Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2013
04/24/2013CN103061859A Engine turbocharger and water pump integrated device
04/24/2013CN103061831A System and method for integrating sections of a turbine
04/24/2013CN103061825A Turbine blade, turbine rotor using thereof and steam turbine
04/24/2013CN103061824A Method and system for use in regulating temperature of component
04/24/2013CN103061823A Lacing hole structure of turbine blade and loose lacing wire installation structure of the same turbine blade
04/24/2013CN103056604A Components with laser cladding and methods of manufacture
04/24/2013CN101476493B 蒸汽涡轮机 Steam turbine
04/23/2013US8425196 Wind turbine blades with a hardened substrate construction
04/23/2013US8425194 Clamped plate seal
04/23/2013US8425193 Blade row for the final stage of a steam turbine
04/23/2013US8425185 Transonic blade
04/23/2013US8425183 Triforial tip cavity airfoil
04/23/2013US8425182 Radial turbine
04/23/2013US8425179 Hesting power turbine device
04/23/2013US8424305 Turbo compressor system for an internal combustion engine comprising a compressor of radial type and provided with an impeller with backswept blades
04/23/2013CA2639080C Gas turbine rotor assembly methods
04/23/2013CA2622017C Vane assembly with improved vane roots
04/18/2013WO2013054798A1 Ceramic matrix composite member and method for producing same
04/18/2013WO2013054049A1 Turbomachine centre blade comprising a curved portion
04/18/2013WO2013054043A1 Cooling for the retaining dovetail of a turbomachine blade
04/18/2013WO2013053582A1 Method for repairing surface damage to a turbomachine component
04/18/2013WO2013053581A1 Method for applying a wear protection layer to a continuous flow machine component
04/18/2013US20130094971 Hot gas path component for turbine system
04/18/2013US20130094969 System for sealing a shaft
04/18/2013US20130094968 Adaptor assembly for coupling turbine blades to rotor disks
04/18/2013US20130094958 System and method for controlling flow through a rotor
04/18/2013US20130094949 Power recovery device of liquid processing apparatus
04/18/2013US20130091861 Turbine
04/18/2013CA2850901A1 Turbomachine centre blade comprising a curved portion
04/17/2013EP2581564A2 A Control System and Methods for Controlling the Operation of Power Generation Systems
04/17/2013EP2581562A2 System and Method for Controlling Flow through a Rotor
04/17/2013EP2581559A2 Adaptor assembly for coupling turbine blades to rotor disks
04/17/2013EP2581558A1 Bucket assembly for turbine system and corresponding turbine system
04/17/2013EP2581557A2 Hot gas path component for turbine system
04/17/2013EP2581556A2 Variable vanes with non uniform lean
04/17/2013EP2581555A1 Turbomachine Component having a Flow Contour Feature
04/17/2013EP2581554A2 System for cooling fluid flow within an engine
04/17/2013EP2581553A1 Method and device for dynamically measuring the imbalance of the rotor of a turbocharger core assembly
04/17/2013EP2581468A1 Method for applying an anti-wear protective coating to a flow engine component
04/17/2013EP2581164A1 Method for repairing surface damage to a flow engine component
04/17/2013EP2580432A1 Turbine blade seal assembly
04/17/2013EP2580431A2 Component wall having diffusion sections for cooling in a turbine engine
04/17/2013EP2580430A1 Film cooled component wall in a turbine engine
04/17/2013EP2580429A1 Blade for a turbo machine
04/17/2013EP2580428A1 Cooling fluid metering system for a turbine blade
04/17/2013CN103052807A Fan rotor blade and fan
04/17/2013CN103052765A Turbine blade and gas turbine
04/17/2013CN103052764A Coupling for rotor balancing
04/17/2013CN103046970A Bucket assembly for turbine system and corresponding turbine system
04/17/2013CN103046968A Adaptor assembly for coupling turbine blades to rotor disks
04/17/2013CN103046967A Turbine air cooling blade
04/17/2013CN103046966A System and method for controlling flow through a rotor
04/17/2013CN103046965A Turbomachine component having a flow contour feature
04/17/2013CN103046964A Active temperature gradient control stress based aero-engine turbine disk
04/17/2013CN102187013B Thermal barrier coating material, thermal barrier coating, turbine member, and gas turbine
04/17/2013CN101779000B Rotor for an axial flow turbomachine
04/16/2013US8420238 Use of a tungsten bronze structured material and turbine component with a thermal barrier coating
04/16/2013US8419489 Propeller unit for marine vessel propulsion device and marine vessel propulsion device including the same
04/16/2013US8419374 Gas turbine engine composite blade
04/16/2013US8419372 Airfoil having reduced wake
04/16/2013US8419366 Blade
04/16/2013US8419365 Member having internal cooling passage
04/16/2013CA2684779C Turbine blade with pressure side winglets
04/16/2013CA2672837C Rotor disc and method of balancing
04/16/2013CA2565011C Boundary layer suction arrangement
04/16/2013CA2505578C Methods and apparatus for sensing parameters of air flows
04/11/2013WO2013051942A1 A bucket connection for a turbine runner
04/11/2013WO2013051818A1 Axial turbine
04/11/2013WO2013050724A1 One-piece blisk comprising blades having a suitable root profile
04/11/2013US20130089434 Methods and systems for use in regulating a temperature of components
04/11/2013US20130089432 Shaft assembly for a gas turbine engine
04/11/2013US20130089431 Airfoil for turbine system
04/11/2013US20130089430 Turbomachine component having a flow contour feature
04/11/2013US20130089429 Turbine engine blade made of composite material, and a method of fabricating it
04/11/2013US20130089428 Method for producing a metal reinforcement for a turbomachine blade
04/11/2013US20130089427 Method for Welding Metallic Blades
04/11/2013US20130089424 Blade row for a turbomachine
04/11/2013US20130089412 Turbomachine rotor having patterned coating
04/11/2013US20130086805 Rotor disc and method of balancing
04/11/2013DE102012109479A1 Turbomaschinenrotor mit gemusterter Beschichtung Turbomachinery rotor having a patterned coating
04/11/2013DE102011084153A1 Safety device, useful for securing a shovel element in a groove of a running disc of a compressor or a turbine, comprises first and second fuse elements, which are inserted between the groove and a blade root and locked together
04/11/2013DE102011084125A1 Blade segment for turbomachine e.g. gas turbine for aircraft engine, has upper shroud which interconnects blades to each other, and lower shroud is divided into several portions which are firmly connected to the blades
04/10/2013EP2578810A1 Seal structure, turbine machine equipped with same, and power plant equipped with said turbine machine
04/10/2013EP2578807A2 Airfoil for turbine system
04/10/2013EP2578806A2 Tip shroud assembly with contoured seal rail fillet
04/10/2013EP2578805A1 Gas turbine engine airfoil with tip recesses
04/10/2013EP2578804A1 Light weight abradable air seal, corresponding gas turbine engine and process of manufacturing
04/10/2013EP2578803A2 Methods and systems for use in regulating a temperature of components
04/10/2013EP2578802A1 Vibration damping blade for fluid
04/10/2013EP2578801A1 Shroud for a turbo engine blade
04/10/2013EP2578720A2 Repair methods for cooled components
04/10/2013EP2578556A2 Method and ceramic component
04/10/2013EP2578553A2 A CMC Component, Power Generation System and Method of Forming a CMC Component
04/10/2013EP2577068A1 Vortex generators for generating vortices upstream of a cascade of compressor blades
04/10/2013EP2576988A1 Measuring the damage to a turbine-blade thermal barrier
04/10/2013EP2576987A1 Blade of a turbomachine, having passive boundary layer control
04/10/2013EP2576853A1 Alloy, protective layer and component
04/10/2013EP2576112A1 Method for machining cavities in a turbomachine turbine disc, turbomachine turbine and milling machine
04/10/2013CN202866901U 712.5-millimeter last stage moving blade used for 60 hertz (Hz) combined cycle turbine
04/10/2013CN103038455A Stator angular sector used for turbine engine compressor and turbine engine stator, and turbine engine including such a sector
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