Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
06/2014
06/10/2014US8747733 Precipitation hardenable martensitic stainless steel and steam turbine blade using the same
06/10/2014US8747061 Steam turbine
06/10/2014CA2632716C Brazed joint between a metal part and a ceramic part
06/10/2014CA2629226C Bimaterial turbine blade damper
06/10/2014CA2525003C Shrouded turbine blades with locally increased contact faces
06/05/2014WO2014085464A1 Turbine blade angel wing with pumping features
06/05/2014WO2014085366A1 Gas turbine engine turbine nozzle impingement cover
06/05/2014WO2014085020A1 Trailing edge and tip cooling
06/05/2014WO2014083325A1 Turbocharger impeller screwed onto shaft with arrangement for accommodating thermal dilatation
06/05/2014WO2014083290A1 Turbomachine or test engine rotor
06/05/2014WO2014083275A1 Method for friction welding a blade onto a turbine engine rotor disc; corresponding integral blade disc
06/05/2014WO2014082947A1 Method and device for repairing an aircraft and/or gas turbine component
06/05/2014WO2014042724A3 Turbine compressor blade tip resistant to metal transfer
06/05/2014US20140154096 Turbine blade airfoils including showerhead film cooling systems, and methods for forming an improved showerhead film cooled airfoil of a turbine blade
06/05/2014US20140154093 Method of heat treating a superalloy article and article made thereby
06/05/2014US20140154092 Wind turbine blade with transition region
06/05/2014US20140154088 Method for manufacturing a metallic component by additive laser manufacturing
06/05/2014US20140154087 Gas turbine engine airfoil
06/05/2014US20140154086 Front fan retention in dual internal fan alternator
06/05/2014US20140154085 Gas turbine and guide blade for a housing of a gas turbine
06/05/2014US20140154084 Non-uniform blade distribution for rotary wing aircraft
06/05/2014US20140154082 Pre-sintered preform repair of turbine blades
06/05/2014US20140154081 Tear-drop shaped part-span shroud
06/05/2014US20140154079 Fillet for use with a turbine rotor blade tip shroud
06/05/2014US20140154078 Impeller with sealing portion
06/05/2014US20140154073 Apparatus having engineered surface feature and method to reduce wear and friction between cmc-to-metal attachment and interface
06/05/2014US20140154069 Turbine wheel, a turbine and use thereof
06/05/2014US20140154068 Endwall Controuring
06/05/2014US20140154063 Airfoil and a method for cooling an airfoil platform
06/05/2014US20140150455 Coated article
06/05/2014US20140150454 Turbine blade apparatus
06/05/2014DE102012222205A1 Running wheel for turbomachine e.g. supercharger, has cavity that includes axial recess which is formed on end face of base, and disc element that is attached with cavity on end face of base
06/05/2014DE102012206126B4 Laufschaufel sowie Strömungsmaschine Blade and flow machine
06/05/2014DE102012023617A1 Schaufelblatt für eine Wasserturbine Airfoil for a water turbine
06/04/2014EP2738353A2 System for damping vibrations in a turbine
06/04/2014EP2738352A1 Fillet for use with a turbine rotor blade tip shroud
06/04/2014EP2738351A1 Rotor blade with tear-drop shaped part-span shroud
06/04/2014EP2738350A2 Turbine blade airfoils including showerhead film cooling systems, and methods for forming an improved showerhead film cooled airfoil of a turbine blade
06/04/2014EP2737179A1 Centrifugal impeller and turbomachine
06/04/2014EP2737178A1 Method for producing, repairing and/or exchanging a housing, in particular an engine housing, and a corresponding housing
06/04/2014EP2737103A1 Method for applying a wear protection layer to a continuous flow machine component
06/04/2014CN203626892U 高炉煤气余压透平装置的悬臂式转子 Blast furnace gas pressure turbine rotor cantilever device
06/04/2014CN103842642A A bucket connection for a turbine runner
06/04/2014CN103113112B Preparation method of metal toughened ceramic-based composite material turbine blade
06/04/2014CN102733866B Compact high-load power turbine generator
06/04/2014CN102691527B Groove structure on back of open centripetal turbine blade
06/04/2014CN102232020B Composite material turbine engine vane, and method for manufacturing same
06/03/2014US8741077 Homogeneous titanium tungsten alloys produced by powder metal technology
06/03/2014US8740573 Adaptor assembly for coupling turbine blades to rotor disks
06/03/2014US8740572 Wear-resistant and oxidation-resistant turbine blade
06/03/2014US8740571 Turbine bucket for use in gas turbine engines and methods for fabricating the same
06/03/2014US8740570 Turbine bucket airfoil profile
06/03/2014US8740568 Turbomachine fan rotor
06/03/2014US8740567 Reverse cavity blade for a gas turbine engine
06/03/2014US8740561 Jacket impeller with functional graded material and method
06/03/2014US8740554 Cover plate with interstage seal for a gas turbine engine
06/03/2014US8740546 Guide vane for a condensation steam turbine and associated condensation steam turbine
06/03/2014US8739508 Shock cancellation mechanism for the control of unsteady interaction in contra-rotating high- and low-pressure turbines
06/03/2014CA2735493C Turbine blade retention device
06/03/2014CA2619927C Turboprop engine with adjustable pitch propeller
06/03/2014CA2535140C Airfoil locator rib and method of positioning an insert in an airfoil
05/2014
05/30/2014WO2014081794A1 Method of extending life of rotating parts
05/30/2014WO2014081790A1 Gas turbine engine compressor rotor assembly and balancing system
05/30/2014WO2014081603A1 Compressor wheel of a radial compressor of an exhaust-gas turbocharger
05/30/2014WO2014081517A1 Turbine shroud mounting and sealing arrangement
05/30/2014WO2014081496A1 Apparatus and method to reduce wear and friction between cmc-to-metal attachment and interface
05/30/2014WO2014081490A2 Film cooling channel array with multiple metering portions
05/30/2014WO2014081380A1 A multifunctional erosion protection strip
05/30/2014WO2014081356A1 An airframe leading edge
05/30/2014WO2014081355A1 An erosion protection strip for a leading edge of an airfoil article
05/30/2014WO2014080087A1 Rotor axle of a high speed permanent magnet machine
05/30/2014WO2014042720A3 Gas turbine engine turbine blade airfoil profile
05/30/2014WO2014031195A3 Gas turbine engine fan blade tip treatment
05/30/2014CA2834022A1 Method and system for integrating gas turbine trim balancing system into electronic engine controls
05/29/2014US20140147620 Infusible unidirectional fabric
05/29/2014US20140147287 Trailing edge and tip cooling
05/29/2014US20140147286 Turbomachine rotor disk
05/29/2014US20140147285 Fixture for an airfoil shroud and method for modifying an airfoil shroud
05/29/2014US20140147284 Method for modifying an airfoil shroud
05/29/2014US20140147283 Method for modifying a airfoil shroud and airfoil
05/29/2014US20140147276 System for damping vibrations in a turbine
05/29/2014US20140147250 Turbine blade angel wing with pumping features
05/29/2014US20140147249 Gas turbine engine rotor drain feature
05/29/2014US20140144157 Dovetail attachment seal for a turbomachine
05/28/2014EP2735705A2 Fixture for an airfoil shroud and method for modifying an airfoil shroud
05/28/2014EP2735704A2 Method for modifying an airfoil shroud and airfoil
05/28/2014EP2735399A1 Determining the direction of travel in the welding of directionally solidified material
05/28/2014DE102013109844A1 Verfahren zur Umfangsausrichtung einer Turbine durch Umgestalten der abströmseitigen Schaufelblätter der Turbine Method for circumferential alignment of a turbine by reshaping the downstream blades of the turbine
05/28/2014DE102012022260A1 Verfahren zur Herstellung einer Welle eines Gasturbinentriebwerks, insbesondere einer Radialwelle oder einer zur Maschinenachse in einem Winkel angeordneten Welle A method of manufacturing a shaft of a gas turbine engine, in particular a rotary shaft or arranged at an angle to the machine axis shaft
05/28/2014DE102012022198A1 Welle eines Gasturbinentriebwerks, insbesondere einer Radialwelle oder einer zur Maschinenachse in einem Winkel angeordneten Welle Shaft of a gas turbine engine, particularly a radial shaft or arranged to the machine axis at an angle shaft
05/28/2014CN203614428U 一种具有螺旋叶片的轴流流体压力机及涡轮 Having a spiral blade and the turbine axial fluid presses
05/28/2014CN103827056A 在由包含SiC的陶瓷基质复合材料制成的基材上形成平滑釉质涂层的方法,和由设置有所述涂层的陶瓷基质复合材料制成的部件 Method on a substrate by a ceramic matrix comprising SiC composite material for forming a smooth coating of enamel, and the parts provided with the coating layer from a ceramic matrix composite material
05/28/2014CN103826799A 具有改善的表面修饰的铝化钛制品及其制备方法 With improved surface modification of titanium aluminide products and its preparation method
05/28/2014CN103821567A 一种航空发动机高压转子结构动力学设计方法 Aeronautical engine high pressure rotor structural dynamics design method
05/28/2014CN102027242B 具有可变椭圆连接部的压缩机叶轮叶片 A compressor impeller blades connected to the variable portion of the ellipse
05/28/2014CN101769170B 涡轮叶片冷却回路 Turbine blade cooling circuit
05/28/2014CA2833986A1 Low hub-to-tip ratio fan for a turbofan gas turbine engine
05/27/2014US8734605 Manufacturing a composite component
05/27/2014US8734116 Turbine bucket airfoil profile
05/27/2014US8734115 Optimized aerodynamic profile for a turbine blade, in particular for a rotary wheel of the third stage of a turbine
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