Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 9 - Stators
Patents for F01D 9 - Stators (10,038)
05/2003
05/14/2003EP1309773A1 Turbine vane system
05/14/2003CN1418284A Cooling system for turbine blade
05/14/2003CN1108441C 燃气轮机 Gas turbine
05/13/2003US6561757 Turbine vane segment and impingement insert configuration for fail-safe impingement insert retention
05/13/2003US6560890 Fixture for locating and clamping a part for laser drilling
05/08/2003WO2003038254A1 Turbine engine with air cooled turbine
05/07/2003EP1308630A1 Stator sector for a compressor of a turbomachine
05/07/2003EP1308611A2 Firewall for gas turbine engines
05/07/2003EP1308601A1 Bleed device for a turbofan
05/07/2003EP0929734B1 Gas turbine airfoil cooling
05/06/2003US6558115 Turbine guide blade
05/06/2003US6558114 Gas turbine with baffle reducing hot gas ingress into interstage disc cavity
05/02/2003EP1306525A1 Antirotation support system for the nozzle sector of a turbomachine
05/02/2003EP1306524A2 Turbine shroud cooling hole configuration
05/02/2003EP1305504A1 Suspension
05/01/2003WO2003036050A1 Device for stopping in rotation a fixed blade bearing sector in a gas turbine casing
05/01/2003US20030082051 Fixed guide vane assembly separated into sectors for a turbomachine compressor
05/01/2003US20030082046 Turbine shroud cooling hole diffusers and related method
05/01/2003US20030079477 Turbine engine having turbine cooled with diverted air
05/01/2003US20030079465 Bleed-off device in a bypass turbojet
04/2003
04/29/2003US6554566 Turbine shroud cooling hole diffusers and related method
04/29/2003US6554563 Tangential flow baffle
04/29/2003US6554562 Combustor hot streak alignment for gas turbine engine
04/29/2003US6553766 Cooling structure of a combustor tail tube
04/29/2003US6553762 Exhaust gas turbocharger for an internal combustion engine
04/29/2003US6553665 Stator vane assembly for a turbine and method for forming the assembly
04/24/2003US20030077171 Method for repairing a turbine vane
04/24/2003US20030077170 Structures of turbine scroll and blades
04/24/2003US20030077166 Low hoop stress turbine frame support
04/23/2003EP1304445A2 Structure of radial turbine scroll and blades
04/23/2003EP1303683A1 Variable nozzle turbocharger with sheet metal shroud
04/23/2003CN1412417A Turbine volute pipeline and moving blade structure
04/23/2003CN1106496C Turbine shaft and process for cooling it
04/22/2003US6551062 Turbine airfoil for gas turbine engine
04/22/2003US6550254 Gas turbine engine bleed scoops
04/17/2003DE20023203U1 Arrangement for improving efficiency of flow machines, preferably in motor vehicles, has flow control body whose inlet and outlet sections have protruding, increased flow cross-sections
04/17/2003DE10207456C1 Exhaust gas turbocharger for IC motor, has a spiral inflow channel into the turbine housing with a gas flow deflector at the inner channel wall to reduce mechanical and thermal stress
04/16/2003EP1302639A2 A method for enhancing part life in a gas stream
04/16/2003EP1302629A1 Compressor stator stage comprising stator vanes and assembly method for the stator vanes
04/16/2003EP1302628A2 Airfoil with indentations to enhance heat transfer
04/15/2003US6547645 Method and backer inserts for blocking backwall water jet strikes
04/15/2003US6547524 Film cooled article with improved temperature tolerance
04/15/2003US6547521 Flow duct guide apparatus for an axial flow turbine
04/15/2003US6547518 Low hoop stress turbine frame support
04/15/2003US6547257 Combination transition piece floating cloth seal and stage 1 turbine nozzle flexible sealing element
04/15/2003US6546735 Methods and apparatus for operating turbine engines using rotor temperature sensors
04/15/2003US6546627 Repair method for a gas turbine
04/10/2003US20030068225 Nozzle lock for gas turbine engines
04/10/2003US20030068223 Bleed deflector for a gas turbine engine
04/10/2003US20030068222 Turbine airfoil with enhanced heat transfer
04/10/2003US20030066292 Wear reduction means for a gas turbine combustor transition duct end frame
04/09/2003EP1300567A2 Bleed deflector for a gas turbine
04/09/2003EP1299619A1 Draining and cooling system for gas turbine cushions
04/09/2003EP1299618A1 Connecting system for a transition duct in a gas turbine
04/09/2003CN1409800A Turbine blade and method for producing turbine blade
04/09/2003CN1105231C Exhaust turbine of exhanst turbine supercharger
04/09/2003CN1105226C Turbine Spray nozzle and turbine rotary blade for axial-flow type turbomachine
04/08/2003US6543998 Nozzle ring for an aircraft engine gas turbine
04/08/2003US6543996 Hybrid turbine nozzle
04/08/2003US6543995 Stator vane and stator assembly for a rotary machine
04/08/2003US6543993 Apparatus and methods for localized cooling of gas turbine nozzle walls
04/08/2003US6543449 Medical ventilator
04/03/2003WO2003027494A1 Method and guiding device for increasing a water turbine's efficiency
04/03/2003DE10137899C1 Axial turbine for exhaust gas turbocharger of diesel engine has gas outlet channel acting as diffuser for surrounding collection space communicating with exit flow line
04/02/2003EP1298286A2 Guide vane assembly
04/02/2003CN1407210A Coolant channel joint structure and pipe sealing of gas turbine and gas turbine
04/01/2003US6540481 Diffuser for a centrifugal compressor
03/2003
03/27/2003WO2003025350A1 Device for maintaining joints with sealing leaves
03/27/2003WO2003025349A1 Turbine housing for high exhaust temperature
03/27/2003US20030059291 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
03/26/2003EP1296023A1 Fixing device for seal strips
03/26/2003EP1295014A1 Transition piece for non-annular gas turbine combustion chambers
03/26/2003CN1405496A Combustion chamber structure of gas turbine
03/26/2003CN1405438A Gas turbine and method for operating gas turbine
03/26/2003CN1405431A Gas turbine blade/guiding blade
03/25/2003US6537022 Nozzle lock for gas turbine engines
03/25/2003US6536216 Apparatus for injecting fuel into gas turbine engines
03/20/2003WO2003023193A1 Assembly of sectors of a dispensing unit in a gas turbine
03/20/2003WO2003023192A1 A conduit for a gas turbine unit and a method of manufacturing a conduit
03/20/2003US20030053910 Turbine housing for high exhaust temperature
03/20/2003US20030052457 Pressure actuated snout sealing system for steam turbines
03/19/2003EP1293645A1 Turbomachine axial compressor with flow splitting device and assembly method for this device
03/19/2003EP1293643A1 Turbomachine stator segment assembly
03/18/2003US6533547 Turbine blade
03/18/2003US6533546 Low-pressure steam turbine with multi-channel diffuser
03/18/2003US6533544 Turbine blade
03/18/2003US6533542 Split ring for gas turbine casing
03/13/2003WO2003021084A1 Combustion chamber intermediate part for a gas turbine
03/13/2003WO2003020469A1 A method for manufacturing a stator or rotor component
03/13/2003US20030049127 Cooling system for a turbine blade
03/13/2003US20030049126 Joint structure of coolant passage, tube seal, and gas turbine
03/13/2003US20030049125 Reinforcement and cooling structure of a turbine blade
03/13/2003US20030047298 Device and method for producing a blade for a turbine and blade produced according to this method
03/13/2003US20030046940 Seal structure for combustor liner
03/13/2003US20030046935 Method for injecting fuel into gas turbine engines
03/12/2003EP1291491A2 Transfer tube for gas turbine coolant passages
03/12/2003EP1291142A2 Method and backer inserts for blocking backwall water jet strikes
03/12/2003EP1040256B1 Support for a turbine stator assembly
03/11/2003US6530745 Cooling system for gas turbine stator nozzles
03/11/2003US6530744 Integral nozzle and shroud
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