Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
08/2014
08/14/2014DE102005017148B4 Drehdichtungsanordnung für Kühlkreisläufe von Turbinenschaufeln Rotary seal assembly for cooling circuits of turbine blades
08/13/2014EP2765275A1 Method for calculating unsteady force acting on rotor blade or stator blade, turbine design technique and turbine manufacturing method
08/13/2014EP2764951A1 Manufacture of hollow aerofoil
08/13/2014EP2764949A2 Material removal method
08/13/2014EP2764947A1 Joint connection preform, method of joining and composite workpiece of components containing harding gamma prime phase
08/13/2014EP2764936A2 Turbomachine rotor blade miilling machine system and method of field repairing a turbomachine rotor blade
08/13/2014EP2764213A2 Gas turbine with optimized airfoil element angles
08/13/2014EP2764212A1 One-piece blisk comprising blades having a suitable root profile
08/13/2014CN203769861U 涡轮增压器用涡轮 A turbocharger turbine
08/13/2014CN203769860U 增压器的变截面机构叶片 Tapered body blade turbocharger
08/13/2014CN203769859U 一种叶轮 One kind of impeller
08/13/2014CN203769645U 线投影叶片制动级定转子组合件 Line projection level brake rotor blade assembly
08/13/2014CN103982462A 一种叶片尾缘的波形射流方法 Waveform jet method trailing edge of the blade
08/13/2014CN103982242A 轮盘圆弧端齿及其轮盘以及带有该轮盘的燃气涡轮发动机 Roulette and Roulette arc end teeth and a gas turbine engine with the roulette
08/13/2014CN102337931B 转子、使用该转子的膨胀机、发动机及膨胀机系统 A rotor, the rotor using the expander, and the expander system of the engine
08/12/2014US8802225 Article having vitreous monocoating
08/12/2014US8802199 Method for microstructure control of ceramic thermal spray coating
08/12/2014US8801405 Centrifugal pump
08/12/2014US8801388 Bi-cast turbine rotor disks and methods of forming same
08/12/2014US8801387 Wind turbine blade and wind turbine generator including the same
08/12/2014US8801385 Vibration damper device for turbomachine blade attachments, associated turbomachine and associated engines
08/12/2014US8801382 Rotor for turbomachinery
08/12/2014US8801381 Turbine blade
08/12/2014US8801379 Wheel and replaceable nose piece
08/12/2014US8801377 Turbine blade with tip cooling and sealing
08/12/2014US8801371 Gas turbine
08/12/2014US8801367 Hollow fan blade channel configuration to reduce stress
08/12/2014US8801366 Stator blade for a gas turbine and gas turbine having same
08/12/2014US8800145 Refurbishing method and system for a main rotor blade spar
08/12/2014CA2571903C Composite blading member and method for making
08/12/2014CA2548361C Integrated counterrotating turbofan
08/07/2014WO2014121060A1 Localized repair of superalloy component
08/07/2014WO2014120736A1 Method of laser re-melt repair of superalloys using flux
08/07/2014WO2014120729A1 Laser microcladding using powdered flux and metal
08/07/2014WO2014120565A1 Bell mouth inlet for turbine blade
08/07/2014WO2014120511A1 Hybrid laser plus submerged arc or electroslag cladding of superalloys
08/07/2014WO2014120135A1 Double snapped cover plate for rotor disk
08/07/2014WO2014118358A1 Turbomachine rotor blade, turbomachine rotor disc, turbomachine rotor, and gas turbine engine with different root and slot contact face angles
08/07/2014WO2014117998A1 Gas turbine rotor blade and gas turbine rotor
08/07/2014WO2014078467A3 Turbine fan blades with sheath
08/07/2014WO2014048549A3 Rotor disk for determining the oscillation behaviour of rotor disk blades, test bench for determining the oscillating behaviour of rotor disk blades, and a method for determining the oscillating behaviour of rotor disk blades
08/07/2014US20140220378 Thermal barrier coating systems and processes therefor
08/07/2014US20140219818 Turbine Component Cooling Channel Mesh with Intersection Chambers
08/07/2014US20140219817 High pressure turbine blade cooling hole distribution
08/07/2014US20140219816 High pressure turbine blade cooling hole distribution
08/07/2014US20140219815 Multi-lobed cooling hole
08/07/2014US20140219813 Gas turbine engine serpentine cooling passage
08/07/2014US20140219811 Twisted gas turbine engine airfoil having a twisted rib
08/07/2014US20140219809 Casting core for twisted gas turbine engine airfoil having a twisted rib
08/07/2014US20140219808 Sheath with extended wings
08/07/2014US20140219807 Under-root spacer for gas turbine engine fan blade
08/07/2014US20140219806 Rotor blade support structure
08/07/2014US20140219803 Attaching the Blades of an Axial Turbocompressor to the Compressor Drum
08/07/2014US20140219794 Bore cavity thermal conditioning system
08/07/2014US20140219788 Impingement cooling of turbine blades or vanes
08/07/2014US20140219778 Gas turbine engine airfoil with vane platform cooling passage
08/07/2014US20140219776 Arrangement for extracting energy from flowing liquid
08/07/2014US20140215822 Method for producing a compressor blade
08/07/2014US20140215783 Production facility comprising a transport system for processing elongated products, in particular wind turbine blades, with elongated mould assemblies
08/06/2014EP2762681A1 Rotor drum of an axial turbomachine and corresponding turbomachine
08/06/2014EP2762680A1 Multilayer component and fabrication process
08/06/2014EP2762679A1 Gas Turbine Rotor Blade and Gas Turbine Rotor
08/06/2014EP2762678A1 Method for misaligning a rotor blade grid
08/06/2014EP2762677A2 Two-shaft gas turbine
08/06/2014EP2762676A1 Turbomachine rotor blade, turbomachine rotor disc, turbomachine rotor, and gas turbine engine with different root and slot contact face angles
08/06/2014EP2762262A1 Welding process with adjustable welding power depending on the thickness
08/06/2014EP2762257A1 Brazing process, braze arrangement, and brazed article
08/06/2014EP2761138A1 Method and apparatus for cooling gas turbine rotor blades
08/06/2014EP2761137A1 Blade of a row of rotor blades or stator blades for use in a turbomachine
08/06/2014EP2760737A1 Blade for a fan of a turbomachine, notably of the unducted fan type, corresponding fan and corresponding turbomachine
08/06/2014EP2760632A1 Titanium aluminide articles with improved surface finish and methods for their manufacture
08/06/2014EP2760621A1 Laser drilling through-bores without protection in the interior
08/06/2014EP2760615A1 Hold and cool process for superalloy joining
08/06/2014EP2760614A1 Remelting method and subsequent refilling and component
08/06/2014CN203756244U 生物质能发电的双涡轮动力装置 Twin-turbo power plant biomass power generation
08/06/2014CN203756239U 小型涡轮增压器的转子系统 Small turbocharger rotor system
08/06/2014CN103975129A 冲击冷却机构、涡轮翼以及燃烧器 Impingement cooling means, the turbine blade and the combustor
08/06/2014CN103975128A 具有最佳化翼片元件角度的燃气轮机 The gas turbine has the best angle of the flap element
08/06/2014CN103974824A 由复合材料制造并包括结合的平台的涡轮机叶片的制备方法 Made of composite material and a method comprising preparing a combination of a turbine blade platform
08/06/2014CN103974797A 背面保护焊接方法及利用该方法的焊接结构物 Back protective welding method and the use of the method for welded structures
08/06/2014CN103967718A 三维曲面翼型的设计方法 Three-dimensional surface of the airfoil design method
08/06/2014CN103967621A 具有微小斜肋-凹陷复合结构的冷却装置 With a slight slant ribs - the composite structure of the cooling apparatus recessed
08/06/2014CN103967590A 具有子午线划分涡轮壳体的轴向涡轮 Has a radial division of axial turbine the turbine housing
08/06/2014CN103967533A 一种涡轮发动机用涡轮 A turbine engine turbine
08/06/2014CN103967532A 多层构件和制造工艺 Multi-layered member and manufacturing processes
08/06/2014CN103967531A 用于流体机械的、薄膜冷却的涡轮叶片 For fluid machine, film cooled turbine blade
08/06/2014CN102301095B 涡轮机叶片系统 Turbine blade system
08/05/2014US8794926 Turbine blade with improved aerodynamic performance
08/05/2014US8794925 Root region of a blade for a gas turbine engine
08/05/2014US8794924 Rotating body
08/05/2014US8794923 Gas turbine engine rotor tie shaft arrangement
08/05/2014US8794921 Apparatus and methods for cooling platform regions of turbine rotor blades
08/05/2014US8794907 Multiple staged compressor with last stage airfoil cooling
08/05/2014US8794906 Turbine stator vane with endwall cooling
08/05/2014CA2791191C Gas turbine engine
08/04/2014CA2841344A1 Attaching the blades of an axial turbocompressor to the compressor drum
07/2014
07/31/2014WO2014116842A1 Structures and methods for forcing coupling of flow fields of adjacent bladed elements of turbomachines, and turbomachines incorporating the same
07/31/2014WO2014116475A1 Gas turbine engine component having contoured rib end
07/31/2014WO2014116326A2 Dmz fracture boundary limit
07/31/2014WO2014116216A1 Gas turbine engine component with angled aperture impingement
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