Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2007
08/22/2007EP1819904A1 Blade for a flow machine
08/22/2007EP1651841B1 Open-cooled component for a gas turbine, combustion chamber, and gas turbine
08/22/2007EP1147291B1 Compressor endwall bleed system and method of operation
08/22/2007CN1333160C Gas turbine
08/22/2007CN1333153C Impeller for radial turbine
08/22/2007CN101021166A Turbine blade with radial cooling channels
08/22/2007CN101021165A Turbine airfoil with weight reduction plenum
08/22/2007CN101021164A Methods and apparatus for turbine engine rotors
08/22/2007CN101021001A Method of coating gas turbine components
08/21/2007US7258934 outer layer presents a different microstructure than the inner layer; especially dysprosia-stabilized zirconia; low thermal conductivity, sufficient mechanical strength and low weight; gas turbine engines
08/21/2007US7258530 CMC component and method of fabrication
08/21/2007US7258529 Securing assembly
08/21/2007US7258528 Internally cooled airfoil for a gas turbine engine and method
08/21/2007US7258524 Method of regulating the flow rate of air in a rotary shaft of a turbomachine
08/21/2007CA2435444C Cooling structure of stationary blade, and gas turbine
08/21/2007CA2390580C Shroud integral type moving blade of a gas turbine
08/21/2007CA2327857C Turbine nozzle with sloped film cooling
08/21/2007CA2324360C Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine
08/16/2007WO2006074949A8 Turbine blade for turbo-engines and method for manufacturing same
08/16/2007US20070190352 Wear protection coating for a gas turbine component
08/16/2007US20070189901 Separable blade platform
08/16/2007US20070189898 Method and apparatus for cooling gas turbine rotor blades
08/16/2007US20070189897 Turbine blade with radial cooling channels
08/16/2007US20070189896 Methods and apparatus for cooling gas turbine rotor blades
08/16/2007DE102007007177A1 Verfahren und Vorrichtung zum Kühlen von Gasturbinen-Rotorschaufeln Method and apparatus for cooling gas turbine rotor blades
08/16/2007DE102006005364A1 Repairing hollow section components, comprises preparing the damaged area, removing the damaged material, and then replacing the material
08/15/2007EP1818508A1 Nozzle vane assembly for a gas turbine and gas turbine with such nozzle vane assemblies
08/15/2007EP1818507A1 Rotor wheel of a turbomachine
08/15/2007EP1818506A1 HCF stress reduction in fir-trees
08/15/2007EP1818505A1 Process to produce a coating sample
08/15/2007EP1818504A2 Material having internal cooling passage and method for cooling material having internal cooling passage
08/15/2007EP1818503A2 Turbine airfoil with weight reduction plenum
08/15/2007EP1817227A1 Dual counterweight balancing system
08/15/2007EP1387926B1 Inner platform impingement cooling by supply air from outside
08/15/2007EP1348066B1 Assembly method for integrally covered axially inserted bucket blades
08/15/2007CN2934583Y 600MW two-cylinder air cool turbine final blade
08/15/2007CN1332125C Steam turbine closure bucket attachment
08/15/2007CN1332124C Steam turbine wheel dynamic system
08/15/2007CN101018952A Device and method for detachably connecting an impeller to a shaft
08/15/2007CN101016847A High supersound air-intake air turbogenerator
08/15/2007CN101016845A Fluid kinetic energy transforming machine
08/14/2007US7255536 Turbine airfoil platform cooling circuit
08/14/2007US7255535 Cooling systems for stacked laminate CMC vane
08/14/2007US7255534 Gas turbine vane with integral cooling system
08/14/2007US7255531 Gas turbine tip shroud rails
08/14/2007US7255530 Vane and throat shaping
08/14/2007US7255529 Cooling fan mounting arrangement with vibration isolation member
08/14/2007CA2414942C Thermal barrier coating system for turbine components
08/14/2007CA2372016C Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine
08/14/2007CA2357305C Process and device for the softening of the sound interaction between the rotor and the reactor of a turbine engine
08/09/2007WO2007089178A1 A compressor-equipped engine
08/09/2007WO2007087931A1 Measuring apparatus
08/09/2007US20070184287 Environmental barrier coating for silicon-containing substrates and process therefor
08/09/2007US20070184182 Method of repairing the turbine airfoil nozzle segment
08/09/2007US20070183894 Turbomachine rotor wheel
08/09/2007US20070183893 Material having internal cooling passage and method for cooling material having internal cooling passage
08/09/2007US20070181539 Apparatus and method for joining a rotor blade to a rotor mount of a gas turbine rotor
08/09/2007US20070180826 Exhaust gas turbocharger for a reciprocating internal combustion engine and corresponding reciprocating internal combustion engine
08/09/2007US20070180812 Approach to extending life of gas turbine engine
08/09/2007DE4427360B4 Innengekühltes Blatt einer Turbinenrotorschaufel eines Gasturbinenmotors Cooled inner leaf of a turbine rotor blade of a gas turbine engine
08/09/2007DE10005874B4 Schweissverfahren zur Rissreparatur Welding method for crack repair
08/08/2007EP1816316A1 Method for Repairing a Component
08/08/2007EP1816238A1 Preferential hardening of signle crystal blades
08/08/2007EP1815209A1 Improved measurement system
08/08/2007EP1815145A1 Vacuum pump impeller
08/08/2007EP1815108A1 Axial flow turbine with overspeed preventing device
08/08/2007EP1814690A1 Component provided a material filled recess
08/08/2007EP1814689A2 Adaptive machining and weld repair process
08/08/2007CN2931795Y 169mm vane special for 100MW and 200MW steam turbine
08/08/2007CN1330865C Failsafe film cooled wall
08/08/2007CN1330856C Combustion gas turbine nited equipment
08/08/2007CN1330456C Dovetail pin drilling method
08/08/2007CN101014752A Vane wheel of a turbine comprising a vane and at least one cooling channel
08/08/2007CN101012758A Engine blade wheel
08/08/2007CN101012542A Preferential hardening of signle crystal blades
08/08/2007CN101012123A High heat expansion rate heat barrier coating material of Yb2O3 and Gd2O3 doped with YSZ
08/08/2007CA2577502A1 Turbine engine rotor wheel
08/07/2007US7252481 Natural frequency tuning of gas turbine engine blades
08/07/2007US7252480 Methods for generation of dual thickness internal pack coatings and objects produced thereby
08/07/2007US7252000 Method and machine for rotor imbalance determination
08/07/2007US7251888 Hollow fan blade for aircraft engines and method for its manufacture
08/07/2007US7251887 Tool for balancing rotating components
08/07/2007CA2226167C Apparatus and method for locking blades into a rotor
08/02/2007WO2007085512A1 Method for producing a component with holes
08/02/2007WO2007085123A1 A composite type fan with low noise fan blades
08/02/2007WO2007067185A3 Turbine engine components with non-aluminide silicon-containing and chromium-containing protective coatings and methods of forming such non-aluminide protective coatings
08/02/2007WO2007066053A3 Brazed joint between a metal part and a ceramic part
08/02/2007WO2007037773A3 Thermal barrier coating with stabilized compliant microstructure
08/02/2007US20070178329 Method for coating a component for use in a crucible drawing method for quartz glass, and coated component obtained according to the method
08/02/2007US20070177979 Vane comprising a transition zone
08/02/2007US20070177976 Microcircuits for small engines
08/02/2007US20070177975 Film cooling method and hole manufacture
08/02/2007DE19939179B4 Kühlbare Schaufel für eine Gasturbine Coolable blade for a gas turbine
08/02/2007DE102007003775A1 Schaufelblattprofil einer Statorschaufel für einen Verdichter Airfoil profile of a stator vane for a compressor
08/02/2007DE102005060698A1 Sekundärfluidkanalherstellungsverfahren Secondary fluid channel establishment procedure
08/02/2007CA2633334A1 Airfoil for a first stage nozzle guide vane
08/01/2007EP1813792A1 Engine shaft linking system with retractable nut
08/01/2007EP1813781A1 Part of a turbine, turbine and operation method thereof
08/01/2007EP1813776A2 Microcircuits for cooling of small turbine engine blades
08/01/2007EP1813775A2 Film cooling method and method of manufacturing a hole in gas turbine engine part
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