Patents for F01D 9 - Stators (10,038)
11/2003
11/18/2003CA2117240C Sealing structures for gas turbine engines
11/12/2003EP0929736B1 Steam turbine and process for cooling a steam turbine in ventilation operation
11/11/2003US6644916 Vane and method of construction thereof
11/11/2003US6644032 Transition duct with enhanced profile optimization
11/06/2003US20030206799 Casing section
11/06/2003US20030206798 Casing assembly for the turbine of an exhaust turbocharger
11/06/2003US20030205047 Turbine casing for an exhaust turbocharger made by casting
11/06/2003US20030204944 Forming gas turbine transition duct bodies without longitudinal welds
11/05/2003EP1358958A1 A way to manufacture inserts for steam cooled hot gas path components
11/05/2003EP1084327B1 Gas turbine and method for cooling a turbine stage
11/04/2003US6641363 Gas turbine structure
11/04/2003US6640547 Effusion cooled transition duct with shaped cooling holes
11/04/2003US6640437 Method for installing stator vanes
10/2003
10/30/2003WO2002055754A3 Method and device for gas phase diffusion coating of metal components
10/30/2003US20030202877 Centrifugal blower having centrifugal fan arranged in scroll casing
10/30/2003US20030201087 Way to manufacture inserts for steam cooled hot gas path components
10/29/2003EP1357278A2 Exhaust gas turbine for a turbocharger
10/29/2003CN1451847A Air and steam cooling platform of turbine vane
10/29/2003CN1451846A Turbine vane and casting assemble for mfg. same
10/28/2003US6638021 Turbine blade airfoil, turbine blade and turbine blade cascade for axial-flow turbine
10/28/2003US6638013 Thermally isolated housing in gas turbine engine
10/28/2003US6637751 Supplemental seal for the chordal hinge seals in a gas turbine
10/22/2003EP1355040A2 Turbine blade platform with steam as well as air cooling
10/22/2003EP0926313B1 Structure and method for holding inserts for stationary blades of gas turbine
10/16/2003WO2003085269A1 Method and apparatus for mounting stator blades in axial flow compressors
10/14/2003US6632070 Guide blade and guide blade ring for a turbomachine, and also component for bounding a flow duct
10/14/2003US6631858 Two-piece steam turbine nozzle box featuring a 360-degree discharge nozzle
10/14/2003US6631561 Turbine blade and method for producing a turbine blade
10/09/2003WO2003083267A1 Impingement cooling of gas turbine blades or vanes
10/08/2003EP1350924A2 Fastening of nozzle segments in a gas turbine
10/08/2003EP1073827B1 Turbine blade
10/07/2003US6629817 System and method for airfoil film cooling
10/07/2003CA2065722C Boltless turbine nozzle/stationary seal mounting
10/02/2003WO2003080999A1 Exhaust gas turbocharger in an internal combustion engine
10/02/2003US20030185683 Stator vane span attachment for a gas turbine
10/02/2003US20030185678 Method and apparatus for mounting stator blades in axial flow compressors
10/02/2003US20030185673 Flow-rectifying member and its unit and method for producing flow-rectifying member
10/02/2003US20030185671 Arrangement for the fastening of struts serving as bearing carriers for the rotor of an aeronautical gas turbine to the casing structure of the aeronautical gas turbine
10/01/2003EP1348833A1 Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes
09/2003
09/30/2003US6627019 Process for making ceramic matrix composite parts with cooling channels
09/30/2003US6626641 Nozzle for turbine
09/25/2003US20030180147 Turbrine vane system
09/25/2003US20030180141 Band cooled turbine nozzle
09/25/2003US20030177640 Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes
09/24/2003EP1347152A2 Cooled turbine nozzle sector
09/24/2003CN1443927A Equipment for fixing supporting blades of disributor component arround circumferential curved line
09/23/2003US6623241 Low-pressure steam turbine
09/18/2003WO2003076768A1 Guide blade fixture in a flow channel of an aircraft gas turbine
09/18/2003US20030173213 Supplying solution of alkali metal carbonate or bicarbonate to both anode and cathode chambers of electrolysis cell, which are separated by diaphragm, electrolyzing solution, mixing resulting cathode and anode water to obtain detergent
09/17/2003CN1442603A Method of manufacturing steam turbine
09/16/2003US6619917 Machined fan exit guide vane attachment pockets for use in a gas turbine
09/16/2003US6619915 Thermally free aft frame for a transition duct
09/16/2003US6619912 Turbine blade or vane
09/16/2003US6619109 Steam turbine inlet bell seal inspection apparatus and method
09/16/2003US6619030 Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
09/16/2003CA2262649C Gas turbine first-stage stator blade sealing structure
09/12/2003WO2003074850A1 Improved vane design for use in variable geometry_turbocharger
09/11/2003US20030170115 Variable stator vane support arrangement
09/11/2003US20030170113 Insert metering plates for gas turbine nozzles
09/11/2003US20030167776 Transition piece for non-annular gas turbine combustion chambers
09/10/2003EP1342883A2 Insert metering plates for gas turbine nozzles
09/10/2003CN1441149A Sheet seal support part for turbine inner belt of gas turbine engine
09/10/2003CN1441148A Method and device for cooling gas turbine spray nozzles
09/09/2003US6616407 Gas turbine engine guide vane
09/09/2003US6616405 Cooling structure for a gas turbine
09/04/2003US20030165382 Geothermal turbine
09/04/2003US20030163984 Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
09/03/2003EP1340902A2 Gas turbine with frame supporting counter rotating low pressure turbine rotors
09/03/2003EP1340885A2 Leaf seal support for a gas turbine engine nozzle vane
09/03/2003EP1340884A2 Methods and apparatus for cooling gas turbine nozzles
09/03/2003EP1163429B1 Sealing device for segmented stator ring
09/03/2003CN2570462Y Large-scale heat supply and power-generating turbine separate high and low pressure cylinder arrangement
09/02/2003US6612811 Airfoil for a turbine nozzle of a gas turbine engine and method of making same
09/02/2003US6612808 Article wall with interrupted ribbed heat transfer surface
09/02/2003US6612807 Frame hub heating system
09/02/2003US6612114 Cooling air system for gas turbine
08/2003
08/28/2003WO2003071113A1 Turboblower and method for operating such a turboblower
08/28/2003US20030161726 Leaf seal support for inner band of a turbine nozzle in a gas turbine engine
08/28/2003US20030161718 Thermally isolated housing in gas turbine engine
08/28/2003US20030161716 Method of forming a thermally isolated gas turbine engine housing
08/27/2003EP1338773A2 Gas turbine assembly for air conditioning
08/27/2003EP1338670A2 Abradable coating and method for forming same
08/27/2003EP1338378A2 Fixture for locating and clamping a part for laser drilling
08/26/2003US6609885 Supplemental seal for the chordal hinge seal in a gas turbine
08/26/2003US6609881 Steam turbine inlet and methods of retrofitting
08/26/2003US6609880 Methods and apparatus for cooling gas turbine nozzles
08/21/2003DE10210866C1 Guide blade segment fixing device for flow channel of aircraft gas turbine uses slot and hook fixing and pin fitting through latter
08/20/2003EP1173657B1 Turbine blade and method for producing a turbine blade
08/20/2003EP0906493B1 Turbomachine and process for cooling a turbomachine
08/20/2003EP0900322B1 Turbine shaft and process for cooling a turbine shaft
08/20/2003CN1436920A 透平机叶片 Turbine blades
08/19/2003US6607355 Turbine airfoil with enhanced heat transfer
08/19/2003CA2263508C Sealing device for gas turbine stator blades
08/14/2003US20030150212 Exhaust gas turbocharger for an internal-combustion engine
08/14/2003DE10218436C1 Exhaust gas turbine for IC engine turbocharger has double-walled housing enclosing turbine wheel provided by inner and outer mantles each having 2 half shells
08/13/2003EP1335113A1 Fastening device for gas turbine distributor sectors
08/13/2003EP1335112A1 Fixing a pivoting lever on the shaft of a variable guide vane of a turbomachine
08/13/2003CN1117931C 离心式鼓风机 Centrifugal Blower
08/12/2003US6604286 Method of fabricating gas turbine fuel injection
08/12/2003US6604285 Method and apparatus for electronically determining nozzle throat area and harmonics
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