Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2008
04/30/2008DE102006049218A1 Verfahren zum Herstellen eines Gasturbinenbauteils A method of manufacturing a gas turbine component
04/30/2008CN101169050A Assembling device for preventing a sealing element from moving along circumference direction and corresponding method
04/30/2008CN101169049A Blade/disk dovetail backcut for blade/disk stress reduction
04/30/2008CN101169048A Erosion-resistant coating and its preparation method
04/30/2008CN101169047A 转子叶片外形优化 Shape optimization of rotor blades
04/30/2008CN100385091C High temperature gas flow passage component with mesh type and impingement cooling
04/30/2008CN100385090C Apparatus and methods for coupling axially aligned turbine rotors
04/29/2008US7364806 Formed via physical vapor deposition; for gas turbines and combustion chambers
04/29/2008US7364802 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity
04/29/2008US7364801 Turbine component protected with environmental coating
04/29/2008US7364405 Microcircuit cooling for vanes
04/29/2008US7364404 Turbomachine with fluid removal
04/29/2008US7364402 Turbine module for a gas turbine engine
04/29/2008US7363707 Braze repair of shroud block seal teeth in a gas turbine engine
04/24/2008WO2008046708A1 Nickel-base superalloys
04/24/2008WO2008046556A2 Turbocharger
04/24/2008WO2008046388A1 High-pressure turbine rotor, and method for the production thereof
04/24/2008WO2008046387A1 High-pressure turbine blade and method of repairing high-pressure turbine blades
04/24/2008WO2008030324A3 Method for damping vibrations in a steam turbine and low coefficient of friction, wear resistant coating for steam turbine blade contact areas
04/24/2008US20080096045 Turbine Engine Components With Non-Aluminide Silicon-Containing and Chromium-Containing Protective Coatings and Methods of Forming Such Non-Aluminide Protective Coatings
04/24/2008US20080095636 Turbine component with tip flagged pedestal cooling
04/24/2008US20080095635 Vane with enhanced heat transfer
04/24/2008US20080095634 Multi-stage turbine using steel and aluminum blades
04/24/2008US20080095633 Fan blade
04/24/2008US20080095632 Turbomachine rotor blade and a turbomachine rotor
04/24/2008US20080095629 Centrifugal fan
04/24/2008US20080095622 Gas Turbine Airfoil With Leading Edge Cooling
04/24/2008US20080095614 Fan platform fin
04/24/2008US20080095613 Balancing system for turbomachine rotor
04/24/2008DE102006049818A1 Fanschaufel aus Textilverbundwerkstoff Fan blade made of textile composite material
04/24/2008DE102006049216A1 Hochdruckturbinen-Rotor und Verfahren zur Herstellung eines Hochdruckturbinen-Rotors High-pressure turbine rotor and method of producing a high-pressure turbine rotor
04/24/2008DE102006041322A1 Dämpfungs- und Dichtungssystem für Turbinenschaufeln Damping and sealing system for turbine blades
04/24/2008CA2665069A1 High-pressure turbine rotor, and method for the production thereof
04/24/2008CA2607238A1 Turbomachinery rotor balancing system
04/24/2008CA2607235A1 Turbomachinery rotor balancing system
04/23/2008EP1914392A2 Turbine case impingement cooling for heavy duty gas turbines
04/23/2008EP1914385A2 Plasma enhanced rapidly expanded gas turbine engine transition duct
04/23/2008EP1914384A2 Part span shrouded fan blisk
04/23/2008EP1914383A2 Fan blade of composite textile material
04/23/2008EP1914382A1 Method for repairing a turbine blade
04/23/2008EP1914327A1 Nickel-base superalloy
04/23/2008EP1914323A2 Method for manufacturing residual compressive stress by shot peening
04/23/2008EP1914036A1 Turbine blade for a turbine with a cooling channel
04/23/2008EP1913176A1 Thermal barrier coating system
04/23/2008EP1670613B1 Method for production of a coating system
04/23/2008EP1478857B1 Compressor with an anti-stall tip treatment
04/23/2008CN201050387Y Exhaust-driven turbo-charger central rotor device
04/23/2008CN101166890A Turbine wheel
04/23/2008CN101165318A Airfoils for use with turbine assemblies and methods of assembling the same
04/23/2008CN100383364C Flow passage sealing of turbine and streamline structure thereof
04/22/2008US7360991 Methods and apparatus for fabricating gas turbine engines
04/22/2008US7360434 Apparatus and method to measure air pressure within a turbine airfoil
04/22/2008CA2367684C High pressure turbine cooling of gas turbine engine
04/22/2008CA2352852C Impeller containment system
04/17/2008WO2008043663A1 Rotor for a turbo-machine
04/17/2008WO2008043340A1 Turbine vane of a gas turbine
04/17/2008US20080090100 Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating
04/17/2008US20080090005 Heat treatment ot a ceramic protectvie coating (oxides of barium, strontium, aluminum and silicon) to form an outer surface region of stoichiometric crystalline phases and crystalline phase free of nonstoichiometric silica; nonporous; heat, corrosion, oxidation chemical resistance; gas turbine engines
04/17/2008US20080089797 Rotary Blood Pump
04/17/2008US20080089788 Part span shrouded fan blisk
04/17/2008US20080089784 Multiblade impeller
04/17/2008US20080088067 Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating
04/17/2008US20080087315 Thermoelectric Fan for Radiation-Based Heaters, and Methods Related Thereto
04/17/2008DE102006048784A1 Verdichter für einen Turbolader sowie Verfahren zu dessen Kühlung Compressor for a turbocharger and method for cooling
04/17/2008DE102006048685A1 Turbinenschaufel einer Gasturbine Turbine blade of a gas turbine
04/17/2008CA2665544A1 Turbine vane of a gas turbine
04/16/2008EP1912038A1 Method for determining the wall thickness of a hollow component
04/16/2008EP1911948A2 Energy generation in a gas turbine with feed for gases containing carbon dioxide
04/16/2008EP1911937A2 A flow cavity arrangement for gas turbine engine
04/16/2008EP1911935A2 Steam turbine rotor blade
04/16/2008EP1911934A1 Mobile blade of a turbomachine
04/16/2008EP1911933A1 Rotor for a turbomachine
04/16/2008EP1911932A2 Turbine rotor and steam turbine
04/16/2008EP1911931A2 Fan exit guide vane and method of repairing therof
04/16/2008EP1911858A1 Process of manufacturing of a coating with columnar structure
04/16/2008EP1910647A1 Securing element for fastening moving blades
04/16/2008EP1910248A1 Cmc with multiple matrix phases separated by diffusion barrier
04/16/2008EP1910018A1 A method and a device for production of a set of holes
04/16/2008EP1910007A1 Method for integrally bonding components using nanoparticles
04/16/2008EP1910006A1 Method of repairing a component comprising a directed microstructure, by setting a temperature gradient during exposure to the laser heat; a component produced by such a method
04/16/2008EP1819904B1 Blade for a flow machine
04/16/2008EP1252424B1 Method of operating a variable cycle gas turbine engine
04/16/2008EP1148967B1 Laser welding superalloy articles
04/16/2008CN101163813A Coating, substrate provided with a coating and method for the application of a corrosion-resistant coating
04/16/2008CN100381781C Surface roughness measuring method and apparatus and turbine deterioration diagnostic method
04/16/2008CN100381689C Piston engine and method for controlling such an engine
04/16/2008CN100381677C Gas turbine pressurizing air supply system
04/15/2008US7357623 Angled cooling divider wall in blade attachment
04/15/2008CA2475402C Hand held powder-fed laser fusion welding torch
04/13/2008CA2606072A1 Mobile turbomachine blade
04/10/2008WO2008042251A2 Axial flow fan
04/10/2008WO2008041889A1 Rotor element and method for producing the rotor element
04/10/2008WO2007143973A3 Thermal barrier layer
04/10/2008US20080085193 Turbine airfoil cooling system with enhanced tip corner cooling channel
04/10/2008DE102006030235B4 Verfahren zum Schutz von Heißgaskorrosion von keramischen Oberflächen oder eines Körpers, hochtemperaturbeständiger Körper und deren Verwendung A method of protecting the hot gas corrosion of ceramic surfaces or a body of high temperature resistant body and their use
04/10/2008DE102004002712B4 Turbinenschaufel-Ermüdungslebensdauer-Bewertungsverfahren und Turbinenschaufel-Kriechdehnungsverformungs-Messvorrichtung Turbine blade fatigue life assessment procedures and turbine blade Kriechdehnungsverformungs measuring device
04/09/2008EP1909061A2 Method for determining the wall thickness of a hollow component
04/09/2008EP1908942A2 Gas turbine engine assembly and method of assembling same
04/09/2008EP1908925A2 Ternary carbide and nitrate thermal spray abradable seal material
04/09/2008EP1908922A2 Device and method for hybrid vapor and film cooling of a turbine blade