 Stator assembly for a gas turbine engine
06/29/2010US7744350 Multiblade fan
06/29/2010US7744348 Method of producing a hot gas component of a turbomachine including an embedded channel
06/29/2010US7744347 Peripheral microcircuit serpentine cooling for turbine airfoils
06/29/2010CA2688882A1 Assembly for rectifier stage of a turbomachine, comprising an outer collar and at least one stationary vane
06/24/2010WO2010071770A1 Environmental barrier coatings providing cmas mitigation capability for ceramic substrate components
06/24/2010WO2010071768A1 Environmental barrier coatings providing cmas mitigation capability for ceramic substrate components
06/24/2010WO2010071765A1 Environmental barrier coatings providing cmas mitigation capability for ceramic substrate components
06/24/2010WO2010071704A1 Durable thermal barrier coating compositions, coated articles, and coating methods
06/24/2010WO2010071703A1 Durable thermal barrier coating compositions, coated articles, and coating methods
06/24/2010WO2010071496A1 Gas turbine composite workpiece to be used in gas turbine engine
06/24/2010WO2010069912A1 Thermal barrier coating system, components coated therewith and method for applying a thermal barrier coating system to components
06/24/2010WO2010069696A1 Mould for soldering, arrangement of moulds, a method and a component
06/24/2010WO2010046704A3 Method and system for altering engine air intake geometry
06/24/2010US20100158701 Turbine blades
06/24/2010US20100158700 Turbine blade assemblies and methods of manufacturing the same
06/24/2010US20100158696 Curved platform turbine blade
06/24/2010US20100158695 Superalloy Compositions, Articles, and Methods of Manufacture
06/24/2010US20100158694 Blade module, a modular rotor blade and a method for assembling a modular rotor blade
06/24/2010US20100158693 Test blade
06/24/2010US20100158691 Component and Method for Joining Metal Elements
06/24/2010US20100158690 One-Piece Bladed Drum of an Axial Turbomachine Compressor
06/24/2010US20100158686 Turbine blade assembly including a damper
06/24/2010US20100158681 Ni-based alloy for a forged part of a steam turbine with excellent high temperature strength, forgeability and weldability, rotor blade of a steam turbine, stator blade of a steam turbine, screw member for a steam turbine, and pipe for a steam turbine
06/24/2010US20100158680 Cmas mitigation compositions, environmental barrier coatings comprising the same, and ceramic components comprising the same
06/24/2010US20100158678 Airfoil shape for a turbine nozzle
06/24/2010US20100155524 Monomolecular carbon-based film for forming lubricious surface on aircraft parts
06/24/2010US20100155224 Multi-Component Deposition
06/24/2010US20100154422 Cmas mitigation compositions, environmental barrier coatings comprising the same, and ceramic components comprising the same
06/24/2010CA2747416A1 Environmental barrier coatings providing cmas mitigation capability for ceramic substrate components
06/24/2010CA2747335A1 Durable thermal barrier coating compositions, coated articles, and coating methods
06/24/2010CA2747329A1 Durable thermal barrier coating compositions, coated articles, and coating methods
06/24/2010CA2746450A1 Environmental barrier coatings providing cmas mitigation capability for ceramic substrate components
06/24/2010CA2746447A1 Environmental barrier coatings providing cmas mitigation capability for ceramic substrate components
06/24/2010CA2688607A1 Blade retention at a compressor rectifier stage for impact resistance
06/24/2010CA2685987A1 One-piece bladed drum of an axial turbomachine compressor
06/23/2010EP2199543A2 Gas turbine engine airfoil
06/23/2010EP2199424A1 Static chemical vapor deposition of gamma-Ni + gamma'-Ni3Al coatings
06/23/2010EP2198154A2 Wind turbine blade with submerged boundary layer control means
06/23/2010EP2198153A1 Wind turbine blade with submerged boundary layer control means comprisin crossing sub-channels
06/23/2010EP2198128A1 Method for producing a blisk or a bling, component produced therewith and turbine blade
06/23/2010EP2198064A1 Hot gas-guided component of a turbomachine
06/23/2010CN101749181A Turbine blade and method of fabricating the same
06/23/2010CN101749059A Vibration reduction in an exhaust gas turbo-supercharger
06/23/2010CN101749053A Hollow passages
06/23/2010CN101749052A Last-stage moving blade of air-cooling feed pump turbine
06/23/2010CN101749051A Method for designing blank material for use in rolling of blade without tenon at two ends
06/23/2010CN101749050A Forged blank material for use in rolling of single-tenon blade
06/23/2010CN101749049A Method for designing forged blank material for use in rolling of single-tenon blade
06/23/2010CN101310100B Method and apparatus for balancing an electrically assisted turbocharger rotor
06/23/2010CN101082286B 涡轮叶片 Turbine blades
06/23/2010CA2687800A1 Turbine cooling air from a centrifugal compressor
06/22/2010US7740451 Turbomachine blade
06/22/2010US7740449 Process for adjusting a flow capacity of an airfoil
06/22/2010US7740445 Turbine blade with near wall cooling
06/22/2010US7739866 Turbofan case and method of making
06/22/2010CA2688374A1 Rotor mounting system for gas turbine engine
06/17/2010WO2010068391A2 Banked platform turbine blade
06/17/2010WO2010067024A2 Turbine wheel provided with an axial retention device that locks blades in relation to a disk
06/17/2010WO2010066791A1 Fan for a turbine engine including a balancing system with blind holes for housing bodies, and related turbine engine
06/17/2010WO2010066548A1 Turbine blade with coating
06/17/2010WO2010036430A3 Imparting deep compressive residual stresses into a gas turbine engine airfoil peripheral repair weldment
06/17/2010US20100150734 Turbine blade
06/17/2010US20100150733 Airfoil with wrapped leading edge cooling passage
06/17/2010US20100150730 Component having an abrasive layer and a method of applying an abrasive layer on a component
06/17/2010US20100150729 Gas turbine engine airfoil
06/17/2010US20100150727 Rotor blade for a gas turbine
06/17/2010US20100150726 Article and ultrasonic inspection method and system therefor
06/17/2010US20100150725 Wheel formed from a bladed ring and disk
06/17/2010US20100150724 Platform seal in a turbomachine rotor, method for improving the seal between a platform and a turbomachine blade
06/17/2010US20100150723 Rotor for a Compressor
06/17/2010US20100150721 Radial blade wheel
06/17/2010US20100150713 Rotating-Plate Radial Turbine in Gas-Turbine-Cycle Configurations
06/17/2010US20100150707 Airfoil
06/17/2010US20100150698 Engine Intake Air Compressor And Method
06/17/2010CA2746431A1 Turbine wheel provided with an axial retention device that locks blades in relation to a disk
06/17/2010CA2746249A1 Fan for a turbine engine including a balancing system with blind holes for housing bodies, and related turbine engine
06/17/2010CA2744816A1 Banked platform turbine blade
06/16/2010EP2196625A1 Turbine blade with a hole extending through a partition wall and corresponding casting core
06/16/2010EP2196624A1 Gas turbine rotor blade
06/16/2010EP2196623A1 Gas Turbine
06/16/2010EP2196559A1 Thermal barrier coating system, components coated therewith and method for applying a thermal barrier coating system to components
06/16/2010EP2196276A1 Form bodies for welding, assembly of form bodies, method and component
06/16/2010EP2104656B1 Composite material part with a silicon-containing ceramic matrix protected against corrosion
06/16/2010EP1540189B1 Restraining device for fan blade root