Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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06/19/2014 | WO2014090907A1 Turbomachine blade, corresponding turbomachine and method of manufacturing a turbine blade |
06/19/2014 | WO2014090323A1 Method for treating a component with geographic adaptation |
06/19/2014 | WO2014065916A3 Seal between blade and vane |
06/19/2014 | WO2014058493A3 Suction side turbine blade tip cooling |
06/19/2014 | WO2013162672A8 Gas turbine engine sump pressurization system |
06/19/2014 | US20140170435 Hollow airfoil with composite cover and foam filler |
06/19/2014 | US20140170369 Chordwise lay-up of fibre sheet material for turbine blades |
06/19/2014 | US20140169979 Gas turbine engine fan blade platform seal |
06/19/2014 | US20140169977 Blade cascade and turbomachine |
06/19/2014 | US20140169976 Rotor blade root spacer for arranging between a rotor disk and a root of a rotor blade |
06/19/2014 | US20140169975 Rotor blade root spacer with a fracture feature |
06/19/2014 | US20140169974 Tapered part-span shroud |
06/19/2014 | US20140169973 Ni-Based Heat Resistant Alloy, Gas Turbine Component and Gas Turbine |
06/19/2014 | US20140169972 Fan with integral shroud |
06/19/2014 | US20140169962 Turbine blade with integrated serpentine and axial tip cooling circuits |
06/19/2014 | US20140169961 Propeller rotor balancing system |
06/19/2014 | US20140169953 Drum seal |
06/19/2014 | US20140169935 Lightweight shrouded fan blade |
06/19/2014 | US20140165593 Gas turbine engine turbine blade leading edge tip trench cooling |
06/19/2014 | US20140165592 Compressor blade for gas turbine engine |
06/19/2014 | US20140165591 Turbine under platform air seal strip |
06/19/2014 | US20140165398 Methods of manufacturing divided blades of turbomachines by additive manufacturing |
06/18/2014 | EP2743511A1 Vane profile for axial-flow compressor |
06/18/2014 | EP2743455A2 Turbine blade, in particular final stage rotor blade of a steam turbine, with an erosion protection component |
06/18/2014 | EP2743454A1 Turbine component having cooling passages with varying diameter |
06/18/2014 | EP2743453A1 Tapered part-span shroud |
06/18/2014 | EP2743452A1 Methods of manufacturing divided blades of turbomachines by additive manufacturing |
06/18/2014 | EP2743451A1 Methods of manufacturing turbomachines blades with shaped channels by additive manufacturing, turbomachine blades and turbomachines |
06/18/2014 | EP2743450A1 Drum seal |
06/18/2014 | EP2743449A2 Impeller backface rotating heat shield |
06/18/2014 | EP2743028A1 System and method for manufacturing rotors |
06/18/2014 | EP2742212A1 Film cooling of turbine blades or vanes |
06/18/2014 | EP2742162A1 Forged tial components, and method for producing same |
06/18/2014 | EP2741890A1 Method for producing a protective reinforcement of the leading edge of a vane |
06/18/2014 | DE102012223220A1 Turbinenschaufel, insbesondere Endstufenlaufschaufel für eine Dampfturbine Turbine blade, in particular final stage rotating blade for a steam turbine |
06/18/2014 | DE102012112410A1 Industrial truck for use in explosion-proof design with internal combustion engine, which is provided with exhaust gas turbocharger that is partially closed from liquid-cooled covering having surface contact at flow-through of exhaust gases |
06/18/2014 | CN203655360U 用于汽轮机叶片的超音速叶型 Turbine blades for supersonic airfoil |
06/18/2014 | CN203655359U 船用汽轮机自带冠叶片外包拉筋减振结构 Marine Turbine blade with tips outsourcing stretch vibration structure |
06/18/2014 | CN203655358U 异向网状布置半剖松拉筋长叶片减振结构 Arranged to mesh different half-sectional Songla tendons long blade damping structure |
06/18/2014 | CN203649666U 一种用于汽轮机叶片进气边激光熔覆的坡口结构 Groove structure for the intake side of the turbine blades laser cladding |
06/18/2014 | CN103874580A Thermal barrier coating systems and processes therefor |
06/18/2014 | CN103867235A Tubular vortex reducer air inducing system |
06/18/2014 | CN103867234A Multiple scroll turbocharger |
06/18/2014 | CN103862234A Method and structure for improving strength performance of central part of supercharger turbine |
06/18/2014 | CN102705017B Steam turbine |
06/18/2014 | CN102367745B Low-resistance culvert current type air turbine generating system |
06/18/2014 | CN102165141B Blade row for the final stage of a steam turbine |
06/18/2014 | CN101952554B Magnetic device for damping blade vibrations in turbomachines |
06/18/2014 | CN101852098B Turbine blade assemblies with thermal insulation |
06/18/2014 | CN101379299B Blade for axial-flow fluid machine |
06/17/2014 | US8753093 Bonded turbine bucket tip shroud and related method |
06/17/2014 | US8753090 Bladed disk assembly |
06/17/2014 | US8753087 Turbine rotor assembly and steam turbine |
06/17/2014 | US8753083 Curved cooling passages for a turbine component |
06/17/2014 | US8753072 Turbojet engine nacelle |
06/17/2014 | US8753071 Cooling channel systems for high-temperature components covered by coatings, and related processes |
06/17/2014 | US8753070 Device and method for redirecting a leakage current |
06/17/2014 | CA2764664C Ni-based single crystal superalloy and turbine blade |
06/17/2014 | CA2549091C Durable thermal barrier coating having low thermal conductivity |
06/17/2014 | CA2540906C Turbine nozzle with trailing edge convection and film cooling |
06/12/2014 | WO2014088929A1 A method of fabricating a rotor of a turbofan engine |
06/12/2014 | WO2014088696A1 Apparatus having engineered surface feature and corresponding method to reduce wear and friction in a cmc-to-metal attachment |
06/12/2014 | WO2014087109A1 Propeller blade for a turbomachine |
06/12/2014 | WO2014087093A1 Method for manufacturing a turbine engine blade root of a composite material and blade root obtained by such a method |
06/12/2014 | WO2013021205A3 Turbine generator |
06/12/2014 | US20140161626 Method for manufacturing an oxide/oxide composite material turbomachine blade provided with internal channels |
06/12/2014 | US20140161625 Turbine component having cooling passages with varying diameter |
06/12/2014 | US20140161624 Method for producing a run-in coating, a run-in system, a turbomachine, as well as a guide vane |
06/12/2014 | US20140161623 Turbine engines with ceramic vanes and methods for manufacturing the same |
06/12/2014 | US20140161622 Propeller |
06/12/2014 | US20140161621 Attachment of composite article |
06/12/2014 | US20140161620 Attachment of composite article |
06/12/2014 | US20140161618 Metal Joining And Strengthening Methods Utilizing Microstructural Enhancement |
06/12/2014 | US20140161598 Impeller backface rotating heat shield |
06/12/2014 | US20140161590 Cover device, integrally bladed main rotor body, method and turbomachine |
06/12/2014 | DE102012222745A1 Turbine blade, useful in fluid-flow machine e.g. stationary gas turbine or aircraft engine, comprises monocrystalline of titanium aluminide material in blade portion, and blade root made of polycrystalline material |
06/12/2014 | DE102010052965B4 Dämpfungsmittel zum Dämpfen einer Schaufelbewegung einer Turbomaschine Damping means for damping movement of a blade of a turbomachine |
06/11/2014 | EP2740900A2 System and method for removing heat from a turbine |
06/11/2014 | EP2740899A2 Coated article |
06/11/2014 | EP2740898A1 An airfoil and a cooling arrangement for an airfoil platform |
06/11/2014 | EP2740897A1 Turbine diffuser |
06/11/2014 | EP2740819A1 Alloy of aluminium rich MAX phases, powders and layer system |
06/11/2014 | EP2739828A1 Turbine-engine impeller |
06/11/2014 | EP2739760A1 Method for forming an improved thermal barrier coating (tbc), thermal-barrier-coated article and method for the repair thereof |
06/11/2014 | EP2739529A2 Method for retrofitting vortex generators on a wind turbine blade |
06/11/2014 | CN103857881A Method and apparatus for cooling gas turbine rotor blades |
06/11/2014 | CN103857880A Turbomachine centre blade comprising a curved portion |
06/11/2014 | CN103857879A Axial turbine |
06/11/2014 | CN103850720A Hollow pneumatic motor with outer rotor |
06/11/2014 | CN103850719A Damping blade with piezoelectric material vibration reduction structure |
06/11/2014 | CN103850718A Novel air-film hole with adjoint hole structures |
06/11/2014 | CN103850717A Fillet for use with turbine rotor blade tip shroud |
06/11/2014 | CN103850716A Tear-drop shaped part-span shroud |
06/11/2014 | CN103850715A Rotor wheel disc |
06/11/2014 | CN103846613A Connection method and connection structure of tapered threads of impeller and rotating shaft of turbine of supercharger |
06/11/2014 | CN102248357B Method for manufacturing low-pressure rotor of megawatt-grade supercritical steam turbine unit |
06/11/2014 | CN101910565B Guide vane for a variable turbine geometry |
06/11/2014 | CN101892868B Turbine coverplate systems |
06/11/2014 | CN101779002B Turbine blade |
06/11/2014 | CN101526013B Arrangement for the attachment of turbine blades |