Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
02/2011
02/10/2011US20110033303 Turbomachine compressor rotor including centripetal air bleed means
02/10/2011US20110033302 Fan blade dovetail with compliant layer
02/10/2011US20110033292 Energy absorbing fan blade spacer
02/10/2011US20110033280 Hybrid ram air turbine with inlet guide vanes
02/10/2011DE102010036623A1 Sicherungszwischenstückanordnung für ein Rotorschaufelbefestigungssystem mit umlaufendendem Schwalbenschwanz Fuse adapter assembly for a rotor blade mounting system with dovetail umlaufendendem
02/10/2011DE102009036406A1 Schaufelblatt Airfoil
02/10/2011DE102009036405A1 Reparatur von Turbinenbauteilen und Lotlegierung hierfür Repair of turbine components and solder alloy thereof
02/10/2011DE102009036342A1 Method for reinforcing edge area of highly loaded component e.g. gas turbine blade, in airplane, involves reinforcing component area by arranging stabilization element, and removing stabilization element
02/10/2011CA2769696A1 Hub for a propeller having variable pitch blades
02/09/2011EP2282015A1 Turbo machine with an Improved Seal
02/09/2011EP2282012A1 Guide vane of a gas turbine and method for replacing a cover plate of a guide vane of a gas turbine
02/09/2011EP2282010A1 Rotor blade for an axial flow turbomachine
02/09/2011EP2282009A1 Serpentine microcircuit vortex turbulators for blade cooling
02/09/2011EP2281913A1 Lubricated abradable coating
02/09/2011EP2281653A1 A method of friction welding a first workpiece to a second workpiece with converging parts
02/09/2011EP2281108A2 Device for bleeding air from a turbomachine compressor
02/09/2011EP2280801A1 Method and device for welding workpieces made of high-temperature resistant super alloys
02/09/2011CN101970803A 带冠涡轮叶片设计 Shrouded turbine blade design
02/09/2011CN101970802A Cover for cooling passage, method of manufacturing the cover, and gas turbine
02/09/2011CN101970170A Method for manufacturing hollow blade
02/09/2011CN101525727B Heat-resisting steel material used as vane or bolt of ultra-supercritical steam turbine and preparation method thereof
02/08/2011US7883320 Article having diffuser holes and method of making same
02/08/2011US7882639 Braze repair of shroud block seal teeth in a gas turbine engine
02/08/2011CA2440995C Control of the axial position of a fan blade
02/08/2011CA2388778C Turbomachine rotor assembly with two bladed-discs separated by a spacer
02/03/2011WO2011013167A1 Erosion resistant machine component, method for forming surface layer of machine component, and steam turbine manufacturing method
02/03/2011WO2011012819A1 Method for manufacturing a thermal barrier
02/03/2011WO2011012818A1 Part comprising a substrate supporting a ceramic coating layer
02/03/2011US20110027103 Impeller which includes improved means of cooling
02/03/2011US20110027102 Cooling structure of turbine airfoil
02/03/2011US20110027099 Metal component, turbine component, gas turbine engine, surface processing method, and steam turbine engine
02/03/2011US20110027096 Method of manufacture of aerofoil leading edge strip
02/03/2011US20110027093 Anti-wear device of a turbomachine rotor
02/03/2011US20110027092 Arrangement for axially securing rotating blades in arotor, and gas turbine having such an arrangement
02/03/2011US20110027090 Locking spacer assembly for a circumferential dovetail rotor blade attachment system
02/03/2011US20110027088 Rotor blades for turbine engines
02/03/2011DE112009000626T5 Verfahren zur visuellen Untersuchung beschichteter Komponenten auf Erosionsschäden A method for visual inspection of coated components on erosion damage
02/03/2011DE102010017105A1 Rotorschaufeln für Turbinenanlagen Rotor blades for turbine installations
02/03/2011DE102009035841A1 Producing an oxidation-protective-coating and a thermal insulation coating on a substrate exposed to high temperatures, comprises e.g. producing two different powders comprising submicroparticles or nanoparticles
02/03/2011DE102009035689A1 Fluid-dynamic effective rotor e.g. propeller, for use in e.g. ship, has contour regions arranged in relationship e.g. coincidental relationship, of part of rotor blades so that regions blow-out waves of specific wavelength and frequency
02/03/2011DE102009034420A1 Device for joining turbine wheel with shaft of exhaust turbo charger, particularly for combustion engine, has appliances that are formed by metal center pin inserted in holes of turbine wheel and shaft
02/03/2011CA2769198A1 Method for manufacturing a thermal barrier
02/03/2011CA2769196A1 Part comprising a substrate supporting a ceramic coating layer
02/02/2011EP2280177A2 Charging device, in particular exhaust gas turbocharger for a motor vehicle
02/02/2011EP2280149A1 Shroud integral type moving blade and split ring of gas turbine
02/02/2011EP2279852A1 Gas turbine engine and method including composite structures with embedded integral electrically conductive paths
02/02/2011EP2279826A1 Brazing repair material and brazing repair method using the brazing repair material
02/02/2011EP2279817A1 Directionally solidified elongated component with elongated grains of differing widths
02/02/2011EP1673490B1 Component with a protective layer for the protection of the component against corrosion and oxidation at elevated temperatures
02/02/2011CN201730680U Electric turbocharger
02/02/2011CN1875169B Turbine cascade structure
02/02/2011CN101963075A Method for changing pure condensation into back pressure heat supply
02/02/2011CN101337299B Welding manufacture method of hollow stationary blade of steam turbine
02/01/2011US7878763 Turbine rotor blade assembly and method of assembling the same
02/01/2011US7878762 Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor
02/01/2011US7878761 Turbine blade with a showerhead film cooling hole arrangement
02/01/2011US7878759 Mitigation of unsteady peak fan blade and disc stresses in turbofan engines through the use of flow control devices to stabilize boundary layer characteristics
01/2011
01/30/2011CA2709140A1 Axial balancing clip weight for rotor assembly and method for balancing a rotor assembly
01/29/2011CA2711325A1 Nickel-based superalloy, mechanical component made of the above mentioned superalloy, piece of turbomachinery which includes the above mentioned component and related methods
01/27/2011WO2011010059A2 Device for retaining a blade for a turbine engine propeller
01/27/2011WO2011009431A1 Method for replacing a blade of a rotor having integrated blades and such a rotor
01/27/2011WO2011009430A1 Method for coating a turbine blade
01/27/2011US20110020137 Spar and shell constructed turbine blade
01/27/2011US20110020132 DECOMPRESSION MACHINE (SUDARSHAN CHAKRA) SU [good], DARHAN [looking;appearance] CHAKRA [wheel]
01/27/2011US20110020127 Component Comprising Overlapping Weld Seams and Method for the Production Thereof
01/27/2011US20110020126 Modular rotor blade for a power-generating turbine and a method for assembling a power-generating turbine with modular rotor blades
01/27/2011US20110020125 Arrangement for axially securing blades in a rotor of a gas turbine
01/27/2011US20110020116 Gas turbine
01/27/2011US20110020115 Refractory metal core integrally cast exit trench
01/27/2011US20110018282 Wind turbine blade and wind power generator using the same
01/27/2011US20110016884 Cooling passage cover, manufacturing method of the cover, and gas turbine
01/27/2011US20110016875 Guide vane having hooked fastener for a gas turbine
01/27/2011DE112009000627T5 Erosionsschutzsysteme und Komponenten die diese enthalten Include erosion control systems and components, these
01/27/2011DE112009000611T5 Verfahren zum Herstellen von Komponenten mit verbesserter Erosionsbeständigkeit A process for the manufacture of components having improved erosion resistance
01/27/2011DE102009033753A1 Hollow turbine blade i.e. hollow guide vane, film cooling method, involves passive-controlling flow separation at blade, and bending nozzles under angle in transverse direction to mainstream direction of gas and under another angle
01/27/2011CA2768537A1 Device for retaining a blade for a turbine engine propeller
01/27/2011CA2710896A1 Axial flow fan for external rotor
01/26/2011EP2278126A2 Method and system for tuning a frequency of a rotating body
01/26/2011EP2278124A1 Swept turbomachinery blade
01/26/2011EP2276920A2 Subsonic and stationary ramjet engines
01/26/2011EP2276911A1 Turbomachine rotor comprising an anti-wear plug, and anti-wear plug
01/26/2011EP2179143B1 Gap cooling between combustion chamber wall and turbine wall of a gas turbine installation
01/26/2011EP1853795B1 Method for machining an integrally bladed rotor
01/26/2011EP1723339B1 Compressor of a gas turbine and gas turbine
01/26/2011CN201723256U Novel steam turbine
01/26/2011CN101960285A Method for testing the coating of a vane base
01/26/2011CN101960098A Droplet impact protection layer for a shovel
01/26/2011CN101960097A Turbine blade with tip cooling and corresponding turbine and turboengine
01/26/2011CN101960096A Turbine vane for a stationary gas turbine
01/26/2011CN101960095A Blade with non-axisymmetric platform: recess and boss on the extrados
01/26/2011CN101960094A Blade with non-axisymmetric platform
01/26/2011CN101960093A Blade with 3D platform comprising an inter-blade bulb
01/26/2011CN101960092A 涡轮盘及燃气轮机 Turbine and gas turbine disc
01/26/2011CN101960091A Wheel for hydraulic machine, hydraulic machine including such wheel, and energy conversion plant including such hydraulic machine
01/26/2011CN101956575A Turbine bucket lockwire rotation prevention
01/26/2011CN101956574A 旋转体 Rotator
01/26/2011CN101956573A Turbine bucket tip cover comprising a plurality of depressions
01/26/2011CN101956572A Rotor structure of turbine
01/26/2011CN101087928B Static gas turbine component and method for repairing such a component
01/25/2011US7874806 Turbomachine rotor blade and a turbomachine rotor