Patents for F01D 9 - Stators (10,038)
04/2006
04/06/2006US20060073011 Corner cooled turbine nozzle
04/06/2006DE102005045459A1 Mechanische Lösung zur Schienenhalterung von Turbinendüsen Mechanical solution for rail mounting of turbine nozzle
04/05/2006EP1643084A1 Turbine engine shroud segment, hanger and assembly
04/05/2006EP1643083A2 Coupled parametric design of flow control and duct shape
04/05/2006EP1642008A1 Turbine shroud segment
04/05/2006EP1642006A1 Turbine shroud segment
04/05/2006CN1755063A Turbine overspeed limiting device
04/04/2006US7021893 Fanned trailing edge teardrop array
04/01/2006CA2520703A1 Corner cooled turbine nozzle
03/2006
03/30/2006WO2006033407A1 Wall shape of axial flow machine and gas turbine engine
03/30/2006US20060067817 Damped assembly
03/30/2006US20060067816 Cooling fan with fluid control device
03/30/2006CA2521983A1 Process for air circulation in a turbine engine compressor, compressor arrangement putting it into play, stage of compression and compressor comprising such an arrangement, and aircraft engine equipped with such a compressor
03/29/2006EP1640591A1 Turbojet engine with a monobloc arm for the connexion of subsidiaries
03/29/2006EP1639234A1 Machine stator and mounting and dismounting methods
03/29/2006CN1752416A Mechanical solution for rail retention
03/28/2006US7020139 Trunking and mirroring across stacked gigabit switches
03/28/2006US7018176 Cooled turbine airfoil
03/28/2006US7018174 Turbine blade
03/28/2006US7018173 Device for stopping in rotation a fixed blade bearing sector in a gas turbine casing
03/23/2006WO2006029844A1 Protection device for a turbine stator
03/23/2006US20060062666 Variable area diffuser
03/23/2006US20060062665 Variable area diffuser vane geometry
03/23/2006DE102004037356A1 Wandstruktur zur Begrenzung eines Heißgaspfads Wall structure for defining a hot gas path
03/23/2006DE102004036594A1 Strömungsstruktur für eine Gasturbine Flow structure for a gas turbine
03/23/2006CA2580472A1 Protection device for a turbine stator
03/22/2006EP1637253A1 Process of fabricating a turbine blade and core assembly to be used in the process
03/22/2006EP1334262B1 Exhaust gas turbocharger for an internal combustion engine with variable turbine geometry
03/21/2006US7013652 Gas turbo set
03/21/2006CA2520282A1 Turbine module for gas turbine engine
03/16/2006WO2005108748A3 Apparatus for bearing lubrication in turbine engines
03/16/2006US20060056963 Retaining of centring keys for rings under variable angle stator vanes in a gas turbine engine
03/16/2006DE102004044703A1 Exhaust gas turbocharger for internal combustion engine, has anti-fatigue bolt provided in bearing housing for fastening guide vane carrier and flow channel unit and gripping through unit and carrier
03/16/2006DE102004044324A1 Abgasturbolader Exhaust gas turbocharger
03/16/2006DE102004037955A1 Turbomaschine, insbesondere Gasturbine Turbo machine, in particular gas turbine
03/15/2006EP1635039A1 Coupling device with key elements for mounting a seal ring to the stator blades of a gas turbine
03/14/2006US7011494 Dual retention vane arm
03/14/2006US7011493 Turbomachine with cooled ring segments
03/14/2006US7011492 Turbine vane cooled by a reduced cooling air leak
03/10/2006CA2518355A1 Retention of centring keys of the rings under the variable setting stator blades of a gas turbine engine
03/09/2006WO2006026695A2 Welding shield for automated welding of impellers and blisks, sized to match within vallexs of a particular designed impeller ; method to provide protection from welding related damage in an impeller
03/09/2006WO2006025847A2 Fanned trailing edge teardrop array
03/09/2006US20060051201 Undercut flange turbine nozzle
03/09/2006US20060051200 Flow structure for a gas turbine
03/09/2006DE102004042699A1 Strömungsstruktur für eine Gasturbine Flow structure for a gas turbine
03/09/2006DE102004042127A1 Rotor-Stator-Vorrichtung mit Anstreifbelag Rotor-stator device with abradable
03/08/2006EP1632648A2 Gas turbine flow path
03/08/2006EP1631736A1 Exhaust gas turbine for an exhaust gas turbocharger
03/07/2006US7009968 Gigabit switch supporting improved layer 3 switching
03/07/2006US7008185 Gas turbine engine turbine nozzle bifurcated impingement baffle
03/07/2006US7008183 Deflector embedded impingement baffle
03/07/2006US7008182 Exhaust-gas-turbine casing
03/07/2006US7008178 Inboard cooled nozzle doublet
03/07/2006US7007488 Modulated flow turbine nozzle
03/07/2006US7007482 Combustion liner seal with heat transfer augmentation
03/02/2006DE102004018987B4 Protective device against bursting turbochargers comprises an endless looped belt of textile fiber material which has a high penetration resistance, and covers at least a part of the turbocharger circumference
03/02/2006DE102004002888B4 Gasturbinen-Endrohrdichtungsanordnung Gas turbine exhaust tip seal assembly
03/01/2006EP1630358A2 A gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger
03/01/2006CN1740522A Variable camber and stagger airfoil and method
02/2006
02/28/2006US7004721 Annular platform for a nozzle of a low-pressure turbine of a turbomachine
02/28/2006US7004720 Cooled turbine vane platform
02/27/2006CA2513079A1 Lightweight annular interturbine duct
02/24/2006CA2513043A1 Vane attachment arrangement
02/23/2006DE102005033362A1 Axialdampfturbinenanordnung Axialdampfturbinenanordnung
02/23/2006DE102004040536A1 Exhaust gas turbocharger for motor vehicle, has adjusting ring connected with guide vane along direction of flow of exhaust gas flow, where angle position of vane relative to direction of flow is adjusted by flexible deformation of vane
02/23/2006DE102004039477A1 Turbine body for turbo-charger, has spiral housing whose one part welded with contour bushing and/or outlet connection forms spiral shaped contour of canal and other part welded at bearing casing is flat base plate
02/23/2006DE102004038903A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine
02/22/2006EP1627990A2 Boundary layer control arrangement
02/22/2006EP1337740B1 Gas turbine stator
02/21/2006US7001147 Airfoil shape and sidewall flowpath surfaces for a turbine nozzle
02/21/2006US7001141 Cooled nozzled guide vane or turbine rotor blade platform
02/21/2006US7001140 Centrifugal fan diffuser
02/21/2006US7001075 Bearing hub
02/21/2006US7000406 Gas turbine combustor sliding joint
02/16/2006US20060034689 Turbine
02/16/2006US20060034688 Axial fan assembly
02/16/2006US20060034685 Gas turbine and gas turbine cooling method
02/16/2006US20060034684 Fluid flow engine and support ring for it
02/16/2006US20060034683 Adjustable flow turbine nozzle
02/16/2006US20060032237 Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle
02/16/2006US20060032236 Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine
02/16/2006DE102004036331A1 Einströmgehäuse für axiale Strömungsmaschinen Inflow for axial flow machines
02/16/2006DE102004036066A1 Verfahren zum Reparieren bzw. Fertigen eines Bauteils A method of repairing or manufacturing a component
02/15/2006EP1626163A2 Clip member for a stator assembly
02/14/2006US6997678 Heat dissipation fan with flow guide device
02/14/2006US6997676 Bifurcated outlet guide vanes
02/14/2006US6997673 Gas turbine high temperature turbine blade outer air seal assembly
02/14/2006US6997672 Turbocharger
02/14/2006US6996992 Gas collection pipe carrying hot gas
02/09/2006US20060029495 Axial flow pump and diagonal flow pump
02/08/2006CN1730913A Solid particle erosion resistant steam turbine nozzle
02/08/2006CN1240931C Three-D axial-flow turbine stage
02/07/2006US6994520 Internal core profile for a turbine nozzle airfoil
02/07/2006US6994514 Turbine blade and gas turbine
02/02/2006DE102004033884A1 Exhaust gas turbocharger for internal combustion engine in especially motor vehicle has wall around axial flow passage bounding resonance chamber on annular passage side formed by section of flow passage component
02/01/2006EP1621734A1 Gas turbine engine with modulated flow turbine nozzle
02/01/2006EP1621733A2 Flow device for a gas turbine
02/01/2006CN1729352A Turbine, fixing device for blades and working method for dismantling the blades of a turbine
02/01/2006CN1727645A High efficiency stator for the first phase of a gas turbine
02/01/2006CN1727642A High temperature gas flow passage component with mesh type and impingement cooling
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