Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2014
04/22/2014US8702391 Gas turbine blade
04/22/2014US8702384 Airfoil core shape for a turbomachine component
04/22/2014US8702379 Quiet blower apparatus and system and method for reducing blower noise
04/22/2014US8702377 Gas turbine engine rotor tip clearance and shaft dynamics system and method
04/22/2014US8701415 Flexible metallic seal for transition duct in turbine system
04/19/2014CA2830565A1 Turbomachine for compressing a fluid
04/17/2014WO2014058718A1 Bi-directional compression fan rotor for a gas turbine engine
04/17/2014WO2014058509A2 Casting cores and manufacture methods
04/17/2014WO2014058505A2 Threaded full ring inner air-seal
04/17/2014WO2014058499A2 Airfoil components containing ceramic-based materials and processes therefor
04/17/2014WO2014058496A2 Blade outer air seal for a gas turbine engine
04/17/2014WO2014058493A2 Suction side turbine blade tip cooling
04/17/2014WO2014057205A1 Method for locally treating a part made from porous composite material
04/17/2014WO2014057199A1 Propeller comprising a movable dynamic scoop
04/17/2014WO2014057194A1 Rotor-stator assembly for a gas-turbine engine
04/17/2014WO2014025440A3 Turbine blade root with microcircuit cooling passages
04/17/2014WO2014006467A3 Tip fabrication for rotor blade or stator vane airfoil
04/17/2014US20140105753 Precipitation Hardening Martensitic Stainless Steel and Long Blade for Steam Turbine Using the Same
04/17/2014US20140105752 Drum pouch wind turbine
04/17/2014US20140105750 Turbine engine blade
04/17/2014US20140105748 Drum Blade Lock in a Circumferential Rotor Groove
04/17/2014US20140105747 Centrifugal pump impellers
04/17/2014US20140105741 Method to improve the thermal properties of a resistance element embedded in an alumina deposit on a surface of a substrate and application of said method
04/17/2014US20140105726 Turbine airfoil vane with an impingement insert having a plurality of impingement nozzles
04/17/2014US20140105725 Fish mouth seal carrier
04/17/2014DE102013111223A1 Kühlfilmlochplateau für Heißgaspfadkomponente Film cooling hole plateau for hot gas path component
04/17/2014DE102013109549A1 System und Verfahren zur Herstellung eines Schaufelblatts System and method for producing a blade
04/17/2014DE102012218692A1 Abgasturboladerwelle mit mit dieser verbundenem Laufrad Exhaust gas turbocharger shaft with associated with this wheel
04/16/2014EP2719866A1 Lock for drum blades in a circumferential rotor groove
04/16/2014EP2719865A1 Insert for disc-blade connections of fluid flow engines
04/16/2014EP2719864A1 Adapter for a blade-disc connection for a rotor of a fluid flow engine and a corresponding rotor of a fluid flow engine
04/16/2014EP2719863A1 Turbine blade
04/16/2014EP2719494A1 Adaptive method for the opening of closed outlets of a component
04/16/2014EP2719493A1 Welding joint and component with different materials
04/16/2014EP2718480A1 Multilayer overlay system for thermal and corrosion protection of superalloy substrates
04/16/2014CN203547803U Turbine cooling blade with impacting bush
04/16/2014CN103732862A Rotor seal wire groove repair
04/16/2014CN103732796A Multilayer overlay system for thermal and corrosion protection of superalloy substrates
04/16/2014CN103732383A Wind turbine blade having a root region with elongated fastening members provided with metal fibres
04/16/2014CN103726885A Lock for drum blades in a circumferential rotor groove
04/16/2014CN103726884A Vibration-reducing structure of net-shaped half-sectional loose tie pieces arranged in different directions for long blade
04/16/2014CN102425458B Frequency modulation method for long blade assembly
04/16/2014CN102392690B Rotating device for heating impeller of turbine
04/16/2014CN102132010B Fixed vane assembly for turbine engine having reduced weight, and turbine engine including at least one such fixed vane assembly
04/15/2014US8696319 Three-dimensionally woven composite blade with spanwise weft yarns
04/15/2014US8696306 Bypass duct of a turbofan engine
04/15/2014US8696304 Turbine disk and blade arrangement
04/15/2014US8695917 Vibration damper mechanism, and a flying machine including a carrier structure and a rotor provided with such a mechanism
04/15/2014CA2625598C Blade tip grinding tooling
04/15/2014CA2607238C Turbomachinery rotor balancing system
04/15/2014CA2607235C Turbomachinery rotor balancing system
04/12/2014CA2829460A1 Drum blade lock in a circumferential rotor groove
04/10/2014WO2014055811A1 Turbine blades with platform cooling and corresponding gas turbine
04/10/2014WO2014055499A1 Sheath with extended wings
04/10/2014WO2014055301A1 Reduced height ligaments to minimize non-integral vibrations in rotor blades
04/10/2014WO2014055299A1 Aluminum based abradable material with reduced metal transfer to blades
04/10/2014WO2014055259A1 Air cooled turbine blade and corresponding method of cooling a turbine blade
04/10/2014WO2014055105A1 Reduced fan containment threat through liner and blade design
04/10/2014WO2014054825A1 Film shape structure of cooling hole for cooling gas turbine blades
04/10/2014WO2014053751A1 Method for producing an aerodynamic part by overmoulding a ceramic shell onto a composite preform
04/10/2014WO2014053327A1 Repairing component edges by means of psp elements and component
04/10/2014WO2014053321A1 Thermal barrier coating system, gas turbine component and method for coating a gas turbine component
04/10/2014WO2014053272A2 Method for manufacturing a turbine assembly
04/10/2014WO2014053185A1 Method for treating a gas turbine blade and gas turbine having said blade
04/10/2014WO2014022107A3 Reinforced articles and methods of making the same
04/10/2014US20140099516 Brazed articles and methods of making the same
04/10/2014US20140099210 System for gas turbine rotor and section coupling
04/10/2014US20140099209 Gas turbine component, method for its production and casting mold for use of this method
04/10/2014US20140099206 Propeller comprising a counterweight system provided with an air discharge channel
04/10/2014US20140099205 Cleat for open-work blade foot
04/10/2014US20140099193 Rotor blade and method for cooling the rotor blade
04/10/2014US20140099189 Gas turbine engine components with lateral and forward sweep film cooling holes
04/10/2014US20140099185 Hydroelectric power generating device and system
04/10/2014US20140099183 Turbine components with passive cooling pathways
04/10/2014US20140096538 Platform cooling of a turbine blade assembly
04/09/2014EP2716872A2 Coated components comprising a silicon-based substrate and a porous thermal barrier coating
04/09/2014EP2716871A2 Turbine component, and turbine component fabrication process
04/09/2014EP2716870A1 Rotor blade, corresponding turbine and method for cooling a rotor blade
04/09/2014EP2716869A2 Hollow airfoil with multiple-part insert
04/09/2014EP2716868A2 Hollow airfoil with multiple-part insert
04/09/2014EP2716867A1 Turbine components with adaptive cooling pathways
04/09/2014EP2716866A2 Gas turbine engine components with lateral and forward sweep film cooling holes
04/09/2014EP2716865A1 An exhaust diffuser
04/09/2014EP2716864A1 Turbine tip leakage reduction system
04/09/2014EP2716787A1 Method for manufacturing a turbine assembly
04/09/2014EP2716405A2 An extruded rotor, a steam turbine having an extruded rotor and a method for producing an extruded rotor
04/09/2014EP2716386A1 Gas turbine component, process for the production of same and casting mould for the use of this method
04/09/2014EP2715274A1 Method and device for measuring a part in a turbine engine
04/09/2014CN103717840A Turbine-engine impeller
04/09/2014CN103717839A Centrifugal impeller and turbomachine
04/09/2014CN103717347A Method for creating a blade for a flow force engine and blade for a flow force engine
04/09/2014CN103711608A Engine airflow passage structure and fanjet
04/09/2014CN101713764B Rotor disk weld inspection method and arrangement
04/09/2014CN101397916B Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
04/08/2014US8690538 Leading edge cooling using chevron trip strips
04/08/2014US8690536 Turbine blade tip with vortex generators
04/08/2014CA2660319C Method for producing a useful layer
04/08/2014CA2589077C Manufacturing process for a turbine engine rotor disk
04/08/2014CA2550535C A method for the treatment of the tip of a turbine blade and a turbine blade treated with a method such as this
04/03/2014WO2014052832A1 Cooled turbine blade with leading edge flow redirection and diffusion
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