| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 07/19/2005 | US6918743 Sheet metal turbine or compressor static shroud |
| 07/19/2005 | US6918739 Seal support |
| 07/19/2005 | US6918598 Hot air seal |
| 07/19/2005 | US6918594 Face seal assembly with composite stator |
| 07/19/2005 | US6918252 Method of and apparatus for cooling a seal for machinery |
| 07/14/2005 | US20050152778 For the axial compressor of a gas turbine engine in which the stator tips rub against an abrasive section on the rotor drum during initial running of the engine to abrade the tips of the stator to provide optimised stator tip running clearance |
| 07/14/2005 | US20050152777 Resilent seal on leading edge of turbine inner shroud |
| 07/14/2005 | US20050151324 Sealing device for a high-pressure turbine of a turbomachine |
| 07/14/2005 | US20050150234 Gas turbine engine component having bypass circuit |
| 07/14/2005 | DE10359730A1 Turbomaschine, insbesondere Gasturbine Turbo machine, in particular gas turbine |
| 07/13/2005 | EP1552111A1 Gas turbine ventilation circuitry |
| 07/13/2005 | CN2709716Y Floating ring honey comb oil seal |
| 07/12/2005 | US6916529 Alloy of chromium, aluminum, and yttrium, with either cobalt, nickel or iron; monolithic intermetallic beta NiAl; increases the brittle nature of the metal matrix |
| 07/12/2005 | US6916154 Diametrically energized piston ring |
| 07/12/2005 | US6916021 Sealing arrangement |
| 07/07/2005 | WO2005061855A1 Gas turbine component |
| 07/07/2005 | WO2005061854A1 Gas turbine tip shroud rails |
| 07/07/2005 | US20050149274 Method and system for active tip clearance control in turbines |
| 07/07/2005 | CA2547619A1 Gas turbine component |
| 07/06/2005 | EP1550791A2 Method and system for active tip clearance control in turbines |
| 07/06/2005 | EP1165941B1 High temperature erosion resistant, abradable thermal barrier composite coating |
| 07/05/2005 | US6914210 Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
| 06/30/2005 | WO2005059312A2 Turbomachine, especially a gas turbine |
| 06/30/2005 | DE10356953A1 Einlaufbelag für Gasturbinen sowie Verfahren zur Herstellung desselben The same run-in coating for gas turbine and processes for preparing |
| 06/30/2005 | DE10352790A1 Turbo machine e.g. gas turbine engine, components` determining method for aircraft, involves determining operational geometry of gap from nominal geometry and total displacement vector of gap |
| 06/30/2005 | CA2548489A1 Turbomachine, especially a gas turbine |
| 06/29/2005 | CN1632290A Sealed wheel bucket type steam turbine |
| 06/28/2005 | US6910858 Seal |
| 06/28/2005 | US6910857 Seal |
| 06/28/2005 | US6910856 Run-in coating for axial-flow compressor of gas turbine engines and method of using and making same |
| 06/28/2005 | US6910854 Leak resistant vane cluster |
| 06/28/2005 | US6910853 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion |
| 06/28/2005 | US6910851 Turbofan jet engine having a turbine case cooling valve |
| 06/28/2005 | US6910619 Brazing of alumina coated honeycomb and fiber metal |
| 06/23/2005 | WO2005056985A1 Use of a thermal insulating layer for a housing of a steam turbine and a steam turbine |
| 06/23/2005 | WO2005056878A2 Running-in coating for gas turbines and method for production thereof |
| 06/23/2005 | US20050135925 Gas turbine stationary blade |
| 06/23/2005 | US20050132706 Device for supplying secondary air in a gas turbine engine |
| 06/23/2005 | US20050132570 Methods and apparatus for machining components |
| 06/23/2005 | DE10353810A1 Innendeckband für die Statorschaufeln des Verdichters einer Gasturbine Inner shroud for the stator blades of the compressor of a gas turbine |
| 06/23/2005 | DE10351583A1 Sealing arrangement for sealing the annular gap between the housing and the fixed vane ring of a gas turbine comprises a sealing device formed as a brush seal |
| 06/23/2005 | DE102004056528A1 Rippendichtung für Turbomaschinen Fin seal for turbomachinery |
| 06/23/2005 | CA2547530A1 Running-in coating for gas turbines and method for production thereof |
| 06/22/2005 | EP1543918A2 Holding Device for Gas Turbine Rotor Blades and Machine Tool incorporating such a device |
| 06/18/2005 | CA2489629A1 Methods and apparatus for machining components |
| 06/16/2005 | US20050129976 An aluminum plate having a purity of 99.5% or more, is caused to contact at least one side of a ceramic substrate of aluminum nitride or alumina to be heated at a temperature of 620 to 650 degrees C. in an inert gas to bond the aluminum plate directly to the ceramic substrate, power modules |
| 06/16/2005 | US20050129525 Sealing arrangement for a rotor of a turbo machine |
| 06/16/2005 | US20050129503 Small-sized hydroelectric generator |
| 06/16/2005 | US20050129499 Gas turbine high temperature turbine blade outer air seal assembly |
| 06/16/2005 | US20050126181 Hybrid turbine tip clearance control system |
| 06/16/2005 | US20050125983 Method of manufacturing axis seals, axis seals, axis seal members and rotary machine using axis seals |
| 06/16/2005 | DE102004055760A1 Dichtungsanordnung für eine Turbine, Schaufel, dieselbe enthaltende Turbine, Verfahren zum Abdichten des Zwischenraums zwischen den rotierenden und stationären Komponenten einer Turbine A sealing arrangement for a turbine blade, turbine containing the same, methods for sealing the gap between the rotating and stationary components of a turbine |
| 06/15/2005 | EP1541810A1 Use of a thermal barrier coating for a part of a steam turbine and a steam turbine |
| 06/15/2005 | EP1541809A2 Cooled platform for a nozzle guide vane |
| 06/15/2005 | EP1541807A2 Use of spray coatings to achieve non-uniform seal clearances in turbomachinery |
| 06/15/2005 | EP1541806A2 Improved tip sealing for turbine rotor blade |
| 06/15/2005 | EP1244881B1 Brush seals |
| 06/15/2005 | CN2704687Y Cavitation rotor turbines |
| 06/15/2005 | CN1626791A Small-sized hydroelectric generator |
| 06/15/2005 | CN1626774A Use of spray coatings to achieve non-uniform seal clearances in turbo machinery |
| 06/14/2005 | US6905305 Engine casing with slots and abradable lining |
| 06/14/2005 | US6905302 Network cooled coated wall |
| 06/09/2005 | WO2005040580A3 Fluid-cooled mechanical face seal rotor |
| 06/09/2005 | US20050123405 Sealing arrangement for an axial turbine wheel |
| 06/09/2005 | US20050123389 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| 06/09/2005 | US20050123388 Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
| 06/09/2005 | US20050121905 Sealing device for connection of a pipe in a hole |
| 06/09/2005 | DE102004049117A1 Dichtungsanordnung unter Verwendung flexibler Dichtungen Seal assembly using flexible seals |
| 06/08/2005 | EP1538306A1 Joining device between a vane and its cooling fluid supply in a turbomachine |
| 06/08/2005 | EP1537349A1 Multidirectional turbine shim seal |
| 06/08/2005 | EP1537297A1 Biased wear resistant turbine seal assembly |
| 06/08/2005 | EP1537296A1 Gas turbine sealing air supply system |
| 06/08/2005 | CN1624299A Method and apparatus for convective cooling of side-walls of turbine nozzle segments |
| 06/02/2005 | WO2005049971A1 Turbine tip clearance control system |
| 06/02/2005 | WO2005049312A1 High-temperature layered system for dissipating heat and method for producing said system |
| 06/02/2005 | US20050118016 Gas turbine arrangement |
| 06/02/2005 | US20050116425 Finned seals for turbomachinery |
| 06/02/2005 | US20050116061 Method and apparatus for arresting a crack within a body |
| 06/02/2005 | CA2546501A1 Turbine tip clearance control system |
| 06/01/2005 | EP1536103A1 Turbo machine having inlet guide vanes and attachment arrangement therefor |
| 06/01/2005 | EP1536101A2 Turbine drum rotor for a turbine engine and method of installation |
| 05/31/2005 | US6899520 Methods and apparatus to reduce seal rubbing within gas turbine engines |
| 05/31/2005 | US6899518 Turbine shroud segment apparatus for reusing cooling air |
| 05/31/2005 | US6899339 Abradable seal having improved durability |
| 05/26/2005 | US20050114082 Method and apparatus for detecting rub in a turbomachine |
| 05/26/2005 | US20050111980 Cooled turbine rotor wheel, in particular, a high-pressure turbine rotor wheel for an aircraft engine |
| 05/26/2005 | US20050111976 Dual coolant turbine blade |
| 05/26/2005 | US20050111970 Turbine durm rotor for a turbine engine |
| 05/26/2005 | US20050111967 Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine |
| 05/26/2005 | US20050111965 Turbine shroud asymmetrical cooling elements |
| 05/26/2005 | US20050111964 Triple circuit turbine cooling |
| 05/26/2005 | US20050110218 Seal arrangement |
| 05/26/2005 | US20050109039 Blade tip clearance control |
| 05/26/2005 | US20050109016 Turbine tip clearance control system |
| 05/25/2005 | EP1533479A2 Method and apparatus for detecting rub in a turbomachine |
| 05/25/2005 | EP1533478A2 Turbine shroud asymmetrical cooling elements |
| 05/25/2005 | EP1533477A2 Dual coolant turbine blade |
| 05/25/2005 | EP1533473A1 Triple circuit turbine cooling |
| 05/25/2005 | EP1533113A1 High temperature layered system for heat dissipation and method for making it |
| 05/25/2005 | CN1619109A Seal assembly and method for sealing interface between rotating and stationary components of a turbine |