Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2008
08/28/2008US20080206061 Optimized aerodynamic airfoil for a turbine blade
08/28/2008US20080206060 Forming firtree profiles
08/28/2008US20080206058 Method for reducing vibration levels of a bladed wheel in a turbomachine
08/28/2008US20080206057 Blade shroud vibration monitor
08/28/2008US20080206056 Modular Tip Turbine Engine
08/28/2008US20080206054 Aerofoil assembly
08/28/2008US20080206046 Rotor seal segment
08/28/2008US20080206040 Anti-Stall Casing Treatment For Turbo Compressors
08/28/2008US20080203235 Apparatus for measuring a turbine blade
08/28/2008US20080202236 Method and apparatus for balancing the rotating elements of a dental handpiece
08/28/2008DE102007009468A1 Making low-density, heat-resistant structural parts, e.g. gas turbine blades, involves hardening a material comprising heat-resistant hollow spheres and inorganic adhesive by heating to not above the usage temperature
08/28/2008DE102007009134A1 Verdichter einer Gasturbine Compressor of a gas turbine
08/28/2008CA2677941A1 Coating for gas turbine components, and method and device for providing a coating
08/28/2008CA2621842A1 Turbomachine fan
08/27/2008EP1961919A2 Variable rotor blade for gas turbine engine
08/27/2008EP1961918A1 Rotor turbine
08/27/2008EP1961917A2 Local indented trailing edge heat transfer devices
08/27/2008EP1961916A1 Aerodynamic profile optimized for a turbine blade
08/27/2008EP1961915A2 Method of manufacturing a rotor and exhaust turbocharger incorporating the rotor
08/27/2008EP1961914A1 Automated method for conducting a refurbishment measure on a turbine of a thermal power plant
08/27/2008EP1961833A1 Thermal barrier coating systems and materials
08/27/2008EP1960320A2 Brazed joint between a metal part and a ceramic part
08/27/2008CN101250703A Gas turbine steel component anticorrosion composite coating
08/27/2008CN100414075C Turbine moving blade
08/27/2008CA2621839A1 Method for reducing the vibratory level of an turbine engine impeller
08/26/2008US7416394 Gas turbine and rotor blade for a turbomachine
08/26/2008US7416393 Apparatus and method for joining a rotor blade to a rotor mount of a gas turbine rotor
08/26/2008US7416391 Bucket platform cooling circuit and method
08/26/2008US7416390 Turbine blade leading edge cooling system
08/26/2008US7416389 Methods and apparatus for assembling rotatable machines
08/26/2008US7415763 Bending device and method for bending a plate
08/26/2008CA2355692C Method for forming a metal alloy coating such as mcraly
08/21/2008WO2008100306A2 Thermally insulated cmc structure with internal cooling
08/21/2008WO2008100305A1 Turbine blade having a convergent cavity cooling system for a trailing edge
08/21/2008WO2007133538A3 Fluid energy converter
08/21/2008US20080200082 Jet Pumping Device
08/21/2008US20080199321 Parabolic radial flow impeller with tilted or offset blades
08/21/2008US20080199320 Detachable leading edge for airfoils
08/21/2008US20080199317 Local indented trailing edge heat transfer devices
08/21/2008US20080199313 Method of manufacturing rotor and exhaust turbo-supercharge incorporating the rotor
08/21/2008US20080199303 Gas Turbine Engine Cooling System and Method
08/21/2008DE19983957B4 Beschichtungszusammensetzung für Hochtemperturschutz A coating composition for Hochtemperturschutz
08/21/2008DE102007008319A1 Verfahren zur Prallluftkühlung für Gasturbinen A method for impingement air cooling for gas turbines
08/21/2008DE102007007509A1 Turbine, particularly for supercharger, has shaft and crosswise press connected turbine wheel, where turbine wheel has smaller thermal expansion coefficient than shaft
08/20/2008EP1959145A2 Arrangement of air intake circuits for a compressor stage
08/20/2008EP1959101A2 Turbine rotor with cover plate
08/20/2008EP1959100A2 Heat resistant member
08/20/2008EP1959099A2 Thermal barrier coating material, thermal barrier member, and member coated with thermal barrier and method for manufacturing the same
08/20/2008EP1959098A1 Turbine rotor blade, turbine rotor and steam turbine comprising them
08/20/2008EP1959097A2 Impingement skin core cooling for gas turbine engine blade
08/20/2008EP1959096A2 Method for impingement cooling for gas turbines
08/20/2008EP1959095A2 Dimensional restoration of stator inner shrouds
08/20/2008EP1957755A1 Turbomachine having axial rotor blade securing
08/20/2008EP1957754A2 Multilayered erosion resistant coating for gas turbines
08/20/2008EP1759102B1 Exhaust gas turbocharger for a reciprocating internal combustion engine and corresponding reciprocating internal combustion engine
08/20/2008EP1558938B1 Turbo engine
08/20/2008CN201103427Y Longitudinal tree type P blade root used for intermediate pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103426Y T blade root used for high pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103425Y T blade root used for high pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103424Y Longitudinal tree type P blade root used for intermediate pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103423Y Longitudinal tree type R blade root used for intermediate pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103422Y Longitudinal tree type R blade root used for intermediate pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103421Y Longitudinal tree type P blade root used for intermediate pressure cylinder blade of macrotype full rotary speed turbine
08/20/2008CN201103420Y High-pressure triplet regulation level moving vane of macrotype full rotary speed turbine
08/20/2008CN201103419Y Second last blade of macrotype supercritical air cooling turbine
08/20/2008CN201103418Y Second last blade of macrotype full rotary speed (60Hz) turbine
08/20/2008CN101245712A High power generator set water supply pump turbine
08/20/2008CN101245711A Axial flow impeller machine design method and blade
08/19/2008US7413409 Turbine airfoil with weight reduction plenum
08/19/2008US7413407 Turbine blade cooling system with bifurcated mid-chord cooling chamber
08/19/2008US7413406 Turbine blade with radial cooling channels
08/19/2008US7413405 Bipedal damper turbine blade
08/19/2008US7413403 Turbine blade tip cooling
08/19/2008US7413399 Method and apparatus for distributing fluid into a turbomachine
08/19/2008US7412780 Template for inspecting and marking repair areas on an object
08/19/2008CA2413640C Process for rejuvenating a diffusion aluminide coating
08/19/2008CA2406430C Method for removing metal cladding from airfoil substrate
08/19/2008CA2349303C Turbine blade to disk retention device
08/14/2008WO2008097287A2 Aero-mixing of rotating blade structures
08/14/2008WO2008095463A1 Device for the protection of components having a flammable titanium alloy from titanium fire, and method for the production thereof
08/14/2008WO2008035135A3 First stage turbine airfoil
08/14/2008US20080193298 Treatment of turbine blades to increase hardness
08/14/2008US20080193294 Industrial ceiling fan
08/14/2008US20080193293 Bladed disk assembly method and impact device
08/14/2008US20080193278 Integrated support/thermocouple housing for impingement cooling manifolds and cooling method
08/13/2008EP1956347A2 Tapered, frequency-tuned rotor for turbine flow meter
08/13/2008EP1956195A2 Heater for the surface of a gas turbine component
08/13/2008EP1956194A1 Turbine assembly comprising a securing member and process of securing a side plate
08/13/2008EP1956193A1 Component with a strip conductor made of indium and tin and the application of indium tin oxide as wear indicator
08/13/2008EP1956190A1 Blade profile for a blade of a turbine assembly and turbine assembly
08/13/2008EP1956189A1 Turbine wheel for a turbocharger
08/13/2008EP1956116A1 Removal of thermal barrier coatings
08/13/2008EP1954919A1 Device for absorbing sound in power plants
08/13/2008EP1954854A1 Two-layer thermal protective coating system with pyrochlore phase
08/13/2008EP1954436A2 Titanium-aluminide turbine wheel and shaft assembly, and method for making same
08/13/2008EP1444417B1 Turbine blade cooling system and method of cooling a turbine blade
08/13/2008CN101240719A Gas turbine with high pressure and low pressure counter-rotating turbines
08/13/2008CN100410496C High efficiency stator for the first phase of a gas turbine
08/13/2008CN100410495C High efficiency stator for the second phase of a gas turbine
08/13/2008CN100410494C High efficiency rotor for a gas turbine