Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
12/2009
12/24/2009US20090317242 Method and device for cooling a component of a turbine
12/24/2009US20090317236 Vibration damping novel surface structures and methods of making the same
12/24/2009US20090317234 Crossflow turbine airfoil
12/24/2009US20090317232 Blade shroud with aperture
12/24/2009US20090317227 Airfoil embodying mixed loading conventions
12/24/2009US20090314698 Combined Axial-Radial Intake Impeller With Circular Rake
12/24/2009DE102009025960A1 Schaufelblatt einer Durchströmturbine The airfoil of a Crossflow
12/24/2009DE102008029528A1 Gas i.e. cooling air, guiding device for use in gas turbine of aircraft engine, has two guiding elements provided at two adjacent rotor disks and dimensioned such that pre-determined gap is formed between guiding elements
12/23/2009WO2009154891A1 Windward cooled turbine nozzle
12/23/2009WO2009154243A1 Rotor of rotary machine and method for manufacturing same
12/23/2009WO2009120778A3 Subsonic and stationary ramjet engines
12/23/2009WO2009101596A3 Shrouded turbine blade design
12/23/2009EP2136034A2 A cooling arrangement
12/23/2009EP2136033A1 Wall of turbo machine and turbo machine
12/23/2009EP2136032A2 Gas turbine comprising at least a compressor section having multiple stages compression modules
12/23/2009EP2134542A2 Thermally insulated cmc structure with internal cooling
12/23/2009CN100572757C Gas turbine wing and its manufacture method
12/23/2009CN100572756C Method and device for reducing temperature of turbine blade top region
12/23/2009CN100572601C Protective layer for the protection of a component against corrosion and oxidation at elevated temperatures, and component
12/23/2009CN100572582C Article having a dispersion of ultrafine titanium boride particles in a titanium-base matrix
12/23/2009CA2726773A1 Windward cooled turbine nozzle
12/22/2009US7634910 Torus shapes for torque converters
12/22/2009CA2368288C Laser shock peening integrally bladed rotor blade edges
12/22/2009CA2330218C Method of removing a thermal barrier coating
12/18/2009CA2668605A1 Crossflow turbine airfoil
12/17/2009WO2009150019A1 Blade for a gas turbine and method for producing such a blade by a casting process
12/17/2009US20090312956 Method and apparatus for measuring on-line failure of turbine thermal barrier coatings
12/17/2009US20090311105 Rotary meter flexible edge impeller assembly
12/17/2009US20090311103 Rotor for steam turbine and method of manufacturing the same
12/17/2009US20090311099 Banded turbine
12/17/2009DE102009025936A1 Schaufelkernform für eine Turbinenleitschaufel Blade core shape for a turbine
12/16/2009EP2133513A2 Bearing system
12/16/2009EP2132412A1 Rotor for a gas turbine
12/16/2009CN101603436A High-efficiency mixed flow turbine
12/15/2009US7634385 Methods of measuring steam turbine efficiency
12/15/2009US7632363 Method for refurbishing a service-degraded component of a gas turbine
12/15/2009US7632362 Property recovering method
12/15/2009US7632075 External profile for turbine blade airfoil
12/15/2009US7632074 HP turbine blade airfoil profile
12/15/2009US7632073 Impeller with machining access panel
12/15/2009US7632072 Third stage turbine airfoil
12/15/2009US7632071 Cooled turbine blade
12/15/2009US7632063 Fan and blower unit having the same
12/15/2009US7632062 Turbine rotor blades
12/15/2009CA2557493C Blade or vane for a turbomachine
12/15/2009CA2545954C Layer system and process for producing a layer system
12/15/2009CA2370256C Method for refurbishing a coating including a thermally grown oxide
12/10/2009WO2009148655A2 Turbine airfoil with metered cooling cavity
12/10/2009WO2009126191A3 Sealing arrangement for turbine engine having ceramic components
12/10/2009US20090304520 Serpentine cooling circuit and method for cooling tip shroud
12/10/2009US20090304519 Gas-Compressor Impeller and Gas Compressor Having The Same
12/10/2009US20090304518 Turbofan engine
12/10/2009US20090304517 Component structure
12/10/2009US20090304516 Platform mate face contours for turbine airfoils
12/10/2009US20090304515 Method and device for joining by way of inductive hf pressure welding a rotor blade with a rotor support of a gas turbine with automatic supply of the rotor blade
12/10/2009US20090304514 Method of manufacturing a turbine rotor
12/10/2009US20090304513 Rotor assembly for a wind turbine and method of assembling the same
12/10/2009US20090304509 Balancing system for turbomachine rotor
12/10/2009US20090304508 Self-adjusting wind turbine generator blade
12/10/2009US20090304494 Counter-vortex paired film cooling hole design
12/10/2009US20090301091 Compressor-less micro gas turbine power generating system
12/10/2009DE102009025880A1 Leitschaufel für den Lufteinlass einer Turbine The air inlet guide vane for a turbine
12/10/2009DE102008026936A1 Vorrichtung zur Verwendung in einem Verfahren zur Herstellung einer Schutzschicht und Verfahren zur Herstellung einer Schutzschicht An apparatus for use in a method for producing a protective layer and method of manufacturing a protective layer
12/09/2009EP2131108A2 Counter-vortex film cooling hole design
12/09/2009EP2131011A2 Particle resistant in-wall cooling passage inlet
12/09/2009EP2131010A1 Gas turbine blade and method for producing a gas turbine blade
12/09/2009EP2130933A1 Coating material, method for production thereof, coating method, rotor blade equipped with shroud
12/09/2009EP2129871A1 Arrangement for axially securing rotating blades in a rotor, and gas turbine having such an arrangement
12/09/2009EP2129870A1 Method and device for coating components of a gas turbine
12/09/2009EP2129812A2 Turbomachine blade with erosion and corrosion protective coating and method of manufacturing the same
12/09/2009EP2024684B1 Gas turbine comprising armor-plated machine components
12/09/2009CN101600853A Turbine bucket
12/09/2009CN101596665A Technology method for connecting three-body structure of titanium aluminum alloy turbine rotation shaft
12/09/2009CN100567518C Component, method for producing said component and device for generating internal compressive stress in the component
12/08/2009US7628589 Turbo-engine and rotor for a turbo-engine
12/08/2009US7628588 Coated bucket damper pin
12/08/2009US7628587 Gas turbine blade shroud
12/08/2009US7628585 Airfoil leading edge end wall vortex reducing plasma
12/08/2009US7628580 Variable geometry turbine
12/08/2009US7628578 Vane assembly with improved vane roots
12/08/2009CA2445756C Turbine or compressor device and method for assembling the device
12/08/2009CA2202255C Platinum aluminide cvd coating method
12/03/2009WO2009144409A1 Annular flange for attaching a rotor or stator element
12/03/2009WO2009144401A1 Turbomachine fan rotor
12/03/2009WO2009144300A1 Assembly including a turbine disc for a gas turbine engine and a bearing-supporting journal, and cooling circuit for the turbine disc of such an assembly
12/03/2009WO2009143909A1 Method and device for welding workpieces made of high-temperature resistant super alloys
12/03/2009WO2009143819A1 Process for repairing single-crystal high-pressure turbine blades by diffusion brazing
12/03/2009US20090297876 Thermal barrier layer
12/03/2009US20090297361 Minimization of fouling and fluid losses in turbine airfoils
12/03/2009US20090297360 Breeze Enhancing Fan Blade Attachment
12/03/2009US20090297359 High Modulus Metallic Component For High Vibratory Operation
12/03/2009US20090297358 Modified blade stiffener and fabrication method therefor
12/03/2009US20090297357 Propfan assembly
12/03/2009US20090297356 Method of replacing a composite airfoil
12/03/2009US20090297355 Wind turbine blade planforms with twisted and tapered tips
12/03/2009US20090297354 Wind turbine blades with twisted and tapered tips
12/03/2009US20090297353 Wind turbine blades with twisted tips
12/03/2009US20090297351 Compressor rotor blade undercut
12/03/2009US20090297350 Hoop snap spacer
12/03/2009US20090297348 Adjusting apparatus for adjusting the pitch angle of propeller blades, variable-pitch propeller, control function which can be implemented in a computer, and method for adjusting the pitch angle of propeller blades