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
03/14/2013DE102012016012A1 Turbine of turbocharger of internal combustion engine, sets distance between impeller blades equal to distance extending between flows of exhaust gas interfering impurities
03/14/2013DE102011082604A1 Arrangement for producing or processing through hole extending through thickness of wall of solid body, has contoured body, which is arranged in such way that body is hit directly by water jet
03/14/2013DE102011082493A1 Sicherungssegment zur Schwingungsdämpfung von Turbinenlauf-schaufeln und Rotorvorrichtung Turbine blades backup segment for vibration damping and rotor assembly
03/14/2013CA2848153A1 Method for profiling a replacement blade as a replacement part for an old blade for an axial-flow turbomachine
03/14/2013CA2848018A1 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
03/14/2013CA2847667A1 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 material composite provided with such a coating
03/14/2013CA2847239A1 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
03/14/2013CA2788311A1 Blade and method for manufacturing blade
03/13/2013EP2568119A2 Gas turbine engines with improved trailing edge cooling arrangements
03/13/2013EP2568118A1 Gas-turbine-component
03/13/2013EP2568117A1 Rotating element for a turbomachine with vibration damper, corresponding turbomachine and use of a liquid metal for a vibration damper
03/13/2013EP2568116A2 An aerofoil assembly in a gas turbine
03/13/2013EP2568115A1 Cooling system for gas turbine blades comprising a compressor positioned aft of the turbine stage in flow direction
03/13/2013EP2568114A1 Method for profiling a replacement blade as a replacement part for an old blade on an axial flow machine
03/13/2013EP2567070A1 Light weight shroud fin for a rotor blade
03/13/2013CN202788948U Shrouded moving blade
03/13/2013CN202788947U Triplet movable vane of turbine
03/13/2013CN102971493A Turbine blade and engine component
03/13/2013CN102971446A Thermal barrier for turbine blades, having a columnar structure with spaced-apart columns
03/13/2013CN102971440A Metallic bondcoat with a high gamma/gamma' transition temperature and a component
03/13/2013CN102971217A Airflow-straightening structure for the nacelle of an aircraft engine
03/13/2013CN102971135A Turbomachine blade with complementary asymetric geometry
03/13/2013CN102971099A Process for manufacturing a metal part by selectively melting a powder
03/13/2013CN102966380A Airfoil with array of cooling pins
03/13/2013CN102966379A Shaft assembly for a gas turbine engine
03/13/2013CN101333937B Device for cooling the cavities of a turbomachine rotor disc
03/13/2013CN101191423B Rotary assembly components and methods of fabricating such components
03/12/2013US8393869 Turbine blade assembly including a damper
03/12/2013US8393867 Chambered airfoil cooling
03/12/2013US8393858 Turbine shroud support coupling assembly
03/12/2013CA2520282C Turbine module for gas turbine engine
03/12/2013CA2520069C Turbine module for gas turbine engine with rotor that includes a monobloc body
03/12/2013CA2518979C Fluted tip turbine blade
03/12/2013CA2502793C High efficiency rotor for the second phase of a gas turbine
03/08/2013CA2788235A1 Turbine rotor blade assembly and method of assembling same
03/07/2013WO2013033295A1 Localized cleaning process and apparatus therefor
03/07/2013WO2013029584A1 Method for manufacturing, repairing and/or exchanging a rotor/stator combination system, and a rotor/stator combination system manufactured in accordance wih the method
03/07/2013WO2013029183A1 Scoop-shaped turbine blade and assembly
03/07/2013WO2012098277A4 Dynamic symmetry turbines
03/07/2013WO2012080332A3 Cooling device for a jet engine
03/07/2013WO2011144567A3 Method and device for supplying cooling air to an engine, in particular an aircraft engine, gas turbine, or the like
03/07/2013US20130058793 System for Heat Dissipation from an Internal Actuator in a Rotor Blade
03/07/2013US20130058791 Protective coating for titanium last stage buckets
03/07/2013US20130058788 Light weight shroud fin for a rotor blade
03/07/2013US20130058787 Turbine airfoil
03/07/2013US20130058786 Creep indication system and method for determining creep amount
03/07/2013US20130058785 Vibration damper for rotating parts
03/07/2013US20130058783 Impeller and centrifugal fan using the same
03/07/2013US20130058771 Spring-tensioned stator restraining strap
03/07/2013DE102012108283A1 Kriechanzeigesystem und Verfahren zum Bestimmen eines Kriechbetrags Kriechanzeigesystem and method for determining a Kriechbetrags
03/07/2013DE102012108057A1 Schutzbeschichtung für Titanschaufeln der letzten Stufe Protective coating for titanium blades of the last stage
03/07/2013DE102011055246A1 Komponenten mit einspringend ausgebildeten Kühlkanälen und Verfahren zu ihrer Herstellung Components with re-entrant formed cooling channels and methods for their preparation
03/07/2013CA2845590A1 Localized cleaning process and apparatus therefor
03/06/2013EP2565384A1 Bladed rotor with axial retention system for multiple blade types and corresponding assembling method
03/06/2013EP2565383A2 Airfoil with nonlinear cooling passage
03/06/2013EP2565382A2 Airfoil with array of cooling pins
03/06/2013EP2565381A2 Assembly and method preventing tie shaft to unscrew
03/06/2013EP2565380A2 Hole liners for repair of variable vane shroud counterbore holes
03/06/2013EP2565379A2 System and method for modifying a rotor
03/06/2013EP2565378A2 Rotor casing liner assembly and corresponding power plant
03/06/2013EP2565295A1 Method for stripping gamma-gamma prime coating from gamma-gamma prime alloy
03/06/2013EP2564980A2 Solid state system and method for refurbishment of forged components
03/06/2013EP2564979A2 Bushing to repair circumferential flanged ring
03/06/2013EP2564936A2 Automated wet masking for diffusion coatings
03/06/2013EP2564031A1 Wear-resistant part for the support of a blade of a turbojet engine fan
03/06/2013EP2564030A1 Turbine airfoil and method for thermal barrier coating
03/06/2013EP2564029A1 Gas turbine blade
03/06/2013EP2564028A1 Gas turbine blade
03/06/2013EP2564027A1 Plasma actuator controlled film cooling
03/06/2013EP2563949A1 Removable mask for a turbomachine blade or distributor sector platform
03/06/2013EP2563743A1 Durable environmental barrier coatings for ceramic substrates
03/06/2013CN102959184A Turbine
03/06/2013CN102959183A Combined sealing and balancing arrangement for a turbine disc
03/06/2013CN102958680A Turbomachine blade having even/odd complementary geometry and manufacturing process thereof
03/06/2013CN102953771A Labyrinth damping sealing device with low leakage and high damping performance
03/06/2013CN102953767A High-temperature turbine blade-cooling system
03/06/2013CN102953766A Axially cooled airfoil
03/06/2013CN102953765A Bucket assembly treating apparatus and method for treating bucket assembly
03/06/2013CN102953764A Coupled blade platforms and methods of sealing
03/06/2013CN102953763A Rotatable component, coating and method of coating the rotatable component of an engine
03/06/2013CN102953762A Turbine airfoil and method for controlling a temperature of a turbine airfoil
03/06/2013CN102953761A Rotors
03/06/2013CN102953760A Ni-base alloy large member, ni-base alloy welded structure made of same, and method for manufacturing structure thereof
03/06/2013CN101506477B Steam turbine
03/06/2013CN101435344B Molded metallic blade and manufacturing process for the blade
03/06/2013CN101328532B Method for surface treatment of Cr-steel
03/05/2013US8388315 Method for operating a wind turbine with reduced blade fouling
03/05/2013CA2709140C Axial balancing clip weight for rotor assembly and method for balancing a rotor assembly
03/05/2013CA2558759C Foil for turbo-jet blade
02/2013
02/28/2013WO2013027449A1 Method for calculating unsteady force acting on rotor blade or stator blade, turbine design technique and turbine manufacturing method
02/28/2013WO2013027239A1 Axial flow turbine
02/28/2013WO2013026984A1 Tool for holding a turbine-engine part, including a means for attaching and immobilising the part and an element to be attached to said part by brazing or welding
02/28/2013WO2013026870A1 Turbomachine comprising a coated rotor blade tip and a coated inner housing
02/28/2013WO2013026735A1 Blade arrangement
02/28/2013WO2013026667A1 Exhaust diffuser and method for manufacturing an exhaust diffuser
02/28/2013WO2013026666A1 Exhaust diffuser and method for manufacturing an exhaust diffuser
02/28/2013WO2013026665A1 Exhaust diffuser and method for manufacturing an exhaust diffuser
02/28/2013WO2013026127A1 Cross-wind-axis wind-turbine rotor vane
02/28/2013WO2012149925A3 Cover device, integrally bladed main rotor body, method and turbomachine
02/28/2013US20130052437 Substrates Coated with Wear Resistant Layers and Methods of Applying Wear Resistant Layers to Same
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