Patents for F01D 9 - Stators (10,038)
07/2004
07/07/2004EP1435492A2 High temperature turbine nozzle and process for manufacturing
07/07/2004EP1435432A1 Turbine blade
07/06/2004US6760264 Apparatus and structure for rapid enablement
07/06/2004US6758653 Ceramic matrix composite component for a gas turbine engine
07/06/2004US6758651 Gas turbine
07/01/2004WO2004055333A1 Grommeted bypass duct penetration
07/01/2004US20040126229 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing
07/01/2004US20040124229 Methods for replacing portions of turbine shroud supports
07/01/2004US20040123445 Method of producing polygonal ring-shaped machine parts having complex cross-section
07/01/2004DE10356243A1 Verfahren zum Herstellen einer Düsenkasteneinrichtung für eine Dampfturbine A method of manufacturing a nozzle box device for a steam turbine
07/01/2004DE10260443A1 Housing for multi-stage rotary pump is fabricated from sheet metal and has impeller wheel separated from the housing walls by a seal
06/2004
06/30/2004EP1433925A1 Fixing process of a blade on a shroud
06/30/2004EP1433924A2 Gas turbine combustor
06/30/2004EP1433565A1 Methods for replacing portions of turbine shroud supports
06/30/2004EP1432549A1 A method for manufacturing a stator or rotor component
06/30/2004CN1508396A Structure for connecting or space sealing members with different thermal expansion coefficients
06/29/2004US6754956 Methods for manufacturing a nozzle box assembly for a steam turbine
06/24/2004US20040120814 Methods and apparatus for assembling gas turbine nozzles
06/24/2004US20040120813 Methods and apparatus for securing turbine nozzles
06/24/2004US20040120811 Methods and apparatus for securing multi-piece nozzle assemblies
06/24/2004US20040120810 Methods and apparatus for assembling gas turbine nozzles
06/24/2004US20040120808 Shroud segment and assembly with surface recessed seal bridging adjacent members
06/24/2004US20040120806 Shroud segment and assembly with circumferential seal at a planar segment surface
06/24/2004US20040120803 Turbine shroud segment apparatus for reusing cooling air
06/24/2004DE10358378A1 Steam turbine has rope seal which is interposed in each interface between nozzle hooks, formed at ends of turbine nozzles supported in stator, and nozzle-hook receiving grooves of stator
06/23/2004EP1431518A2 Turbine engine shroud segment assembly with a surface-recessed seal bridging adjacent shroud segments
06/23/2004EP1431517A2 Turbine nozzles
06/23/2004EP1431516A2 Diffuser arrangement
06/23/2004EP1431515A2 Turbine engine shroud segment and assembly with circumferential seal on a planar segment surface
06/23/2004EP1431514A2 Venturi outlet turbine airfoil
06/23/2004EP1431513A2 Methods and apparatus for assembling gas turbine nozzles
06/22/2004US6752591 Suspension
06/22/2004US6751962 Tail tube seal structure of combustor and a gas turbine using the same structure
06/17/2004US20040115462 Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration
06/17/2004US20040115053 Venturi outlet turbine airfoil
06/17/2004US20040115046 Sealing of steam turbine nozzle hook leakages using a braided rope seal
06/17/2004US20040112287 Method and device for gas phase diffusion coating of metal components
06/17/2004US20040112039 Gas turbine combustor
06/17/2004US20040111829 Grommeted bypass duct penetration
06/16/2004EP1428982A1 A method of depositing a local MCrAIY-coating
06/16/2004EP1428903A2 Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration
06/15/2004US6749396 Failsafe film cooled wall
06/15/2004US6749395 Device and method for controlling a cooling air flow of a gas turbine
06/10/2004US20040109765 Turbine blade
06/10/2004US20040109759 Housing for a turbocharger
06/10/2004US20040109724 Fastening system
06/10/2004US20040107573 Methods for manufacturing a nozzle box assembly for a steam turbine
06/09/2004EP1426561A2 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
06/09/2004EP1426559A1 Inner shroud for an axial compressor
06/09/2004EP1426558A2 Gas turbine transition piece with dimpled surface and cooling method for such a transition piece
06/09/2004EP1426557A1 Casing for turbo charger
06/09/2004EP1425495A1 Turbine housing for high exhaust temperature
06/09/2004DE10355449A1 Turbinenschaufel Turbine blade
06/09/2004DE10255389A1 Low pressure steam turbine has multi-channel diffuser with inner and outer diffuser rings to take blade outflow out of it
06/09/2004CN2620091Y Improvement of jet nozzle ring cover for pressurizing device of IC engine
06/09/2004CN1502788A 涡轮叶片和燃气轮机 Turbine blades and turbine
06/08/2004US6746209 Methods and apparatus for cooling gas turbine engine nozzle assemblies
06/03/2004US20040103534 Method for manufacturing a stator component
06/03/2004US20040103533 Method for manufacturing a stator or rotor component
06/02/2004EP1424467A2 Row of long and short chord length turbine airfoils
06/02/2004EP1423586A1 Combustion chamber intermediate part for a gas turbine
06/02/2004EP1423230A1 A method for manufacturing a hollow blade for a stator or rotor component
06/02/2004CN1500970A Turbine nozzle retention apparatus at the carrier horizontal joint face
06/01/2004US6743350 Apparatus and method for rejuvenating cooling passages within a turbine airfoil
06/01/2004US6742989 Structures of turbine scroll and blades
06/01/2004US6742987 Cradle mounted turbine nozzle
06/01/2004US6742986 Variable displacement turbine
06/01/2004US6742984 Divided insert for steam cooled nozzles and method for supporting and separating divided insert
05/2004
05/27/2004WO2004044387A1 Slotted guide vane
05/27/2004US20040101405 Row of long and short chord length and high and low temperature capability turbine airfoils
05/27/2004US20040101400 Cooled turbine assembly
05/26/2004EP1422383A2 Gas turbine blade cooling
05/26/2004EP1422382A1 Axial flow turbine
05/26/2004EP1422381A2 Method of repairing a turbine nozzle segment, and turbine nozzle segment
05/25/2004US6740177 Castable and weldable nickel-base alloys exhibiting desirable properties suitable for gas turbine engine applications
05/25/2004US6739832 Exhaust turbocharger
05/25/2004US6739594 Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint
05/25/2004US6739381 Method of producing a turbine blade
05/20/2004US20040096328 Turbine blade and gas turbine
05/20/2004US20040096323 Turbine nozzle segment and method of repairing same
05/20/2004US20040096322 Fabricated repair of cast nozzle
05/20/2004US20040093869 Lead-in structure and a fixing flange for a turbo generator
05/19/2004EP1419849A1 Fabricated repair of cast nozzle
05/19/2004DE10250302A1 Drallerzeugungseinrichtung für einen Verdichter Swirler for a compressor
05/19/2004CN1497217A Cylinder combustion chamber irrelevant on dynamic
05/18/2004US6736599 First stage turbine nozzle airfoil
05/18/2004US6736401 Laminated finger seal with ceramic composition
05/13/2004WO2004040108A1 Effusion cooled transition duct with shaped cooling holes
05/13/2004US20040088988 Gas turbine engine transition liner assembly and repair
05/13/2004DE10350946A1 Turbinendüsenhaltevorrichtung an der horizontalen Verbindungsfläche des Trägers Turbine nozzle holder at the horizontal joint surface of the carrier
05/13/2004DE10307028B3 Exhaust gas manifold for automobile IC engine has channels feeding exhaust gas received from engine cylinders to turbine wheel of exhaust gas turbine of turbocharger
05/12/2004EP1418320A1 Gas turbine
05/12/2004CN1495341A Easy-to-assemble heat-screening device for connecting cooling tube and through hole
05/12/2004CN1495339A Simplified nozzle supporting device for gas turbine
05/12/2004CN1495338A Method for sealing variable blade component of gas-turbine
05/11/2004US6733237 Method and apparatus for mounting stator blades in axial flow compressors
05/11/2004US6733236 Compressor in a turbocharger
05/11/2004US6733231 Vapor tube structure of gas turbine
05/11/2004US6733229 Insert metering plates for gas turbine nozzles
05/06/2004WO2004038197A1 Transition duct with enhanced profile optimization
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