Patents for F01D 9 - Stators (10,038)
10/2013
10/02/2013EP2644828A1 Modular turbine blade having a platform
10/02/2013EP2643069A1 Oil discharge device and turbomachine comprising such a device
10/01/2013US8545170 Turbo machine efficiency equalizer system
09/2013
09/26/2013WO2013141941A1 Turbine engine and vane system
09/26/2013WO2013140655A1 Gas turbine
09/26/2013WO2013139404A1 Blade row for an unsteady axial flow gas turbine stage
09/26/2013US20130251536 Hybrid airfoil for a gas turbine engine
09/26/2013US20130251520 Scalloped surface turbine stage
09/26/2013US20130251519 Turbojet casing and turbojet receiving such casings
09/26/2013US20130251518 Connector assembly for variable inlet guide vanes and method
09/26/2013US20130251517 Grommet for gas turbine vane
09/26/2013US20130251508 Dual-use of cooling air for turbine vane and method
09/26/2013CA2809805A1 Connector assembly for variable inlet guide vanes and method
09/25/2013EP2642079A1 Turbine diaphragm construction
09/25/2013EP2642078A2 System and method for recirculating a hot gas flowing through a gas turbine
09/25/2013CN203214107U Turbine type air-magnetic engine
09/25/2013CN103321688A System and method for recirculating a hot gas flowing through a gas turbine
09/25/2013CN103321686A Scalloped surface turbine stage
09/24/2013US8540484 Low mass diffuser vane
09/24/2013US8540483 Turbine engine rotating cavity anti-vortex cascade
09/23/2013CA2810029A1 Grommet for gas turbine vane
09/23/2013CA2808804A1 Scalloped surface turbine stage
09/21/2013CA2809000A1 Dual-use of cooling air for turbine vane and method
09/19/2013WO2013138041A1 Arrangement for delivering combustion gas
09/19/2013US20130243580 Gas turbine engine variable stator vane assembly
09/19/2013DE112011104492T5 Verfahren zum Auswuchten einer rotierenden Anordnung eines Gasturbinenmotors Method for balancing a rotating assembly of a gas turbine engine
09/19/2013DE102012102186A1 Turbine für einen Abgasturbolader Turbine for an exhaust gas turbocharger
09/19/2013DE102012005216A1 Turbine for exhaust gas turbocharger of internal combustion engine, has gap having first length portion extending in axial direction and which is smaller than the second length portion of gap, adjoining and extending in axial direction
09/18/2013EP2639408A1 Gas turbine, guide vane for a housing of a gas turbine and method of manufacturing a guide vane
09/18/2013EP2639404A1 Exhaust diffuser for a turbine
09/18/2013EP2639004A1 Blade ring segment with inner end wall having an undulating height profile and method for producing same
09/18/2013CN203201595U Ejector for impact generating device
09/18/2013CN203196787U Ejection nozzle for ejector
09/18/2013CN103306747A Transition piece aft-frame seals
09/18/2013CN103306746A Apparatus and system for directing hot gas
09/18/2013CN103306745A Stator of a gas turbine
09/18/2013CN103306736A Power turbine and power machine of the power turbine
09/18/2013CN103306735A Hybrid power machine
09/17/2013US8534991 Compressor with asymmetric stator and acoustic cutoff
09/17/2013CA2547026C Stage control system for the variable pitch stator blades of a turbomachine
09/12/2013WO2013134181A1 Turbine diaphragm airfoil, diaphragm assembly, and method of repair
09/12/2013US20130236302 In-situ gas turbine rotor blade and casing clearance control
09/12/2013US20130236295 Compact igv for turboexpander application
09/12/2013US20130236293 Systems and methods for an improved stator
09/12/2013DE102012101974A1 Turbine i.e. radial-flow turbine, for supercharger for compressing air supplied to internal combustion engine of motor vehicle, has mean line surface positioned relative to rotational axis in flow channel
09/11/2013EP2636850A1 Stator of a gas turbine
09/11/2013EP2636849A1 Compressor
09/11/2013EP2636848A2 Transition piece aft-frame seals
09/11/2013EP2636847A2 Apparatus and system for directing hot gas
09/11/2013CN103291377A Gas compressor multistage stationary blade rigid adjusting mechanism
09/11/2013CN103291376A Rotating turbomachine component having a tip leakage flow guide
09/06/2013WO2013130570A1 Turbine engine rotor blade groove
09/06/2013WO2013130309A1 Mid-section of a can-annular gas turbine engine with an improved rotation of air flow from the compressor to the turbine
09/06/2013WO2013130308A1 Buffer cooling system providing gas turbine engine architecture cooling
09/06/2013WO2013130307A1 Gas turbine engine buffer cooling system
09/06/2013WO2013130246A1 Gas turbine engine buffer cooling system
09/06/2013WO2013130245A1 Gas turbine engine cooling system
09/06/2013WO2013130163A1 Airfoils and corresponding fabricating method
09/06/2013WO2013130162A1 Stator vane shroud having an offset
09/06/2013WO2013127833A1 Arrangement for a turbomachine
09/04/2013EP2634378A1 Low pressure steam turbine
09/04/2013EP2634374A1 Turbine and method for manufacturing turbine
09/04/2013EP2634373A1 Arrangement for a turbomachine
09/04/2013EP2634372A1 Transition piece aft frame assembly having a heat shield and corresponding combustion system
09/04/2013CN103282606A Low pressure steam turbine
08/2013
08/29/2013WO2013126471A1 Turbine frame fairing for a gas turbine engine
08/29/2013WO2013124171A1 Turbine nozzle segment
08/29/2013US20130224011 Gas turbine
08/29/2013US20130224004 Radial Diffuser Vane for Centrifugal Compressors
08/29/2013US20130223995 Turbocharger With Annular Rotary Bypass Valve for the Turbine
08/29/2013US20130219922 Geared gas turbine engine with reduced fan noise
08/29/2013DE102012203144A1 Strömungsmaschine Flow machine
08/29/2013DE102012202907A1 Abgasturbolader mit relativ zueinander verdrehbaren Leitgitterringen Turbocharger with relatively rotatable Leitgitterringen
08/29/2013CA2807678A1 Nano-metal coated vane component for gas turbine engines and method of manufacturing same
08/28/2013EP2631491A1 Transonic blade
08/28/2013EP2631428A1 Turbine nozzle segment
08/28/2013CN103270276A Method for balancing rotating assembly of gas turbine engine
08/28/2013CN103266922A Turbine stator blade with interstage combustor
08/28/2013CA2807212A1 Sensor-based performance-seeking gas turbine engine control
08/22/2013WO2013122878A1 Anti-rotation stator segments
08/22/2013WO2013056757A3 Hydraulic machine
08/22/2013US20130216368 Turbine stator airfoils with individual orientations
08/22/2013US20130216359 Compressor
08/22/2013DE102012003214A1 Exhaust gas turbocharger for internal combustion engine of e.g. passenger car, has connection channel to arrange guide portion end facing receiving space in which average value of downstream and upstream turbine pressure is applied
08/22/2013DE102012003213A1 Verstellbarer Leitapparat für eine Turbine eines Abgasturboladers und Turbine für einen Abgasturbolader Adjustable diffuser for a turbine of a turbocharger turbine and an exhaust gas turbocharger
08/22/2013DE102004024683B4 Dichtungssystem für horizontale Verbindungsstellen von Zwischenböden von Dampfturbinen Sealing system for horizontal joints of shelves of steam turbines
08/22/2013CA2806401A1 Low-ductility turbine shroud
08/21/2013EP2628903A2 Gas Turbine Engine Airfoil Cooling Circuit
08/21/2013EP2628900A1 Turbine vane with a throttling element
08/21/2013EP2627909A2 Thermally insulating turbine coupling
08/21/2013CN102182517B Boundary layer turbine with blade plate
08/21/2013CN101178016B Set of insulating sheets on a casing to improve blade tip clearance
08/20/2013US8511982 Compressor vane diaphragm
08/20/2013US8511981 Diffuser having detachable vanes with positive lock
08/20/2013US8511980 Segmented ceramic matrix composite turbine airfoil component
08/20/2013US8511979 High pressure turbine vane airfoil profile
08/20/2013US8511978 Airfoil array with an endwall depression and components of the array
08/20/2013US8511969 Interturbine vane with multiple air chambers
08/15/2013WO2013117258A1 Turbine assembly, corresponding impingement cooling tube and gas turbine engine
08/15/2013WO2013081714A3 Guide vane assembly for a gas turbine engine
1 ... 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 ... 101