Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
01/2002
01/22/2002US6340285 End rail cooling for combined high and low pressure turbine shroud
01/22/2002CA2047275C Fully floating inlet flow guide for double-flow low pressure steam turbines
01/17/2002WO2002004819A1 Accumulator/oil tank for journal oil supply
01/17/2002WO2001051771A3 Array for regulating the diameter of a stator of a gas turbine
01/17/2002US20020006329 Nozzle airfoil having movable nozzle ribs
01/17/2002US20020005038 Method and apparatus for the cooling of jet-engine turbine casings
01/17/2002DE10032454A1 Vorrichtung zum Kühlen eines ungleichmäßig stark temperaturbelasteten Bauteiles Apparatus for cooling an uneven strongly temperature-loaded component
01/16/2002EP1171691A1 Frangible cover for turbofan engine blade removal and access
01/15/2002US6338578 Retaining arrangement for a bearing, in particular for a high pressure compressor shaft
01/15/2002CA2065679C Shroud cooling assembly for gas turbine engine
01/10/2002WO2002003024A1 Play measuring sensor by multiple depth abrasion
01/10/2002WO2002002913A1 Drainage system for gas turbine supporting bearings
01/10/2002WO2002002912A1 Draining and cooling system for gas turbine cushions
01/10/2002WO2002002911A1 Connecting system for a transition duct in a gas turbine
01/10/2002US20020004005 Gas turbine engine blade containment assembly
01/10/2002US20020004003 Device for cooling a component subject to temperature stress of nonuniform intensity
01/10/2002US20020004002 Turbo machines
01/09/2002EP1170571A1 Sensor to measure play by multi-stage abrasion
01/09/2002EP1170520A2 Rolling element bearing provided with a squeeze film damper
01/09/2002EP1170464A2 Cooling device for an element with an unequal thermal charge
01/09/2002EP1170207A2 Link component for aircraft engine mounting systems
01/09/2002EP1169586A1 Brush seals for steam turbine applications
01/09/2002EP1169585A1 Self-centering brush seal
01/09/2002CN2470603Y Multi-spline oil-scraper ring
01/09/2002CN1330747A Device for connecting conduit sections
01/09/2002CN1330134A Nickel compound used as vanadium corrosion inhibitor and burning method using it
01/08/2002US6336790 Axial flow power tool turbine machine
01/08/2002US6336789 Casing for a steam or gas turbine
01/03/2002US20020000343 Apparatus for damping acoustic vibrations in a combustor
01/03/2002DE10029640A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine
01/02/2002EP1167882A1 Methods and apparatus for decreasing combustor emissions with spray bar assembly
01/02/2002EP1167788A1 Sealing device of a squeeze film damper incorporated in a rolling element bearing
01/02/2002EP1167754A2 Turning device for the rotor of a wind turbine
01/02/2002EP1167697A1 Turbine engine
01/02/2002EP1167691A2 Blade damper and method for making same
01/02/2002EP1165942A1 Turbo-engine with an array of wall elements that can be cooled and method for cooling an array of wall elements
01/02/2002CN1329696A Rotor blade of wind driven generator
01/01/2002US6334295 Rotating diffuser for pressure recovery in a steam cooling circuit of a gas turbine
01/01/2002CA2053038C Temperature control of a steam turbine steam to minimize thermal stress
12/2001
12/27/2001WO2001098437A1 Use of nickel compounds as vanadium corrosion inhibitors
12/27/2001WO2001098232A1 Protective coating including porouos silicon nitride matrix and noble metal
12/25/2001US6332754 Steam turbine
12/25/2001US6332272 Method of repairing a turbine blade
12/20/2001WO2001096713A1 Exhaust gas turbocharger for an internal combustion engine
12/20/2001US20010053329 Exhaust-gas turbocharger for an internal combustion engine
12/20/2001DE10028161A1 Exhaust turbocharger turbine casing cast by thin walled precision casting
12/20/2001DE10028160A1 Casing assembly for exhaust turbocharger turbine made of thin metal sheet and surrounded by insulation
12/20/2001DE10019437A1 Verfahren und Vorrichtung zum Kühlen der Gehäuse von Turbinen von Strahltriebwerken Method and apparatus for cooling the housing of turbines of jet engines
12/19/2001EP1164253A1 Cooling system for the shroud of paired rotor blades
12/19/2001EP1164252A2 Support pedestals for a wall cover in a gas turbine nozzle segment
12/19/2001EP1163430A1 Covering element and arrangement with a covering element and a support structure
12/19/2001EP0928365B1 Steam turbine, steam turbine plant and method of cooling a steam turbine
12/19/2001CN1076430C Heat recovery gas turbine rotor
12/18/2001US6331096 Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment
12/18/2001US6331078 Turbine engine bearing
12/18/2001US6330985 Link component for aircraft engine mounting systems
12/18/2001US6330790 Oil sump buffer seal
12/13/2001WO2001094756A2 Steam turbine with a divided housing
12/13/2001WO2001094755A1 Turbine casing for an exhaust turbocharger made by casting
12/13/2001WO2001094754A1 Casing assembly for the turbine of an exhaust turbocharger
12/12/2001EP1162347A1 Steam turbine with a splitted casing
12/12/2001EP1162346A2 Cooling for turbine shroud segments
12/12/2001EP1090222B1 Driving mechanism with counter-rotating rotors
12/12/2001CN1076075C Method and device for cooling the low-pressure stage of a steam turbine
12/11/2001US6328810 Removing loose contamination from hardware surfaces; selectively applying reactive metal and filler to preselected portion of hardware surfaces; heating to cause reaction between combustion products and reactive metal; cooling
12/11/2001US6327857 Device, method and application in connection with a turbomachine and pumping and lubricating arrangement in connection with such a machine
12/11/2001US6327844 Methods and apparatus for retaining flow restrictors within turbine engines
12/06/2001WO2001092689A1 Method and device for operating a steam turbine comprising several no-load or light-load phases
12/06/2001WO2001091932A1 Methods for foam cleaning combustion turbines
12/06/2001WO2001057364A8 Frangible cover for turbofan engine blade removal and access
12/06/2001US20010048878 Cooling circuit for a gas turbine bucket and tip shroud
12/06/2001US20010048876 Casing structure of metal construction
12/06/2001US20010047651 Device for supplying seal air to bearing boxes of a gas turbine engine
12/06/2001US20010047647 Process and device for lubricating an aircraft engine
12/05/2001EP1160551A1 Sensors and methodology for improved turbine exhaust gas temperature measurements
12/05/2001EP1160424A2 Silencer with internal rain diverter
12/05/2001EP1160419A1 Lubricating device for aeronautical engine
12/05/2001EP1160418A2 Steam exit flow design for aft cavities of an airfoil
12/04/2001US6325596 Turbine diaphragm support system
12/04/2001US6325546 Fan assembly support system
12/04/2001US6325380 Face seal assembly
11/2001
11/30/2001CA2349133A1 Silencer with internal rain diverter
11/29/2001US20010046441 Axial thermal medium delivery tubes and retention plates for a gas turbine rotor
11/29/2001DE10026121A1 Vorrichtung zur Dämpfung akustischer Schwingungen in einer Brennkammer Apparatus for damping acoustic vibrations in a combustion chamber
11/29/2001DE10025500A1 Internal combustion engine has additional wall for turbine housing creating hollow space which has inlet and outlet connection for intake and discharge of heat-absorbing cooling fluid upstream of heat exchanger
11/28/2001EP1158247A2 Apparatus to reduce acoustic vibrations in a combustion chamber
11/28/2001EP1158142A2 Reducing cracking adjacent shell flange connecting bolts
11/28/2001EP1158140A2 Exit joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
11/28/2001EP1156962A2 Tangentially directed acoustic jet controlling boundary layers
11/27/2001US6322321 Nozzle chamber warming-up structure for a steam turbine
11/27/2001US6322320 Coolable casing of a gas turbine or the like
11/27/2001US6322081 Circumferential seal with ceramic rotor
11/27/2001US6321528 Turbine, for a liquid-propellant rocket engine mainly
11/27/2001US6321449 Method of forming hollow channels within a component
11/22/2001WO2001088355A1 Method for remote monitoring of gas turbine
11/22/2001WO2001088354A2 Device for controlling the cooling flows of gas turbines
11/21/2001EP1156189A1 Turbine blade, turbine and operating method of a turbine
11/21/2001EP1156188A2 A leaf seal for gas turbine stator shrouds and a nozzle band
11/21/2001EP1156187A2 Nozzle cavity insert having impingement and convection cooling regions
11/21/2001EP1156186A2 Film cooling air pocket in a closed loop cooled airfoil