Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
03/2013
03/27/2013EP2573325A1 Impingement cooling of turbine blades or vanes
03/27/2013EP2573324A2 Hollow fan blade with channel configuration to reduce stress
03/27/2013EP2573323A2 Fan blade
03/27/2013EP2573322A2 Fan blade
03/27/2013EP2573321A2 Fan blade
03/27/2013EP2573320A2 Components with cooling channels and methods of manufacture
03/27/2013EP2573319A2 Turbomachine configured to burn ash-bearing fuel oils and method of burning ash-bearing fuel oils in a turbomachine
03/27/2013EP2573318A1 A blade for a turbomachine comprising temperature and expansion sensors
03/27/2013EP2573317A1 Rotor for a steam turbine
03/27/2013EP2573201A2 Method for refurbishing ptal coating to turbine hardware removed from service
03/27/2013EP2572979A1 Rotor blade erosion protection system
03/27/2013CN202832667U 1075mm penultimate stage moving blade used for semi-rotation nuclear turbine
03/27/2013CN103003527A Radial turbine
03/27/2013CN103003472A Porous ceramic coating system
03/27/2013CN102996258A Non-continuous ring seal
03/27/2013CN102996185A Turbine rotor blade assembly and method of assembling same
03/27/2013CN102996184A Airfoil shape for turbine bucket and turbine incorporating same
03/27/2013CN102996183A Compressive stress system for a gas turbine engine
03/27/2013CN101832154B Method for cooling air film of turbine blade of aircraft engine
03/27/2013CN101709656B Coupling method for improving blade cooling efficiency and combustion efficiency of interstage/afterburner/channel combustion chambers
03/27/2013CN101078354B Porous metal vane coupling design method
03/26/2013US8403645 Turbofan flow path trenches
03/26/2013US8403632 Gas turbine engine component cooling scheme
03/26/2013US8403631 Gas turbine engine component cooling scheme
03/26/2013US8403629 Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
03/26/2013US8403626 Arrangement for a gas turbine engine
03/26/2013CA2634738C Second stage turbine airfoil
03/26/2013CA2502788C High efficiency stator for the second phase of a gas turbine
03/23/2013CA2790089A1 Method for refurbishing ptal coating to turbine hardware removed from service
03/21/2013WO2013037999A1 Compressor blade and method for the production thereof
03/21/2013WO2013037945A1 Erosion resistant impeller vane made of metallic laminate
03/21/2013WO2013037662A1 Gas-turbine-component
03/21/2013WO2013037483A1 Securing segment for the vibration damping of turbine blades and rotor device
03/21/2013US20130071255 Gas Turbine Blade
03/21/2013US20130071254 Turbine blades and methods of forming modified turbine blades and turbine rotors
03/21/2013US20130071252 Rotor Blade Erosion Protection System
03/21/2013US20130071250 Process of welding a turbine blade, a process of welding a non-uniform article, and a welded turbine blade
03/21/2013US20130071249 Airfoil shape for turbine bucket and turbine incorporating same
03/21/2013US20130071248 Compressive stress system for a gas turbine engine
03/21/2013US20130071247 Impeller and method for producing same
03/21/2013US20130071245 Rotor with improved balancing features
03/21/2013US20130071236 Cooling and climate control system and method for a wind turbine
03/21/2013US20130068894 Wing for generating lift from an incident flow
03/21/2013US20130068888 Airfoil structure
03/21/2013DE102012016978A1 Schwingungsdämpfer für rotierende Teile Vibration damper for rotating parts
03/21/2013CA2876768A1 Rotor blade erosion protection system
03/21/2013CA2788117A1 Rotor blade erosion protection system
03/20/2013EP2570674A1 Erosion resistant impeller vane made of metallic laminate
03/20/2013EP2570611A2 Ceramic matrix composite airfoil for a gas turbine engine and corresponding method of forming
03/20/2013EP2570610A2 Ceramic matrix composite vane structure for a gas turbine engine and corresponding low pressure turbine
03/20/2013EP2570609A2 Ceramic matrix composite airfoil for a gas turbine engine and corresponding rotor disk assembly
03/20/2013EP2570608A2 Ceramic matrix composite rotor module for a gas turbine engine, corresponding turbine assembly and method of assembling
03/20/2013EP2570607A2 Gas turbine engine with ceramic matrix composite static structure and rotor module, and corresponding method of tip clearance control
03/20/2013EP2570606A2 Ceramic matrix composite turbine exhaust case for a gas turbine engine and corresponding gas turbine engine
03/20/2013EP2570605A2 Ceramic matrix composite rotor disk for a gas turbine engine and corresponding rotor module
03/20/2013EP2570604A2 Ceramic matrix composite airfoil for a gas turbine engine, corresponding vane structure and method of forming
03/20/2013EP2570603A2 Ceramic matrix composite platform assembly for an airfoil of a gas turbine engine and corresponding rotor disk assembly
03/20/2013EP2570602A2 Ceramic matrix composite vane structure for a gas turbine engine, corresponding low pressure turbine and assembling method
03/20/2013EP2570601A2 Ceramic matrix composite rotor disk for a gas turbine engine and corresponding rotor module
03/20/2013EP2570600A2 Turbine rotor blade assembly and method of assembling same
03/20/2013EP2570599A1 Compressive stress system and method for a gas turbine engine
03/20/2013EP2570598A2 Rotor disk assembly for a gas turbine engine
03/20/2013EP2570597A2 Method of manufacturing a composite filled metal airfoil and corresponding fan blade
03/20/2013EP2570596A2 Rotor blade and method for manufacturing blade
03/20/2013EP2570595A1 Methods for manufacturing components from articles formed by additive-manufacturing processes
03/20/2013EP2570594A2 Turbine bucket with metallic airfoil and ceramic tip cap, and corresponding gas turbine engine
03/20/2013EP2570593A2 Ceramic matrix composite airfoil segment for a gas turbine engine, corresponding structure and method of assembling
03/20/2013EP2570592A2 Method and apparatus for controlling temperature of gas turbine components
03/20/2013EP2570591A2 Method for repairing a ceramic fiber reinforced ceramic composite article and corresponding intermediate
03/20/2013EP2569609A2 Wireless temperature measurement system and method of using same
03/20/2013EP2569594A1 Surface analysis for detecting closed holes and method for reopening
03/20/2013EP2569514A1 Fastening assembly for blades of turbomachines having axial flow and method for producing such an assembly
03/20/2013EP2569513A1 Turbine nozzle segment and corresponding gas turbine engine
03/20/2013CN202810960U Jet-propelled reverse worm wheel steam turbine power generation device
03/20/2013CN202810955U Disk shaft connection structure
03/20/2013CN202810954U Medium and low pressure blades of 155 for turbine with subcritical grade of 300mw
03/20/2013CN102985582A Method for producing a rotor/stator seal of a gas turbine
03/20/2013CN102979583A Separate-type column rib cooling structure for turbine blade of gas turbine
03/20/2013CN102979582A 712.5 mm last-stage moving blade used for high power combined-cycle steam turbine
03/19/2013US8398374 Method and apparatus for a segmented turbine bucket assembly
03/19/2013US8398371 Turbine blade with multiple near wall serpentine flow cooling
03/19/2013US8398370 Turbine blade with multi-impingement cooling
03/14/2013WO2013034857A2 Method for manufacturing a sector of a turbine nozzle or compressor stator vane made of a composite material for a turbine engine, and turbine or compressor including a nozzle or stator vane consisting of said sectors
03/14/2013WO2013034838A1 Method for forming a smooth glaze-like coating on a substrate made of a ceramic matrix composite material containing sic, and part made of a ceramic matrix composite material provided with such a coating
03/14/2013WO2013034837A1 Assembly consisting of a turbine nozzle or a compressor stator vane made of cmc for a turbine engine and an abradable support ring, and turbine or compressor including such an assembly
03/14/2013WO2013034402A1 Method for profiling a replacement blade as a replacement part for an old blade for an axial turbomachine
03/14/2013WO2013034385A1 Guide device for a turbine
03/14/2013US20130065077 Process for Applying a Heat Shielding Coating System on a Metallic Substrate
03/14/2013US20130064681 Trailing edge cooling system in a turbine airfoil assembly
03/14/2013US20130064680 Turbine endwall with grooved recess cavity
03/14/2013US20130064676 Composite filled metal airfoil
03/14/2013US20130064671 Airfoil shape for turbine bucket and turbine incorporating same
03/14/2013US20130064670 Turbine blade
03/14/2013US20130064669 Blade and method for manufacturing blade
03/14/2013US20130064668 Turbine rotor blade assembly and method of assembling same
03/14/2013US20130064667 Turbine blade and non-integral platform with pin attachment
03/14/2013US20130064646 Steam turbine
03/14/2013US20130064619 Method of machining slots in a turbine disk of a turbine engine
03/14/2013DE102012216160A1 Device for measuring vibration of moving blade in e.g. steam turbine, calculates amplitude and frequency of blade vibration based on temporal changes in distance between contactless distance sensor and blade head position
03/14/2013DE102012108184A1 Niederdruckdampfturbine mit schwenkbarer Düse Low-pressure steam turbine with pivoting nozzle
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