Patents for F01D 9 - Stators (10,038)
03/2005
03/31/2005DE10311227B4 Leitapparat Diffuser
03/30/2005EP1519009A1 Turbomachine with cabin bleed air through a tube with ball joint
03/30/2005EP1519007A1 Gas turbine
03/30/2005CN1601067A Turbomachine with cabin bleed air through a tube with bi-ball joint
03/29/2005US6872047 Steam-cooling-type turbine
03/24/2005US20050063816 Transition duct honeycomb seal
03/23/2005EP1516106A1 Variable geometry turbocharger having internal bypass exhaust gas flow
03/23/2005CN2687344Y Vertical centrifugal pump series connected with suction type pressurized water well
03/22/2005US6869049 Method and apparatus for modulating flow separation
03/17/2005US20050058546 Vane apparatus for a gas turbine engine
03/17/2005US20050058541 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing
03/17/2005US20050058537 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
03/17/2005US20050056015 Exhaust-gas turbocharger for an internal combustion engine
03/16/2005EP1515002A1 Anti-rotation means for turbine stator vanes in the split plane of the casing
03/15/2005US6866477 Airfoil shape for a turbine nozzle
03/10/2005US20050053463 Exhaust-gas-turbine casing
03/10/2005US20050053462 Sealing of nozzles in a steam turbine
03/10/2005US20050053457 Turbine blade ring assembly and clocking method
03/09/2005CN2683858Y Horizontal flange beveled baffle plate of impulse-type steam turbine
03/08/2005US6863497 Stator vane span attachment for a gas turbine
03/03/2005US20050047907 Transition duct cooling system
03/03/2005US20050044708 Method for manufacturing a hollow blade for a stator or rotor component
03/02/2005EP1510659A2 Turbine airfoil cooling flow particle separator
03/02/2005EP1510654A1 Unitary turbine blade array and method to produce the unitary turbine blade array.
03/02/2005CN1589361A Gas turbo group
03/01/2005US6860718 Geothermal turbine
03/01/2005US6860717 Axial turbine for aeronautical applications
03/01/2005US6860716 Turbomachine frame structure
03/01/2005US6860108 Gas turbine tail tube seal and gas turbine using the same
02/2005
02/24/2005US20050042474 High-temperature protection layer
02/24/2005US20050042085 Arrangement for mounting a non-rotating component
02/24/2005US20050042083 Guide vane
02/24/2005US20050042081 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
02/24/2005US20050042079 Device for pivotally guiding variable-pitch vanes in a turbomachine
02/24/2005US20050042077 Sheet metal turbine or compressor static shroud
02/24/2005US20050040210 Method of joining ceramic or graphite to metal with an alloy having high nickel or cobalt content, alloys for joining the same, and products formed therewith
02/24/2005US20050039333 Method for manufacturing steam turbines
02/23/2005EP1508670A2 Cooled vane of a gas turbine
02/23/2005EP1507977A1 Discrete passage diffuser
02/23/2005EP1507959A1 Arrangement for axially and radially fixing the guide vanes of a vane ring of a gas turbine
02/22/2005US6857847 Simplified support device for nozzles of a gas turbine stage
02/17/2005US20050036885 Guide system for the outer pivot of a variable stator vane, for a turbojet stator
02/17/2005US20050035559 Inner air seal anti-rotation device
02/16/2005EP1507067A2 Inner air seal anti-rotation device
02/16/2005EP1507015A1 High-temperature member for use in gas turbine
02/16/2005EP1228293B1 Method for producing a turbine blade
02/16/2005CN1580500A Airfoil shape for a turbine nozzle
02/15/2005US6854738 Sealing structure for combustor liner
02/10/2005US20050031445 Cooling system for a turbine vane
02/10/2005US20050031444 Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
02/10/2005US20050028523 Turbocharger
02/10/2005US20050028340 Instrumented transition alignment fixture and method
02/09/2005EP1505259A1 An arrangement for mounting a non-rotating component of a gas turbine engine
02/09/2005CN1576611A Methods and apparatus for assembling gas turbine engines
02/08/2005US6851264 Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine
02/08/2005CA2299148C Compressor system and methods for reducing cooling airflow
02/03/2005WO2005010330A1 Turbocharger
02/03/2005WO2005010323A1 Device for fixing the blade root on a turbomachine
02/03/2005US20050025618 Airfoil shape for a turbine nozzle
02/03/2005US20050025617 Geothermal turbine
02/03/2005DE10331599A1 Bauteil für eine Gasturbine sowie Verfahren zur Herstellung desselben Of the same component for a gas turbine and processes for preparing
02/02/2005EP1503040A1 Lightweight inter-blade platform for a blade support disk of a turbo engine
02/02/2005EP1503037A2 Airfoil shape for a turbine nozzle
02/02/2005CN2675868Y Indexing device for separator stationary blade assembling
02/02/2005CN2675867Y Stationary integral blade separator of impulse steam turbine
02/02/2005CN1573119A Turbocharger
02/02/2005CN1573053A Turbomachine frame structure
02/02/2005CN1573052A Methods and apparatus for supplying cooling fluid to turbine nozzles
02/01/2005US6848884 Three-dimensional axial-flow turbine stage
02/01/2005CA2365090C Gas turbine
01/2005
01/27/2005WO2005008033A1 Cooling circuit for gas turbine fixed ring
01/27/2005WO2005008032A1 Lightweight blade for gas turbine and method for making same
01/27/2005US20050019158 Twin flow turbine housing
01/27/2005US20050019157 Axial flow turbine
01/27/2005US20050015980 Repair of combustion turbine components
01/27/2005DE10330169A1 Exhaust gas turbocharger for an internal combustion engine, has a blower and variable turbine geometry with a guide grid and guide vanes of a turbine
01/26/2005EP1500791A1 Guiding set for the external pivot of a variable angle vane system in a turbo engine
01/26/2005EP1500789A1 Impingement cooled ring segment of a gas turbine
01/26/2005EP1500788A1 Double flow scroll
01/25/2005US6847004 Process of removing a ceramic coating deposit in a surface hole of a component
01/25/2005US6846575 Article having turbulation and method of providing turbulation on an article
01/25/2005US6846156 Gas turbine
01/25/2005US6845558 Method of fabricating vanes
01/20/2005WO2005005888A1 Cooling structure of gas turbine tail pipe
01/20/2005WO2005005783A1 Steam turbine
01/20/2005US20050013693 Blade structure in a gas turbine
01/19/2005CN1568397A Methods and apparatus for cooling gas turbine engine blade tips
01/19/2005CN1568396A Second-stage turbine nozzle airfoil
01/18/2005US6844518 Hole-drilling guide and method
01/18/2005US6843637 Cooling circuit within a turbine nozzle and method of cooling a turbine nozzle
01/18/2005US6843479 Sealing of nozzle slashfaces in a steam turbine
01/13/2005WO2005003520A1 Turbine shroud segment
01/13/2005WO2005003518A1 Turbine shroud segment
01/13/2005US20050008486 Exit stator mounting
01/13/2005US20050008485 Turbine nozzle airfoil
01/13/2005US20050008480 Device for injecting cooling air into a turbine rotor
01/13/2005DE10328167A1 Turbinengehäuse für einen Abgasturbolader Turbine housing for an exhaust gas turbocharger
01/13/2005DE102004028158A1 Turbolader Turbocharger
01/12/2005EP1496208A1 Supporting pivot shafts of variable guide vanes for turbomachines
01/12/2005EP1496205A1 Cooled blade for a gas turbine engine
1 ... 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 ... 101