Patents for F01D 9 - Stators (10,038) |
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03/12/2002 | US6354795 Shroud cooling segment and assembly |
03/07/2002 | WO2002018674A2 Thermal barrier coating system for turbine components |
03/07/2002 | US20020028139 Stator vane assembly for a turbine and method for forming the assembly |
03/07/2002 | US20020028135 Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment |
03/07/2002 | US20020028134 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment |
03/07/2002 | DE10133679A1 Axial flow steam turbine has moisture extraction pocket for improved moisture extraction efficiency with moisture chamber, slot for connecting chamber to working fluid flow path |
03/05/2002 | US6352405 Interchangeable turbine diaphragm halves and related support system |
02/28/2002 | US20020025248 Method for enhancing heat transfer inside a turbulated cooling passage |
02/27/2002 | EP1181438A1 Radial turbo-machine |
02/27/2002 | CN1079895C Wet purification method and device of spray nozzle ring of exhaust steam turbocharger-pulley machine |
02/21/2002 | WO2002014654A1 Turbine vane system |
02/21/2002 | US20020021966 Method and apparatus for cooling a wall within a gas turbine engine |
02/21/2002 | US20020020168 Turbojet power plant with heat exchanger |
02/20/2002 | EP1180581A2 Interchangeable turbine diaphragm halves and related support system |
02/20/2002 | EP1180578A1 Statoric blades for a turbomachine |
02/20/2002 | EP1180577A2 Cooling method for a turbine rotor |
02/20/2002 | EP0835363B1 Active automatic clamping control |
02/20/2002 | CN1079491C Turbine shaft and process for cooling same |
02/14/2002 | WO2002012680A1 Suspension |
02/14/2002 | US20020018489 Gigabit switch supporting improved layer 3 switching |
02/14/2002 | DE10037684A1 Niederdruckdampfturbine mit Mehrkanal-Diffusor Low pressure steam turbine with multi-channel diffuser |
02/14/2002 | CA2391082A1 Suspension |
02/12/2002 | US6345955 Bowed nozzle vane with selective TBC |
02/12/2002 | US6345494 Side seal for combustor transitions |
02/12/2002 | CA2229883C Gas turbine shroud and platform seal system |
02/06/2002 | EP1178183A2 Low pressure steam turbine with multi channel diffuser |
02/06/2002 | EP1178182A1 Gas turbine split ring |
02/05/2002 | US6343912 Gas turbine or jet engine stator vane frame |
02/05/2002 | US6343911 Side wall cooling for nozzle segments for a gas turbine |
02/05/2002 | US6343463 Support and locking device for nozzles of a high pressure stage of a gas turbines |
01/31/2002 | US20020012585 Gigabit switch with fast filtering processor |
01/31/2002 | US20020012345 Cascading of gigabit switches |
01/31/2002 | DE10135204A1 Turbinendüsendeckelstützsystem Turbine nozzle cover support system |
01/30/2002 | EP1176285A2 Shroud cooling segment and assembly |
01/30/2002 | EP1176284A2 Brazeless fillet turbine nozzle |
01/24/2002 | WO2002006637A1 Variable nozzle turbocharger with sheet metal shroud |
01/24/2002 | US20020010791 Trunking and mirroring across stacked gigabit switches |
01/24/2002 | US20020009090 Flexible header protocol for network switch |
01/24/2002 | US20020009084 Gigabit switch supporting multiple stacking configurations |
01/24/2002 | US20020009083 Gigabit switch with multicast handling |
01/24/2002 | US20020009081 Gigabit switch with frame forwarding and address learning |
01/24/2002 | DE10033465A1 Turbine rotor, for a motor turbo-charger, has paddles held in place by pins between the rotor sides to give easy and rapid changes to the paddle structure |
01/24/2002 | DE10029060A1 Turboluftstrahltriebwerk mit Wärmetauscher Turbojet engine with heat exchanger |
01/23/2002 | EP1173664A1 Cooling air system |
01/23/2002 | EP1173657A1 Turbine blade and method for producing a turbine blade |
01/22/2002 | US6340285 End rail cooling for combined high and low pressure turbine shroud |
01/22/2002 | CA2047275C Fully floating inlet flow guide for double-flow low pressure steam turbines |
01/17/2002 | WO2001051771A3 Array for regulating the diameter of a stator of a gas turbine |
01/17/2002 | US20020006329 Nozzle airfoil having movable nozzle ribs |
01/17/2002 | DE10032454A1 Vorrichtung zum Kühlen eines ungleichmäßig stark temperaturbelasteten Bauteiles Apparatus for cooling an uneven strongly temperature-loaded component |
01/16/2002 | EP1172524A2 Method for deploying shroud segments of different thickness in a turbine engine |
01/15/2002 | US6339208 Method of forming cooling holes |
01/10/2002 | WO2002002912A1 Draining and cooling system for gas turbine cushions |
01/10/2002 | WO2002002911A1 Connecting system for a transition duct in a gas turbine |
01/10/2002 | US20020004003 Device for cooling a component subject to temperature stress of nonuniform intensity |
01/09/2002 | EP1170464A2 Cooling device for an element with an unequal thermal charge |
01/09/2002 | EP0760051B2 Airfoil with dual source cooling |
01/09/2002 | CN1330209A Turbomachine blade unit |
01/09/2002 | CN1330208A Guide blade with consistent base |
01/08/2002 | US6336790 Axial flow power tool turbine machine |
01/08/2002 | CA2230325C Steam cooled gas turbine system |
01/02/2002 | EP1167694A2 Cooled nozzle vane |
01/02/2002 | EP1167693A2 Guide vane platforms |
01/01/2002 | US6334310 Fracture resistant support structure for a hula seal in a turbine combustor and related method |
01/01/2002 | CA2251198C Gas turbine stationary blade |
01/01/2002 | CA2251192C Gas turbine stationary blade double cross type seal device |
12/25/2001 | US6332754 Steam turbine |
12/20/2001 | WO2001096712A1 Transition piece for non-annular gas turbine combustion chambers |
12/20/2001 | US20010052230 Fuel preheating in a gas turbine |
12/20/2001 | DE10028161A1 Exhaust turbocharger turbine casing cast by thin walled precision casting |
12/20/2001 | DE10028160A1 Casing assembly for exhaust turbocharger turbine made of thin metal sheet and surrounded by insulation |
12/19/2001 | EP1164273A2 Turbo jet engine with heat exchanger |
12/19/2001 | EP1164252A2 Support pedestals for a wall cover in a gas turbine nozzle segment |
12/19/2001 | EP1164250A2 Floating connector for an impingement insert |
12/19/2001 | EP1163429A1 Sealing device for segmented stator ring |
12/19/2001 | EP1163428A1 Guide blade and guide blade rim for a fluid-flow machine and component for delimiting a flow channel |
12/19/2001 | EP0988441B1 Combustion turbine cooling panel |
12/18/2001 | US6331110 External dilution air tuning for dry low NOx combustors and methods therefor |
12/18/2001 | US6331096 Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment |
12/18/2001 | CA2076083C Flow activated flowpath liner seal |
12/13/2001 | WO2001094755A1 Turbine casing for an exhaust turbocharger made by casting |
12/13/2001 | WO2001094754A1 Casing assembly for the turbine of an exhaust turbocharger |
12/13/2001 | US20010051095 Turbine nozzle stage having thermocouple guide tube |
12/12/2001 | EP1162798A2 Packet forwarding among different types of gigabit switches |
12/12/2001 | EP1162797A2 Flexible header protocol for network switch |
12/12/2001 | EP1162796A2 Cascading of gigabit switches |
12/12/2001 | EP1162795A2 Gigabit switch supporting improved layer 3 switching |
12/12/2001 | EP1162794A2 Gigabit switch with fast filtering processor |
12/12/2001 | EP1162793A2 Gigabit switch with multicast handling |
12/12/2001 | EP1162792A2 Gigabit switch with frame forwarding and address learning |
12/12/2001 | EP1162788A2 Trunking and mirroring across stacked gigabit switches |
12/12/2001 | EP1162346A2 Cooling for turbine shroud segments |
12/12/2001 | CN1076075C Method and device for cooling the low-pressure stage of a steam turbine |
12/11/2001 | CA2256597C Steam cooled type gas turbine |
12/05/2001 | EP1160512A2 Fracture resistant support structure for a hula seal in a turbine combustor and related method |
12/05/2001 | EP1160418A2 Steam exit flow design for aft cavities of an airfoil |
12/05/2001 | CN1324981A Nozzle-regulation mechanism of volume-variable turbomachine |
12/04/2001 | US6325596 Turbine diaphragm support system |
12/04/2001 | US6325593 Ceramic turbine airfoils with cooled trailing edge blocks |
11/29/2001 | US20010046651 External dilution air tuning for dry low NOX combustors and methods therefor |