Patents for F01D 9 - Stators (10,038)
12/2002
12/04/2002EP1262631A2 Film cooled blade or vane
12/04/2002CN1095524C Cross flow type blower
12/03/2002US6488470 Annular flow diffusers for gas turbines
11/2002
11/27/2002EP1259711A1 Aerofoil for an axial flow turbomachine
11/27/2002EP0972128B1 Surface structure for the wall of a flow channel or a turbine blade
11/26/2002US6485655 Method and apparatus for retaining an internal coating during article repair
11/21/2002US20020172596 Film cooled article with improved temperature tolerance
11/20/2002EP1002184B1 Housing for a fan, pump or compressor
11/20/2002CN1380487A 燃气轮机 Gas turbine
11/20/2002CN1380486A Method for manufacturing turbine blade and turbine blade
11/14/2002US20020168537 Article having turbulation and method of providing turbulation on an article
11/14/2002US20020168262 Nozzle adjustment mechanism for variable-capacity turbine
11/13/2002EP1256698A2 Axial turbine with a variable-geometry stator
11/13/2002EP1256695A1 Element for a gas turbine guiding ring and gas turbine comprising such element
11/13/2002EP1212167A4 Method for replacing a turbine vane airfoil
11/13/2002CN1379170A Combustion turbine
11/13/2002CN1379165A Turbine propeller and turbine engine
11/13/2002CN1378890A Method for making turbine vanes
11/11/2002CA2385834A1 Axial turbine for aeronautical applications
11/07/2002US20020163134 Combination transition piece floating cloth seal and stage 1 turbine nozzle flexible sealing element
11/05/2002CA2229915C Gas turbine stationary blade
10/2002
10/31/2002US20020157251 Method of producing a turbine blade
10/31/2002US20020157250 Turbine blade and turbine
10/30/2002EP1252424A1 Variable cycle gas turbine engine
10/24/2002US20020155000 Turbine blade or vane
10/24/2002US20020152753 Fuel mixing in a gas turbine engine
10/23/2002CN1093214C Steam turbine and process for cooling a steam turbine in ventilation operation
10/22/2002US6468669 Article having turbulation and method of providing turbulation on an article
10/22/2002US6468031 Nozzle cavity impingement/area reduction insert
10/22/2002US6467339 Method for deploying shroud segments in a turbine engine
10/17/2002US20020150470 Gas turbine
10/17/2002US20020150467 Steam-cooling-type turbine
10/17/2002US20020150466 Disc turbine inlet to assist self-starting
10/17/2002US20020148233 Gas turbine
10/16/2002EP1249592A2 Steam cooled turbine
10/16/2002EP1249591A2 Cooling structure for gas turbines
10/16/2002EP1249578A1 Cooling of a gas turbine
10/16/2002CN1092749C Exhaust gas structural component for steam turbine
10/16/2002CN1092748C Gas turbine airfoil cooling system and method
10/15/2002US6464457 Turbine leaf seal mounting with headless pins
10/15/2002US6464456 Turbine vane assembly including a low ductility vane
10/15/2002US6463729 Combined cycle plant with gas turbine rotor clearance control
10/10/2002US20020146320 Diffuser for a centrifugal compressor
10/10/2002US20020146317 Vapor tube structure of gas turbine
10/09/2002EP1247944A2 Gas turbine frame
10/09/2002EP1247940A1 Gas turbine stationary blade
10/09/2002EP1247939A1 Turbine blade and process of manufacturing such a blade
10/09/2002EP1247937A1 Gas turbine blade and gas turbine
10/09/2002EP1247602A1 Method for producing an airfoil
10/08/2002US6461109 Third-stage turbine nozzle airfoil
10/08/2002US6461105 Variable vane for use in turbo machines
10/08/2002US6460343 Gas turbine engine
10/03/2002US20020141864 Methods and apparatus for preferential placement of turbine nozzles and shrouds based on inlet conditions
10/03/2002US20020141863 Twisted stator vane
10/02/2002EP1245841A1 Anti-rotation retainer for a conduit
10/02/2002EP1245806A1 Cooled gas turbine balde
10/02/2002EP1245789A1 Exhaust turbocharger
10/02/2002EP1245788A2 Methods and apparatus for preferential placement of turbine nozzles and shrouds based on inlet conditions
10/02/2002EP0998361B1 Turbine blade and use of a known method for producing such a turbine blade
10/02/2002EP0938624B1 Turbofan aircraft engine
10/02/2002DE10101070C1 Verfahren zum Gasphasendiffusionsbeschichten von metallischen Bauteilen Method for gas phase diffusion coating of metal components
10/01/2002US6457933 Methods and apparatus for controlling bearing loads within bearing assemblies
09/2002
09/26/2002WO2002075158A1 Radial flow compressor
09/26/2002US20020134070 Method of increasing engine temperature limit margins
09/24/2002US6453674 Method of operation of gas turbine engine
09/24/2002US6453557 Method of joining a vane cavity insert to a nozzle segment of a gas turbine
09/19/2002DE10112764A1 Radial compression turbocharger for an internal combustion engine has noise reducing openings along the housing wall
09/18/2002EP1240411A1 Split ring for tip clearance control
09/18/2002EP1240410A1 Axial flow turbine type rotor machine for elastic fluid operation
09/17/2002US6450766 Stator vane blank and method of forming the vane blank
09/17/2002US6450763 Replaceable variable stator vane for gas turbines
09/17/2002US6450762 Integral aft seal for turbine applications
09/17/2002US6450759 Gas turbine nozzle vane insert and methods of installation
09/12/2002WO2002070867A1 Methods and apparatus for cooling gas turbine engine blade tips
09/12/2002US20020127111 Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine
09/12/2002US20020127101 Stator vane for an axial flow turbine
09/12/2002US20020127100 Low-pressure steam turbine with multi-channel diffuser
09/12/2002US20020127097 Turbine vane assembly including a low ductility vane
09/12/2002US20020127095 Gas turbine engine guide vane
09/11/2002EP1239131A2 Methods and apparatus for operating gas turbine engines
09/11/2002EP1239121A2 An air-cooled gas turbine exhaust casing
09/11/2002EP1239120A2 Gas turbine engine guide vane
09/11/2002EP1239119A1 Turbine vane assembly including a low ductility vane
09/11/2002EP1239118A2 Flexible cloth seal for turbine combustors
09/11/2002EP1239117A2 Gas turbine combustor transition piece outlet structure, transition piece, combustor and gas turbine
09/11/2002EP1239058A2 Coating for gas turbine blades
09/05/2002US20020122716 Methods and apparatus for cooling gas turbine engine blade tips
09/05/2002US20020121744 Low leakage flexible cloth seals for turbine combustors
09/05/2002US20020121082 Air-cooled gas turbine exhaust casing
09/03/2002US6443694 Rotor machine device
09/03/2002US6442946 Three degrees of freedom aft mounting system for gas turbine transition duct
08/2002
08/29/2002WO2002018674A3 Thermal barrier coating system for turbine components
08/29/2002US20020117854 Integrated compression sleeve
08/27/2002US6439841 Turbine frame assembly
08/27/2002US6439838 Periodic stator airfoils
08/27/2002US6439837 Nozzle braze backside cooling
08/27/2002US6439616 Anti-rotation retainer for a conduit
08/27/2002US6438938 Bearing compartment self cooling vent system
08/22/2002US20020114696 Gas turbine nozzle vane insert and methods of installation
08/22/2002US20020112483 Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure
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