Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages
Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581)
08/2003
08/27/2003CN1119503C Sealing device and use of sealing device
08/26/2003US6610416 Material treatment for reduced cutting energy and improved temperature capability of honeycomb seals
08/26/2003US6609888 Method and apparatus for reducing contamination in an axial compressor
08/26/2003US6609886 Composite tubular woven seal for gas turbine nozzle and shroud interface
08/26/2003US6609885 Supplemental seal for the chordal hinge seal in a gas turbine
08/26/2003US6609882 Device for compensating for an axial thrust in a turbo engine
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
08/20/2003EP1248924B1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
08/20/2003EP1177367B1 Seal for sealing a gap, in particular in a turbine, and a turbine
08/20/2003EP1163430B1 Covering element and arrangement with a covering element and a support structure
08/19/2003US6607350 Gas turbine engine system
08/19/2003CA2264996C Sealing device for axial flow turbine
08/19/2003CA2263508C Sealing device for gas turbine stator blades
08/14/2003US20030152457 Gas turbine engine and a rotor for a gas turbine engine
08/14/2003US20030152455 Engine casing
08/12/2003US6604286 Method of fabricating gas turbine fuel injection
08/07/2003WO2003064818A2 Geothermal steam turbine
08/05/2003US6602050 Covering element and arrangement with a covering element and a support structure
08/05/2003US6602048 Gas turbine split ring
08/05/2003CA2263576C Stationary blade of gas turbine
07/2003
07/31/2003US20030143069 Steam turbine and power generating equipment
07/30/2003EP1331364A2 Flexible coupling of a service tube to a dual shell bearing housing
07/30/2003EP1331362A2 Geothermal steam turbine
07/30/2003CN1116500C Seal ring for steam turbine
07/29/2003US6599089 Supplemental seal for the chordal hinge seal in a gas turbine
07/29/2003US6599088 Dynamically sealing ring fan shroud assembly
07/29/2003US6599087 Actuator shaft seal for variable nozzle turbocharger
07/24/2003US20030138319 Draining and cooling system for gas turbine cushions
07/23/2003EP1329594A1 Blade tip clearance control of a gas turbine
07/23/2003CN1431387A Rotation axis sealer and helium gas turbine generating system using same
07/22/2003US6595745 Supplemental seal for the chordal hinge seals in a gas turbine
07/22/2003US6595741 Pre-swirl nozzle carrier
07/17/2003US20030133793 Cloth seal for an inner compressor discharge case and methods of locating the seal in situ
07/17/2003US20030133790 Turbine shroud segment and shroud assembly
07/17/2003US20030132119 Turbine and manufacturing method therefor
07/17/2003US20030131980 Multiple impingement cooled structure
07/17/2003US20030131602 Turbine power plant having an axially loaded floating brush seal
07/16/2003EP1327802A2 Hydraulic sealing arrangement
07/16/2003EP1327748A1 Seal for gas turbine nozzle and shroud interface
07/15/2003US6592331 Reinforcement ring for the tower of an wind energy facility
07/15/2003US6592326 Connecting stator elements
07/09/2003EP0983421B1 Laser segmented thick thermal barrier coatings for turbine shrouds
07/08/2003US6589012 Method and apparatus for eliminating thermal bowing using brush seals in the diaphragm packing area of steam turbines
07/08/2003US6588214 Wear reduction means for a gas turbine combustor transition duct end frame
07/03/2003WO2003054360A1 Hot gas path subassembly of a gas turbine
07/03/2003WO2003054359A1 Sealing module for components of a turbo-engine
07/03/2003WO2003054358A1 Gas turbine assembly
07/03/2003US20030123982 Supplemental seal for the chordal hinge seal in a gas turbine
07/03/2003US20030123981 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030123980 Supplemental seal for the chordal hinge seal in a gas turbine
07/03/2003US20030123979 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030123978 Composite tubular woven seal for gas turbine nozzle and shroud interface
07/03/2003US20030122325 Seal for gas turbine nozzle and shroud interface
07/03/2003US20030122321 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122320 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122316 Supplemental seal for the chordal hinge seal in a gas turbine
07/03/2003US20030122312 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122311 Method of forming and installing a seal
07/03/2003US20030122310 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122309 Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation
07/02/2003EP1323957A2 Composite tubular woven seal for gas turbine nozzle and shroud interface
07/02/2003EP1323901A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323900A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323899A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323898A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323897A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323896A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323895A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323894A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323893A2 A method of forming and installing a seal into a turbomachine
07/02/2003EP1323892A2 Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation
07/02/2003EP1323891A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323890A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003CN1427921A System for sealing off gap
07/02/2003CN1427140A Flexibly jointed double casing type bearing seat
07/01/2003US6585479 Casing treatment for compressors
06/2003
06/26/2003WO2003052240A2 Gas turbine system
06/25/2003EP1320662A1 Seal system
06/24/2003US6582195 Compressor rotor blade spacer apparatus
06/24/2003US6582189 Turbo machines
06/24/2003US6581881 Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method for refining it
06/19/2003US20030113207 Structure for separating the high and low pressure turboexpanders of a gas turbine
06/19/2003US20030111797 Laminated finger seal with ceramic composition
06/19/2003US20030110778 Flexibly coupled dual shell bearing housing
06/17/2003US6579065 Methods and apparatus for limiting fluid flow between adjacent rotor blades
06/12/2003US20030107181 System for sealing off a gap
06/12/2003US20030106214 Method of retrofitting seals in a gas turbine
06/11/2003EP1318275A2 Structure for separating the high and low pressure turboexpanders of a gas turbine
06/11/2003EP0981703B1 Brush-hair seal
06/10/2003US6575704 Turbomachine and sealing element for a rotor thereof
06/10/2003US6575703 Turbine disk side plate
06/10/2003US6575699 Gas turbine engine and a rotor for a gas turbine engine
06/10/2003US6575698 Sealing of a thermal turbomachine
06/10/2003US6575697 Device for fixing a turbine ferrule
06/10/2003US6575693 Labyrinth seal for rotating shaft
06/10/2003US6574965 Rotor tip bleed in gas turbine engines
06/05/2003US20030103844 Turbine air seal replacement rings
06/05/2003US20030102630 Actuated brush seal
06/05/2003US20030102629 Brush seal coil for rotary machinery and method of retrofitting
06/05/2003US20030102409 Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (LRES), multifunctional launch vehicle of combined scheme with cruise LRES and method for refining it
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