Patents for F01D 9 - Stators (10,038)
10/2009
10/22/2009US20090263237 Coated turbine component and method of coating a turbine component
10/22/2009DE102008019740A1 Stator- und/oder Rotor-Stufe eines Axialverdichters einer Strömungsmaschine mit Strömungsleitelementen zur Wirkungsgradsteigerung Stator and / or rotor stage of an axial flow machine with a flow guidance to increase the efficiency
10/22/2009DE102008019156A1 Strebe für ein Turbinenzwischengehäuse, Turbinenzwischengehäuse und Verfahren zur Herstellung eines Turbinenzwischengehäuses Strut for a turbine housing, the turbine housing and intermediate process for producing a turbine center frame
10/21/2009EP1373593B1 Method and device for gas phase diffusion coating of metal components
10/21/2009CN201330620Y Novel high pressure clapboard static cascade applicable to steam turbine varying duty running
10/20/2009CA2569026C Wall configuration of axial-flow machine, and gas turbine engine
10/20/2009CA2416331C Variable geometry turbocharger with sheet metal shell
10/15/2009WO2009125078A2 Sectored distributor for turbomachine
10/15/2009US20090257868 Diffuser
10/15/2009US20090257866 Stator blade for a turbomachine, especially a steam turbine
10/15/2009CA2715454A1 Sectored distributor for turbomachine
10/14/2009EP2108787A2 Methods for repairing a damaged variable vane shroud and corresponding vane shroud
10/14/2009EP2108785A2 Turbine blade and vane assembly with a ceramic platform
10/14/2009EP2108784A2 Flow machine with fluid injector component group
10/14/2009EP2108078A2 A gas turbine
10/14/2009CN101558219A Turbine housing for a turbocharger
10/14/2009CN100549366C Protection device for a turbine stator
10/13/2009US7600970 Ceramic matrix composite vane seals
10/13/2009US7600962 Turbine exhaust system and method for modifying the same
10/13/2009US7600382 Turbine engine with interstage heat transfer
10/08/2009WO2009123300A2 Rotary machine scroll structure and rotary machine
10/08/2009WO2009121653A1 Device for a horizontally split turbomachine housing, guide disc segment and guide blade carrier for a horizontally split turbomachine housing
10/08/2009US20090252603 Airfoil for nozzle and a method of forming the machined contoured passage therein
10/08/2009US20090249786 Turbomachine system and turbine therefor
10/08/2009DE10350946B4 Turbinendüsenhaltevorrichtung an der horizontalen Verbindungsfläche des Trägers Turbine nozzle holder at the horizontal joint surface of the carrier
10/08/2009DE102009003710A1 Schaufelblatt für einen Leitapparat mit einem maschinell bearbeiteten kontourierten Kanal darin Airfoil for a diffuser with a machined contoured channel therein
10/07/2009EP2107219A1 Vane ring segment and vane ring carrier for a horizontally split turbo engine casing
10/07/2009CN100547229C Stator vane stage actuated by a rotary actuator ring moved by electric motor means
10/01/2009WO2009120778A2 Subsonic and stationary ramjet engines
10/01/2009WO2009118490A2 Turbine distributor for turbine engine
10/01/2009WO2009118245A1 Guide vane for a gas turbine and gas turbine comprising such a guide vane
10/01/2009WO2009118235A2 Guide vane for a gas turbine
10/01/2009US20090246014 method and system for supporting stator components
10/01/2009US20090246012 Turbine stator mount
10/01/2009US20090246008 Layer System
10/01/2009DE102009003647A1 Austauschbare Blende zur Abstimmung der Verbrennung und zugehöriges Verfahren Replaceable diaphragm for combustion and associated method
10/01/2009DE102009003638A1 System und Verfahren zur Halterung von Statorkomponenten System and method for holding stator
10/01/2009DE102008000856A1 Exhaust gas turbocharger for internal combustion engine of motor vehicle, has passing component arranged between turbine housing and turbine wheel, where passing component defines outline of turbine wheel
10/01/2009DE102008000855A1 Housing, particularly turbocharger housing for use in devices heated during operation, has partially metallic foam with external surface, which contains coating or sealing, and housing external surface which has metallic structure
10/01/2009DE102008000852A1 Abgasturbolader für ein Kraftfahrzeug Exhaust gas turbocharger for a motor vehicle
10/01/2009DE102008000849A1 Exhaust gas turbocharger for vehicles, has housing, in which guide vane module is inserted centered to rotating axis of turbine, where guide vane of guide vane module is arranged between base plate and cover plate
10/01/2009CA2719575A1 Subsonic and stationary ramjet engines
10/01/2009CA2717983A1 Turbine distributor for turbine engine
09/2009
09/30/2009CA2660179A1 A system and method for supporting stator components
09/29/2009US7594794 Leaned high pressure compressor inlet guide vane
09/25/2009CA2659489A1 Hybrid impingement cooled turbine nozzle
09/24/2009WO2009115390A1 Guide vane for a gas turbine
09/24/2009WO2009115384A1 Guide blade having hooked fastener for a gas turbine
09/24/2009US20090238682 Compressor stator with partial shroud
09/24/2009DE202009008234U1 Adaptive kinematische Segmente für bewegliche Statorschaufeln von Vorleitapparaten in Strömungsmaschinen Adaptive kinematic segments for movable stator blades of Vorleitapparaten in turbomachines
09/24/2009DE102008014743A1 Verdichterstator mit Teildeckband Compressor stator with partial shroud
09/23/2009EP2103783A2 Compactor stator with partial cover band
09/23/2009EP2103782A1 Blade structure for gas turbine
09/23/2009CN101539031A Heat exchange type nozzle box of turbine engine
09/23/2009CN100543283C Gas turbine engine component having bypass circuit
09/22/2009US7591634 Stator shim welding
09/22/2009CA2445057C Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine
09/22/2009CA2398515C Turbine airfoil for gas turbine engine
09/17/2009WO2009113897A1 Turbine comprising a flexible seal and corresponding flexible seal for a gas turbine engine
09/17/2009WO2009083456A3 Gas turbine
09/17/2009US20090232650 Tip turbine engine and corresponding operating method
09/17/2009US20090232646 Use of a Thermal Barrier Coating for a Housing of a Steam Turbine, and a Steam Turbine
09/16/2009EP2101041A2 Cooling air manifold splash plate for a gas turbine engine
09/16/2009CN201310386Y Oblique flow type exhaust turbine pressure booster
09/15/2009US7588412 Cooled shroud assembly and method of cooling a shroud
09/11/2009WO2009109430A1 Sealing arrangement and gas turbine
09/10/2009US20090226322 Airfoil design for rotor and stator blades of a turbomachine
09/10/2009DE102009010997A1 Ladeeinrichtung Loader
09/10/2009DE102008011258A1 Gekühltes Gehäuse bestehend aus einem Turbinengehäuse und einem Lagergehäuse eines Turboladers Cooled housing comprising a turbine housing and a bearing housing of a turbocharger
09/10/2009DE102008011257A1 Gekühltes Turbinengehäuse Cooled turbine housing
09/09/2009EP2098686A2 Two-shaft gas turbine
09/09/2009EP2097798A2 Flow distribution regulation arrangement with bimetallic elements for adjusting the flow distribution in a cooling channel
09/09/2009EP2097617A2 Vane ring, and method for the production thereof
09/09/2009EP1689978B1 Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction
09/09/2009CN101529053A Guiding device of a flow machine and guide vane for such a guiding device
09/09/2009CN101526015A Recuperative high efficiency turbine engine
09/09/2009CN100538018C Turbine shroud segment
09/08/2009CA2303970C Medical ventilator
09/03/2009WO2009108084A1 A gas turbine component and a method for producing a gas turbine component
09/03/2009WO2009106464A1 Turbine blade or vane with cooled platform
09/02/2009EP2096268A2 Valve assembly for regulating a fluid flow
09/02/2009EP2096265A2 Turbine nozzle with integral impingement blanket
09/02/2009EP2096264A2 Variable geometry turbine and turbocharger
09/02/2009EP1885999B1 Air intake for a turbocharger for an internal combustion engine
09/01/2009US7581924 Turbine vanes with airfoil-proximate cooling seam
09/01/2009US7581920 Method for air circulation in a turbomachine compressor, compressor arrangement using this method, compression stage and compressor incorporating such a arrangement, and aircraft engine equipped with such a compressor
08/2009
08/29/2009CA2655689A1 Turbine nozzle with integral impingement blanket
08/27/2009WO2009104317A1 Gas turbine
08/27/2009WO2009103671A1 Gas turbine having an improved cooling architecture
08/27/2009WO2009103658A1 Gas turbine having an annular combustion chamber
08/27/2009WO2009103632A1 Gas turbine
08/27/2009WO2009085580A3 Turbine nozzle segment and method for repairing a turbine nozzle segment
08/27/2009US20090214335 Method of repair for cantilevered stators
08/26/2009EP2093383A1 Vane and vane assembly
08/26/2009EP2093382A2 Stator vane having a fanned cooling hole array on a large fillet between airfoil and platform
08/26/2009EP2093381A1 Turbine blade or vane with cooled platform
08/26/2009EP2093380A2 Single channel inner diameter shroud with lightweight inner core in a gas turbine
08/26/2009EP2093379A2 Variable-nozzle assembly for a turbocharger
08/26/2009EP2092163A1 Vane assembly configured for turning a flow ina a gas turbine engine, a stator component comprising the vane assembly, a gas turbine and an aircraft jet engine
08/25/2009US7578653 Ovate band turbine stage
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