Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
09/2013
09/26/2013WO2012114058A8 A turbine wheel, a turbine and use thereof
09/26/2013US20130251939 Process for producing ceramic composite components
09/26/2013US20130251539 Trailing edge or tip flag antiflow separation
09/26/2013US20130251538 Trailing edge cooling
09/26/2013US20130251537 Titanium aluminide intermetallic compositions
09/26/2013US20130251536 Hybrid airfoil for a gas turbine engine
09/26/2013US20130251534 Turbine
09/26/2013US20130251532 Securing device for axially securing a blade root of a turbomachine blade
09/26/2013US20130251525 Lift Propulsion and Stabilizing System and Procedure For Vertical Take-Off and Landing Aircraft
09/26/2013US20130251520 Scalloped surface turbine stage
09/26/2013US20130247586 Blade Wedge Attachment
09/26/2013DE102012213227B3 Schaufelkranz für eine Turbomaschine Blade ring for a turbomachine
09/25/2013EP2642080A1 Turbomachine blade and corresponding operating method
09/25/2013EP2642077A1 Turbine rotor for a thermal electric power station
09/25/2013EP2642076A2 Connecting system for metal components and cmc components, a turbine blade retaining system and a rotating component retaining system
09/25/2013EP2642075A2 Turbine stage and corresponding turbine blade having a scalloped platform
09/25/2013EP2642074A1 Process of repairing a component, a repair tool for a component, and a component
09/25/2013EP2641993A2 A method of manufacturing a thermal barrier coated article
09/25/2013EP2641992A2 A thermal barrier coated article and a method of manufacturing a thermal barrier coated article
09/25/2013EP2640946A1 Thermal integration of thermoelectric device
09/25/2013EP2640935A1 Rotor blade arrangement for a turbo machine
09/25/2013CN203214109U Turbine blade tail edge cooling structure
09/25/2013CN203214108U Turbine blade front edge cooling structure
09/25/2013CN203214107U Turbine type air-magnetic engine
09/25/2013CN103328771A Method for disconnecting, by induction, a magnetic mechanical part adhered to a mechanical part
09/25/2013CN103328150A Method for producing a metal reinforcement
09/25/2013CN103321748A Vertical combustion gas turbine
09/25/2013CN103321687A Connecting system for metal components and cmc components, a turbine blade retaining system and a rotating component retaining system
09/25/2013CN103321686A Scalloped surface turbine stage
09/25/2013CN103321685A Through-hole connection method and connection structure of titanium aluminum turbine impeller and rotating shaft
09/25/2013CN103321684A Turbine rotor for a thermal electric power station
09/25/2013CN103317307A Bi-arc self-locking interference threaded connection method and structure for titanium aluminum turbine and spindle
09/25/2013CN102282276B Ni-based single crystal superalloy
09/25/2013CN101837482B Processing technology of steam turbine seven-fork blade root pin holes and special fixture
09/24/2013US8540490 Noise reduction in a turbomachine, and a related method thereof
09/24/2013US8540488 Turbine blade damping device with controlled loading
09/24/2013US8540486 Apparatus for cooling a bucket assembly
09/24/2013US8540481 Rotor blade assembly
09/24/2013US8540480 Aerofoil having a plurality cooling air flows
09/24/2013CA2714871C Method and apparatus for production of a cast component
09/24/2013CA2708940C Methods for repairing barrier coatings
09/23/2013CA2808804A1 Scalloped surface turbine stage
09/21/2013CA2809000A1 Dual-use of cooling air for turbine vane and method
09/19/2013WO2013138129A1 Gas turbine engine airfoil cooling circuit
09/19/2013WO2013138055A1 Apparatus and method for servicing turbomachinery components in-situ
09/19/2013WO2013138042A1 Advanced pass progression for build-up welding
09/19/2013WO2013138009A1 Improved cooling pedestal array
09/19/2013WO2013137964A2 Method and coating for protecting and repairing an airfoil surface
09/19/2013WO2013135319A1 Gas turbine arrangement alleviating stresses at turbine discs and corresponding gas turbine
09/19/2013US20130243606 Turbine blade tip cooling
09/19/2013US20130243604 Turbomachine blades or vanes having complementary even/odd geometry
09/19/2013US20130243603 Three-dimensionally woven composite blade wtih spanwise weft yarns
09/19/2013US20130243602 Blade ring segment having an annular space delimiting surface having a wavy height profile and a method for manufacturing same
09/19/2013US20130243601 Connecting system for metal components and cmc components, a turbine blade retaining system and a rotating component retaining system
09/19/2013US20130243596 Shark-bite tip shelf cooling configuration
09/19/2013US20130243591 Gas turbine engine airfoil cooling circuit
09/19/2013US20130243576 Gas turbine
09/19/2013US20130239586 Fan blade and method of manufacturing same
09/18/2013EP2639407A1 Gas turbine arrangement alleviating stresses at turbine discs and corresponding gas turbine
09/18/2013EP2639406A1 Turbomachine blade with improved stiffness to weight ratio
09/18/2013EP2639405A1 Turbine blade tip cooling
09/18/2013EP2639404A1 Exhaust diffuser for a turbine
09/18/2013EP2639403A2 Shaft Assembly for a Gas Turbine Engine
09/18/2013EP2638249A1 Method for optimising the profile of a blade made from composite material for a movable wheel of a turbomachine
09/18/2013EP2637863A1 Alloy, protective layer and component
09/18/2013CN103307021A Reverse engineering forming method of turbomachinery blade grid based on mixed material filling
09/18/2013CN103306892A Power fin
09/18/2013CN103306744A Cooling device for guide vane
09/18/2013CN103306743A Fabricated turbine airfoil
09/18/2013CN103306742A Method for cooling combustion gas turbine blade
09/18/2013CN103306741A Turbomachine blade with improved stiffness to weight ratio
09/18/2013CN103306740A Compressor/turbine rotor-torque transmission through hybrid drive
09/18/2013CN103306739A Centripetal impeller for gas turbine engine
09/18/2013CN103306738A Annular Tesla turbine
09/18/2013CN103306736A Power turbine and power machine of the power turbine
09/18/2013CN103306735A Hybrid power machine
09/18/2013CN101356302B Layer system comprising two pyrochlore phases
09/17/2013US8535013 Aeroengine fan assembly
09/17/2013US8535012 Arrangement for axially securing blades in a rotor of a gas turbine
09/17/2013US8535006 Near-wall serpentine cooled turbine airfoil
09/17/2013US8535005 Blades, turbine blade assemblies, and methods of forming blades
09/17/2013US8535004 Four-wall turbine airfoil with thermal strain control for reduced cycle fatigue
09/17/2013US8534997 Fluid flow machine with a blade row group featuring a meridional edge distance
09/17/2013US8534995 Turbine engine sealing arrangement
09/17/2013US8534990 Inlet guide vane drive system with spring preload on mechanical linkage
09/17/2013US8534066 Two-stage turbocharged engine system
09/17/2013CA2565266C Fluid flow machine blade
09/17/2013CA2509863C Double impingement vane platform cooling
09/12/2013WO2013134181A1 Turbine diaphragm airfoil, diaphragm assembly, and method of repair
09/12/2013WO2013133945A1 Airfoil with improved internal cooling channel pedestals
09/12/2013WO2013133875A2 Composite rotor and vane assemblies with integral airfoils
09/12/2013WO2013132189A1 Turbomachine blade comprising an insert protecting the blade tip
09/12/2013WO2013132113A1 Fan impellers and method for producing fan impellers
09/12/2013WO2013132055A1 Radial turbomachine having a swirl-reducing element
09/12/2013WO2013131774A1 Impeller for a rotor of a turbomachine, and rotor and turbomachine having an impeller of said type
09/12/2013US20130236330 Turbine airfoil with an internal cooling system having vortex forming turbulators
09/12/2013US20130236329 Rotor blade with one or more side wall cooling circuits
09/12/2013US20130236326 Blade pocket design
09/12/2013US20130236325 Blade tip profile
09/12/2013US20130236323 Leading edge protection and method of making
1 ... 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 ... 330