Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
02/2013
02/28/2013US20130052037 Airfoil with nonlinear cooling passage
02/28/2013US20130052036 Pin-fin array
02/28/2013US20130052035 Axially cooled airfoil
02/28/2013US20130052032 Vibration damper comprising a strip and jackets between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel
02/28/2013US20130052031 Propeller blades having icephobic coating
02/28/2013US20130052030 Ceramic matrix composite vane structure with overwrap for a gas turbine engine
02/28/2013US20130052029 Hollow core airfoil stiffener rib
02/28/2013US20130052027 Hydrofoil with features to generate cavitation
02/28/2013US20130052026 Axial retention system for a bladed rotor with multiple blade types
02/28/2013US20130052025 Replaceable staking insert assembly and method
02/28/2013US20130052024 Turbine Nozzle Vane Retention System
02/28/2013US20130052022 Rotor for a compressor of a gas turbine
02/28/2013US20130052021 Rotor asymmetry
02/28/2013US20130052020 Coupled blade platforms and methods of sealing
02/28/2013US20130052019 Rotor assembly for a turbomachine
02/28/2013US20130052012 Metallic fan blade platform
02/28/2013US20130052009 Bucket assembly treating apparatus and method for treating bucket assembly
02/28/2013US20130052008 Gas turbine engine airfoil baffle
02/28/2013US20130052001 Centrifugal blower
02/28/2013US20130051979 Turbine shroud segment with integrated impingement plate
02/28/2013US20130051974 Gas turbine engines and methods for cooling components thereof with mid-impeller bleed cooling air
02/28/2013US20130051972 Blade outer air seal with multi impingement plate assembly
02/28/2013CA2846053A1 Blade arrangement
02/28/2013CA2844375A1 Tool for holding a turbine-engine part, including a means for attaching and immobilising the part and an element to be attached to said part by brazing or welding
02/28/2013CA2787675A1 Automated wet masking for diffusion coatings
02/27/2013EP2562427A2 A rotor for a compressor of a gas turbine
02/27/2013EP2562360A2 Ceramic matrix composite vane structure with overwrap for a gas turbine engine
02/27/2013EP2562357A1 Replaceable staking insert assembly and corresponding method
02/27/2013EP2562356A1 Blade assembly
02/27/2013EP2562355A2 Coupled blade platforms and methods of sealing
02/27/2013EP2562354A2 Cooling insert for a gas turbine engine airfoil
02/27/2013EP2562353A2 Axially cooled airfoil
02/27/2013EP2562352A2 Bucket assembly treating apparatus and method for treating bucket assembly
02/27/2013EP2562281A1 Ni-base alloy large member, Ni-base alloy welded structure made of same, and method for manufacturing structure thereof
02/27/2013EP2562277A1 A nickel alloy
02/27/2013EP2561187A1 Exhaust gas diffuser of a gas turbine
02/27/2013EP2561185A1 Discretely defined porous wall structure for transpirational cooling
02/27/2013CN202756028U Ultra-supercritical 1300-millon-watt (MW) steam turbine
02/27/2013CN202756026U Locking mechanism of turbine blades
02/27/2013CN202756025U High-middle-low pressing cylinder blade of HE type combined cycle steam turbine
02/27/2013CN202756024U Steam turbine
02/27/2013CN102947598A Compressor and turbomachine with optimized efficiency
02/27/2013CN102947596A Method for producing a metal reinforcement for a turbomachine blade
02/27/2013CN102947548A Light weight shroud fin for a rotor blade
02/27/2013CN102947547A Balance correction weight providing constant mass
02/27/2013CN102947546A 蒸汽涡轮机 Steam turbine
02/27/2013CN102943695A Balancing method for bacterial type looped blade roots and blades
02/27/2013CN102943694A Clapboard-type labyrinth structure for moving blade tip
02/27/2013CN102943693A Efficient cooling turbine movable vane of gas turbine with low-heat and medium-heat values
02/27/2013CN102345122B Multipurpose low-conductivity ceramic/noble metal lamellar composite thermal barrier coating
02/27/2013CN101627182B Cooled turbine blade for a gas turbine and use of such a turbine blade
02/27/2013CN101460708B Coated turbine component and method of coating a turbine component
02/26/2013US8382438 Blade of a turbomachine with enlarged peripheral profile depth
02/26/2013US8382436 Non-integral turbine blade platforms and systems
02/26/2013US8382433 Method for producing a blade by casting and blade for a gas turbine
02/26/2013US8382432 Cooled turbine rim seal
02/26/2013US8382431 Turbine rotor blade
02/26/2013US8381533 Direct transfer axial tangential onboard injector system (TOBI) with self-supporting seal plate
02/26/2013CA2633323C Third stage turbine airfoil
02/22/2013CA2786394A1 Method for milling a blank in the production of a turbine blade
02/22/2013CA2786362A1 Metallic fan blade platform
02/21/2013WO2013025384A1 Rotor seal wire groove repair
02/21/2013WO2013023928A1 Internally coolable component for a gas turbine with at least one cooling duct
02/21/2013WO2013023507A1 Rotor device, turbine rotor device, and gas turbine and turbine engine having same
02/21/2013WO2012140039A3 Wind turbine blade comprising circumferential retaining means in root regions
02/21/2013US20130045120 Segmented fan assembly
02/21/2013US20130045111 Turbine blade cooling system with bifurcated mid-chord cooling chamber
02/21/2013US20130045106 Angled trench diffuser
02/21/2013US20130045105 Wind turbine blade and method of protecting the same
02/21/2013US20130045096 Removable mask for a turbomachine blade or distributor sector platform
02/21/2013US20130045083 Turbine rotor disk inlet orifice for a turbine engine
02/21/2013DE102011111011A1 Adjustable shovel element of a gas turbine of an aircraft engine, comprises adjusting device for changing shape of adjustable shovel element, which is constructed by a generative manufacturing process
02/21/2013DE10124393B4 Hitzebeständiger Stahl, Verfahren zur thermischen Behandlung von hitzebeständigem Stahl, und Kompenten aus hitzebeständigem Stahl A heat-resistant steel, process for the thermal treatment of heat-resistant steel, heat-resistant steel and Kompenten from
02/21/2013CA2844646A1 Rotor seal wire groove repair
02/20/2013EP2559856A2 Components with cooling channels and methods of manufacture
02/20/2013EP2559855A2 Turbine blade with film cooling hole diffusers and method of its manufacture
02/20/2013EP2559854A1 Internally cooled component for a gas turbine with at least one cooling channel
02/20/2013EP2559853A2 Gasturbine engine airfoil seal
02/20/2013EP2559852A1 Exhaust diffuser and method for manufacturing an exhaust diffuser
02/20/2013EP2559851A1 Exhaust diffuser and method for manufacturing an exhaust diffuser
02/20/2013EP2559850A1 Exhaust diffuser and method for manufacturing an exhaust diffuser
02/20/2013EP2559849A2 Gas turbine engine seal assembly having flow-through tube
02/20/2013EP2559848A2 Method for Regenerating Oxide Coatings on Gas Turbine Components by Addition of Oxygen into SEGR System
02/20/2013EP2559787A1 Method for producing a component for high thermal loads, a component that can be created using the method and an aircraft engine with the component
02/20/2013EP2559784A2 Deposition apparatus and methods
02/20/2013EP2558687A1 Rotor blade assembly
02/20/2013EP2558686A1 Blade or vane for a turbomachine
02/20/2013EP2558685A2 Guide blade of a turbomachine
02/20/2013EP2558611A1 Process for internally coating functional layers with a through-hardened material
02/20/2013EP2558245A1 Germanium-containing solder, a component with a solder and a process for soldering
02/20/2013EP2558244A2 Solder alloy, soldering method and component
02/20/2013EP2558243A2 Solder alloy, soldering method and component
02/20/2013CN202745949U Variable-speed turbine low-pressure vane level group with steam exhaust area of 2.8m<2>
02/20/2013CN202745948U Cooling structure of heavy duty gas turbine high-temperature turbine working blade
02/20/2013CN202745947U Split type turbine for valve lifting machine
02/20/2013CN101482136B Axial maintenance system
02/20/2013CN101333940B Rotor wheel for a jet engine, and jet engine comprising same
02/19/2013US8376709 Impeller of a suction-enforced type and fan-motor having the same
02/19/2013US8376706 Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
02/19/2013US8376705 Turbine endwall with grooved recess cavity
1 ... 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 ... 330