Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
02/2012
02/02/2012US20120027609 Wind turbine rotor blade with precured fiber rods and method for producing the same
02/02/2012US20120027608 Rotor Blade Section and Method for Assembling a Rotor Blade for a Wind Turbine
02/02/2012US20120027606 Rotor assembly disk spacer for a gas turbine engine
02/02/2012US20120027605 Turbomachine blade, a rotor, a low pressure turbine, and a turbomachine fitted with such a blade
02/02/2012US20120027604 Composite vane mounting
02/02/2012US20120027603 Dual blisks in the high-pressure compressor
02/02/2012US20120027601 Rotatable component mount for a gas turbine engine
02/02/2012US20120027600 Separative tidal current rotor blade
02/02/2012US20120027598 Rotor cover plate retention method
02/02/2012US20120027597 Centrifugal fan
02/02/2012US20120027588 Root flap for rotor blade in wind turbine
02/02/2012US20120027584 Turbine seal system
02/02/2012US20120023945 Method and device for cooling steam turbine generating facility
02/02/2012DE19940556B4 Vorrichtung zum Kühlen von Leit- oder Laufschaufeln in einer Gasturbine Device for the cooling of guide vanes or rotor blades in a gas turbine
02/02/2012DE102009037410B4 Erosionsschutz für Dampfturbinenstufen Erosion control for steam turbine stages
02/02/2012CA2806031A1 Inter-vane seal for a wheel of a turbine or a turbomachine compressor
02/01/2012EP2412940A2 Rotatable component mount for a gas turbine engine
02/01/2012EP2412938A2 Shaft assembly for a gas turbine engine
02/01/2012EP2412929A1 Cmc turbine stator vane
02/01/2012EP2412927A1 Turbine blade
02/01/2012EP2412926A2 Hollow blade for a gas turbine
02/01/2012EP2412925A1 Turbine blade and gas turbine
02/01/2012EP2412924A2 A disk spacer for a gas engine turbine and a method for providing a rotor assembly
02/01/2012EP2412923A2 Rotor cover plate retention
02/01/2012EP2412922A1 Low-pressure steam turbine and method for operating thereof
02/01/2012EP2412469A1 High pressure compressor with welded dual discs in Ti6242 and Ti6246 ; Method of manufacturing such high pressure compressor
02/01/2012EP2412430A1 Bladed reactor for the pyrolysis of hydrocarbons
02/01/2012EP2411631A1 Sealing plate and rotor blade system
02/01/2012EP2411630A1 Axial turbomachine rotor having blade cooling
02/01/2012EP2411629A1 Gas turbine
02/01/2012EP2411216A1 Coating of fatigue corrosion cracked metallic tubes
02/01/2012EP2193225B1 Bimetallic bond layer for thermal barrier coating on superalloy
02/01/2012CN102341588A Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train
02/01/2012CN102341568A Rotor element with a fluid passage and passage-blocking member, and turbine engine including the rotor element
02/01/2012CN102341567A Turbine Rotor Blade
02/01/2012CN102337932A Radial-flow turbine
02/01/2012CN102337931A Rotor, expansion machine and engine using rotor and expansion machine system
01/2012
01/31/2012US8107239 Electronic apparatus and cooling fan
01/31/2012US8105043 HP turbine blade airfoil profile
01/31/2012US8105042 Intermediate-manufactured composite airfoil and methods for manufacturing
01/31/2012US8105041 Arrangement for axially securing rotating blades in a rotor, sealing element for such an arrangement, and use of such an arrangement
01/31/2012US8105039 Airfoil tip shroud damper
01/31/2012US8105038 Steam turbine, and intermediate support structure for holding row of long moving blades therein
01/31/2012US8105033 Particle resistant in-wall cooling passage inlet
01/31/2012US8105032 Systems and methods for internally cooling a wheel of a steam turbine
01/31/2012US8105031 Cooling arrangement for turbine components
01/31/2012US8105030 Cooled airfoils and gas turbine engine systems involving such airfoils
01/31/2012US8105016 Damping arrangement for guide vanes
01/31/2012US8105014 Gas turbine engine article having columnar microstructure
01/26/2012WO2011086055A3 Blade disc having a circular groove for receiving blade bases
01/26/2012US20120020806 Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine
01/26/2012US20120020805 Reverse cavity blade for a gas turbine engine
01/26/2012US20120020804 Turbine nozzle segment having arcuate concave leading edge
01/26/2012US20120020803 Turbine blades, systems and methods
01/26/2012US20120020802 Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structure
01/26/2012US20120020800 Optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine
01/26/2012US20120020799 Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbine
01/26/2012US20120020797 Vortex reducing device for a gas turbine engine
01/26/2012US20120020796 Retaining ring
01/26/2012US20120020794 Rotor with inlet perimeters
01/26/2012US20120020793 Turbine blade system
01/26/2012US20120020789 Turbine wheel having de-tuned blades and including a damper device
01/26/2012US20120020787 Cooled blade for a gas turbine
01/26/2012DE112009002628T5 Schaufel für eine Gasturbine Blade for a gas turbine
01/26/2012DE102011052077A1 Turbinenleitapparatsegment mit bogenförmiger konkaver Vorderkante Turbine nozzle arcuate concave front edge
01/26/2012DE102010032098A1 Verfahren zur Herstellung eines Werkstücks mit definierter Oberfläche A process for producing a workpiece with a defined surface
01/26/2012DE102010032097A1 Verdichterschaufel eines Gasturbinentriebwerks mit selbstschärfender Vorderkantenstruktur Compressor blade of a gas turbine engine with self-sharpening leading edge structure
01/26/2012DE102010031795A1 Verfahren zur Reparatur von Gasturbinenbauteilen aus keramischen Verbundwerkstoffen und Vorrichtung zur Durchführung des Verfahrens A process for the repair of gas turbine components made of ceramic composite materials and apparatus for performing the method
01/26/2012CA2746882A1 An optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine
01/26/2012CA2746714A1 An optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the second stage of a turbine
01/26/2012CA2746643A1 An optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the first stage of a turbine
01/26/2012CA2746575A1 An optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbine
01/26/2012CA2746290A1 An optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the fourth stage of a turbine
01/25/2012EP2410136A2 Vortex reducing device for a gas turbine engine
01/25/2012EP2410132A2 Compressor blade of a gas turbine engine with self-sharpening leading edge structure
01/25/2012EP2410131A2 Rotor of a turbomachine
01/25/2012EP2410130A2 Fan outlet guide vanes of a turbofan engine
01/25/2012EP2410129A2 Rotationally balancing a rotating part
01/25/2012EP2410126A1 Turbine wheel
01/25/2012EP2409793A1 Method for manufacturing a workpiece with defined surface
01/25/2012EP2409127A1 Method and device for measuring physical properties on a turbocharger core assembly
01/25/2012EP2409002A2 Tandem blade design
01/25/2012EP2408584A1 Method for producing an integrally bladed rotor, rotor and apparatus for carrying out the method
01/25/2012EP1825177B1 Inflatable bleed valve for turbine engine and method of controlling bleed air
01/25/2012CN102333935A Turbine blade and gas turbine
01/25/2012CN102330572A Rotor of a turbomachine
01/25/2012CN102330571A Turbine blade with enhanced wake mixing via fluidic-generated vortices
01/24/2012US8103375 Fillet machining system
01/24/2012US8100667 Turbomachinery disc
01/24/2012US8100662 Fan blade made of a textile composite material
01/24/2012US8100661 Wind turbine rotor blade and wind turbine rotor
01/24/2012US8100659 HP turbine vane airfoil profile
01/24/2012US8100654 Turbine blade with impingement cooling
01/24/2012US8100653 Gas-turbine blade featuring a modular design
01/24/2012US8100640 Blade outer air seal with improved thermomechanical fatigue life
01/24/2012US8100638 Centering device
01/24/2012US8100635 Control of clearance at blade tips in a high-pressure turbine of a turbine engine
01/24/2012US8100634 Vane and a vane assembly for a gas turbine engine
01/24/2012CA2496093C Process for producing components or semi-finished products which contain intermetallic titanium aluminide alloys, and components producible by the process
01/24/2012CA2472324C Cooled blade of a gas turbine starter
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