Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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09/14/2005 | EP1573239A1 Honeycomb seal |
09/14/2005 | EP1573238A1 Sealing arrangement |
09/14/2005 | CN2725533Y High power steam turbine low pressure self crown carried long blade stepped surrounding belt |
09/13/2005 | US6942452 Grommeted bypass duct penetration |
09/13/2005 | US6942445 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
09/13/2005 | US6942203 Spring mass damper system for turbine shrouds |
09/09/2005 | WO2005071290A3 Traction drive shaft seal |
09/08/2005 | US20050196278 Turbine blade arrangement |
09/08/2005 | US20050196270 Device for axially holding a ring spacer sector of a high-pressure turbine of a turbomachine |
09/08/2005 | US20050196267 Method and apparatus for reducing self sealing flow in combined-cycle steam turbines |
09/08/2005 | US20050194747 Sealing arrangement |
09/08/2005 | US20050194745 Sealing arrangement in turbine machinery |
09/08/2005 | DE10393433T5 Bürstendichtungen verwendende Dichtungsanordnung Brush seals used seal assembly |
09/07/2005 | EP1571294A1 Hook-shaped sideplate for a rotor disc |
09/07/2005 | CN1664318A Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine |
09/07/2005 | CN1664317A Method and apparatus for reducing self sealing flow in combined-cycle steam turbines |
09/06/2005 | US6939106 Sealing of steam turbine nozzle hook leakages using a braided rope seal |
09/06/2005 | US6939104 Turbine blade with sealing element |
09/06/2005 | CA2239460C Circumferential seal with ceramic rotor |
09/01/2005 | WO2005059312A3 Turbomachine, especially a gas turbine |
09/01/2005 | US20050191182 Turbine blade shroud cutter tip |
09/01/2005 | US20050191171 Sealing element and pivoting motor |
09/01/2005 | US20050191166 Passive improved air turbine starter lubrication system |
09/01/2005 | US20050189723 Transition strip for covering layers on a support surface |
09/01/2005 | US20050189720 Dynamic seal for use in high-speed turbomachinery |
08/31/2005 | EP1568889A2 Shaft seal for use in high-speed turbomachinery |
08/31/2005 | EP1456508B1 Hot gas path subassembly of a gas turbine |
08/30/2005 | US6935837 Methods and apparatus for assembling gas turbine engines |
08/30/2005 | US6935836 Compressor casing with passive tip clearance control and endwall ovalization control |
08/30/2005 | US6935833 Recirculation structure for turbo chargers |
08/30/2005 | US6935631 Sheet brush seal |
08/30/2005 | CA2407155C Axis seal mechanism and turbine |
08/25/2005 | WO2005078242A1 Damping arrangement for guide vanes |
08/25/2005 | US20050186079 Gas turbine tip shroud rails |
08/25/2005 | US20050186074 Moving blade and gas turbine using the same |
08/25/2005 | DE102004006706A1 Damping arrangement for vanes, especially for vanes of a gas turbine or aircraft engine, comprises a spring element in the form of a leaf spring arranged between an inner shroud of the vanes and a seal support |
08/25/2005 | CA2555578A1 Damping arrangement for guide vanes |
08/24/2005 | EP1566531A1 Gas turbine with compressor casing protected against cooling and Method to operate a gas turbine |
08/24/2005 | EP1566530A1 Gas turbine |
08/24/2005 | EP1566524A2 Turbine casing cooling arrangement |
08/24/2005 | EP1566521A1 Seal device |
08/24/2005 | CN1657807A Seal device |
08/23/2005 | US6932575 Blade damper |
08/23/2005 | US6932567 Method and apparatus for controlling fluid leakage through gas turbine engines |
08/23/2005 | US6932566 Gas turbine shroud structure |
08/23/2005 | US6932349 Sealing system for gas turbine |
08/23/2005 | US6932347 Device for a non-hermetic seal |
08/23/2005 | CA2381664C Steam tube structure of gas turbine |
08/18/2005 | WO2005056878A8 Running-in coating for gas turbines and method for production thereof |
08/18/2005 | US20050179215 Seal device |
08/18/2005 | US20050179207 Compliant brush shroud assembly for gas turbine engine compressors |
08/18/2005 | DE102004004915A1 Dichtungsanordnung Seal assembly |
08/17/2005 | EP1564455A1 Sealing arrangement for the high-pressure turbine of a turbomachine |
08/17/2005 | CN1654785A Shroud honeycomb cutter |
08/16/2005 | CA2366717C Division wall and shroud of gas turbine |
08/11/2005 | WO2005073667A1 Inductive apparatus and method for measuring compressor blade tip clearance in a gas turbine engine |
08/11/2005 | WO2005073518A1 Sealing arrangement |
08/11/2005 | US20050175463 Control of leak zone under blade platform |
08/11/2005 | US20050175453 Shroud honeycomb cutter |
08/11/2005 | US20050175446 Compressor system with movable seal lands |
08/11/2005 | DE102004002943A1 Schichtsystem für eine Rotor-/Statordichtung einer Strömungsmaschine Layer system for a rotor / stator seal of a turbomachine |
08/10/2005 | EP1561904A2 Honeycomb cutting device for a blade shroud |
08/09/2005 | US6926495 Turbine blade tip clearance control device |
08/09/2005 | US6926284 Sealing arrangements |
08/09/2005 | US6925814 Hybrid turbine tip clearance control system |
08/04/2005 | WO2005071290A2 Traction drive shaft seal |
08/04/2005 | WO2005071229A1 Non-positive-displacement machine having an axially displaceable rotor |
08/04/2005 | WO2005071228A1 Layer system for a rotor/stator seal of a turbine machine, especially a gas turbine |
08/04/2005 | US20050169761 Rotor blade for a rotary machine |
08/04/2005 | US20050169749 Labyrinth seal device for gas turbine engine |
08/04/2005 | US20050167531 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors |
08/04/2005 | DE202005008606U1 Setting shaft fitting for supercharger has base body of setting shaft with stepped external outline and bush with complementary internal outline |
08/04/2005 | DE102004001722A1 Turbomaschinenschaufel und Verfahren zur Herstellung einer Schaufelspitzenpanzerung an Turbomaschinenschaufeln Turbomachine blade and method of producing a blade tip plating to turbomachinery blades |
08/03/2005 | EP1559873A2 Sealing arrangement for turbomachinery |
08/03/2005 | EP1559871A2 Rotor blade for a turbomachine |
08/03/2005 | EP1167188A4 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lrps), hybrid multifunction booster rocket with cruising lrps and development test therefor |
08/03/2005 | CN1650091A Device for fixing a rotor on a shaft |
08/03/2005 | CN1648416A Rotor blade for a rotary machine |
08/02/2005 | US6923005 System to feed cooling air into a gas turbine rotor |
08/02/2005 | CA2253601C Brush seal |
07/28/2005 | WO2005068786A1 Turbine blade and gas turbine equipped with a turbine blade of this type |
07/28/2005 | WO2005068785A1 Turbine blade and gas turbine equipped with a turbine blade of this type |
07/28/2005 | WO2005068784A1 Turbo machine blade and method for producing armour plating on the tips of turbo machine blades |
07/28/2005 | US20050163608 Gas turbine engine |
07/27/2005 | EP1557536A1 Gas turbine with axially displaceable rotor |
07/27/2005 | EP1557535A1 Turbine blade and gas turbine with such a turbine blade |
07/27/2005 | EP1557534A1 Turbine blade and gas turbine with such a turbine blade |
07/27/2005 | CN1646790A Recirculation structure for turbo chargers |
07/27/2005 | CN1644891A Turbine shroud asymmetrical cooling elements |
07/26/2005 | US6921079 Hydraulic seal arrangement |
07/21/2005 | US20050158572 Thermal spray compositions for abradable seals |
07/21/2005 | US20050158169 Gas turbine clearance control devices |
07/21/2005 | US20050158168 Methods and apparatus for coupling ceramic matrix composite turbine components |
07/21/2005 | US20050158166 Traction drive shaft seal |
07/21/2005 | US20050155454 Thermal spray compositions for abradable seals |
07/21/2005 | DE10360164A1 Gasturbinenbauteil Gas turbine component |
07/20/2005 | EP1555394A1 Device to control clearances in a gas turbine |
07/20/2005 | EP1555393A2 Gas turbine engine component having bypass circuit |
07/20/2005 | EP1555392A2 Cantilevered stator stage |
07/20/2005 | CN1643236A Turbine blade pocket shroud |