Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
07/2014
07/16/2014EP2753799A1 Rotor seal wire groove repair
07/16/2014EP2753798A1 Assembly consisting of a turbine nozzle or a compressor stator vane made of cmc for a turbine engine and an abradable support ring, and turbine or compressor including such an assembly
07/16/2014EP2753729A1 Production method for a coating system
07/16/2014EP2753595A1 Method for forming a smooth glaze-like coating on a substrate made of a ceramic matrix composite material containing sic, and part made of a ceramic matrix composite material provided with such a coating
07/16/2014EP2753466A2 Method for manufacturing a sector of a turbine nozzle or compressor stator vane made of a composite material for a turbine engine, and turbine or compressor including a nozzle or stator vane consisting of said sectors
07/16/2014EP2753451A1 Isothermal structural repair of superalloy components including turbine blades
07/16/2014EP2753450A1 Splice insert repair for superalloy turbine blades
07/16/2014EP2753449A2 Ni-ti-cr near ternary eutectic alloy for gas turbine component repair
07/16/2014CN203717129U 一种叶轮发动机用叶轮 One kind of engine impeller impeller
07/16/2014CN203717045U 一种工业汽轮机末级动叶片 The final stage of an industrial steam turbine rotor blades
07/16/2014CN203717044U 大型汽轮发电机转子用异型截面接头铜管 Large Steam Turbine Generator Rotor shaped cross-section with brass fittings
07/16/2014CN203717043U 涡轮机中用于高压降的自适应级以及涡轮机 Pressure drop for the turbine stage and the turbine adaptive
07/16/2014CN103930652A 一种用于涡轮发动机的转子轮 A rotor for a turbine engine
07/16/2014CN103925010A 小型汽油机涡轮增压器涡轮转子 Small gasoline engine turbocharger turbine rotor
07/16/2014CN102414331B 具有多活性元素的镍基γ/γ'超合金和所述超合金在复杂材料体系中的用途 With multiple active elements nickel base γ / γ 'super alloys and super alloys in the complex material systems in use
07/16/2014CN102378850B 具有密封盘的轴流式涡轮机转子 A sealing disc axial turbine rotor
07/16/2014CN102257245B 具有用于轴向地保持叶片的系统的涡轮机叶轮 For axially holding the blade having a system turbine wheel
07/16/2014CN102137736B 涡轮机叶片盘的抛光方法以及抛光装置 Polishing method of the turbine blade and disk polishing apparatus
07/15/2014US8777583 Turbine airfoil components containing ceramic-based materials and processes therefor
07/15/2014US8777582 Components containing ceramic-based materials and coatings therefor
07/15/2014US8777577 Hybrid fan blade and method for its manufacture
07/15/2014US8777576 Metallic fan blade platform
07/15/2014US8777572 Rotor blade
07/15/2014US8777571 Turbine airfoil with curved diffusion film cooling slot
07/15/2014US8777570 Turbine vane with film cooling slots
07/15/2014US8777569 Turbine vane with impingement cooling insert
07/15/2014US8777568 Apparatus and methods for cooling platform regions of turbine rotor blades
07/15/2014US8777567 Turbine blades, turbine assemblies, and methods of manufacturing turbine blades
07/15/2014US8777554 Intermediate fan stage
07/15/2014CA2714740C Radial balancing clip weight for rotor assembly
07/15/2014CA2704595C Anti-vortex device for a gas turbine engine compressor
07/15/2014CA2571145C Turbine blade retaining apparatus
07/15/2014CA2562710C Apparatus and method of balancing a shaft
07/15/2014CA2561474C Bi-layer tip cap
07/10/2014WO2014106598A1 Blade for a turbomachine
07/10/2014WO2014106421A1 Pneumatic hydraulic potential circulating power generation system
07/10/2014WO2014070279A3 Endwall contouring
07/10/2014WO2014058505A3 Threaded full ring inner air-seal
07/10/2014US20140193664 Recoating process and recoated turbine blade
07/10/2014US20140193274 Fuel-cooled bladed rotor of a gas turbine engine
07/10/2014US20140193273 Interior configuration for turbine rotor blade
07/10/2014US20140193270 Ceramic composite matrix material bonded assembly and processes thereof
07/10/2014US20140193268 Method of formation of impeller with shape defined by plurality of lines and such impeller
07/10/2014US20140193267 DMZ Fracture Boundary Limit
07/10/2014US20140193249 Electrical conductor paths
07/10/2014US20140190181 Rotor cover plate
07/10/2014US20140190011 Method of Calculating Unsteady Force Acting on Rotor Blade or Stator Blade, Method of Designing Turbine and Method of Manufacturing Turbine
07/10/2014DE102014100087A1 Innenaufbau einer Turbinenlaufschaufel Internal structure of a turbine blade
07/10/2014DE102005025086B4 Anordnung zum Feinauswuchten des Rotors eines Gasturbinentriebwerks Arrangement for precision balancing of the rotor of a gas turbine engine
07/09/2014EP2752557A2 Platformless turbine blade
07/09/2014EP2752556A1 Rotor blade support structure
07/09/2014EP2752555A1 Turbine blade, and gas turbine including same
07/09/2014EP2752554A1 Blade for a turbomachine
07/09/2014EP2752553A1 Rotor device, turbine rotor device, and gas turbine and turbine engine having same
07/09/2014EP2751394A1 Modified interface around a hole
07/09/2014EP2751306A1 Localized cleaning process and apparatus therefor
07/09/2014EP2750824A1 Projection resistance welding of superalloys
07/09/2014CN203697601U 一种含有桩钉结构增强体的热障涂层 Thermal barrier coatings containing pegs reinforced body structure
07/09/2014CN103917502A 高温热障涂层 High temperature thermal barrier coating
07/09/2014CN103917445A 用于改造风力涡轮机叶片上的涡流发生器的方法 Methods for the transformation of vortex generators on wind turbine blades of
07/09/2014CN103917325A 超级合金的凸起电阻焊接 Projection resistance welding superalloys
07/09/2014CN103917320A 利用凸出电阻钎焊连接或修复超级合金结构的方法:相应的超级合金部件 Methods resistance brazing alloy structural connections or repair using super bulge: the corresponding super alloy parts
07/09/2014CN103912317A 生物质能双涡轮动力发电装置 Biomass twin turbine power generation device
07/09/2014CN103912315A 一种航空发动机转子结构动力学的设计方法 A design method for aeroengine structural dynamics of the rotor
07/09/2014CN103909380A 电动涡轮增压器的转子装配方法及通过该方法装配的转子 Electric turbocharger rotor assembling method and assembling method by the rotor
07/09/2014CN102330572B 涡轮机的转子 Turbine rotor
07/09/2014CN102197193B 装有冷却流体流量调整装置的涡轮叶片 Turbine blade fitted with a cooling fluid flow rate adjusting device
07/09/2014CN101960098B 用于叶片的液滴冲击保护层 Droplet impact protection layer for the blade
07/08/2014US8771786 Method for repair of a component of a turbomachine and a component repaired according to this method
07/08/2014US8770952 Centrifugal pump
07/08/2014US8770949 Ceiling fan
07/08/2014US8770944 Turbine airfoil component and method for making
07/08/2014US8770943 Axial flow fan
07/08/2014US8770942 Blade and laminated protective sheet for the blade
07/08/2014US8770939 Turbine rotor blade assembly and steam turbine
07/08/2014US8770938 Rotor for an axial-throughflow turbomachine and moving blade for such a rotor
07/08/2014US8770936 Turbine blade with near wall cooling channels
07/08/2014US8770934 Teeter mechanism for a multiple-bladed wind turbine
07/08/2014US8770927 Abrasive cutter formed by thermal spray and post treatment
07/08/2014US8770926 Rough dense ceramic sealing surface in turbomachines
07/08/2014US8770920 Gas turbine airfoil with shaped trailing edge coolant ejection holes
07/08/2014US8770919 Turbine disk and gas turbine
07/08/2014US8769817 Seal assembly retention method
07/08/2014CA2600502C Eddy current heating for reducing transient thermal stresses in a rotor of a gas turbine engine
07/08/2014CA2571652C Methods and apparatus for gas turbine engines
07/08/2014CA2548133C Counterrotating turbofan engine
07/03/2014WO2014105701A2 Non-integral fan blade platform
07/03/2014WO2014105593A1 Compressor rotor for gas turbine engine with deep blade groove
07/03/2014WO2014105547A1 Gas turbine engine component having suction side cutback opening
07/03/2014WO2014105533A1 Shrouded turbine blade with cut corner
07/03/2014WO2014105524A1 Inter-module flow discourager
07/03/2014WO2014105432A1 Airfoil with variable profile responsive to thermal conditions
07/03/2014WO2014105393A1 Non-line of sight electro discharge machined part
07/03/2014WO2014105392A1 Gas turbine engine serpentine cooling passage with chevrons
07/03/2014WO2014105245A1 Integral instrumentation in additively manufactured components of gas turbine engines
07/03/2014WO2014105113A1 Gas turbine engine component having vascular engineered lattice structure
07/03/2014WO2014105108A1 Gas turbine engine component having vascular engineered lattice structure
07/03/2014WO2014105104A1 Blade underroot spacer with hook removal
07/03/2014WO2014105103A1 Platform with curved edges
07/03/2014WO2014105102A1 Platform with curved edges adjacent suction side of airfoil
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