| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 02/02/2006 | DE102005032068A1 Laufschaufelspielkontrolle Blade game control |
| 02/02/2006 | DE102004034312A1 Dichtungsanordnung und Verfahren zur Herstellung eines Dichtkörpers für eine Dichtungsanordnung A sealing arrangement and method for manufacturing a sealing body for a sealing arrangement |
| 02/01/2006 | EP1621736A2 Wall structure for a hot gas flow path |
| 02/01/2006 | EP1621735A2 Gas turbine rotor |
| 02/01/2006 | EP1620632A1 Hub-centered brush seal arrangement for use in a gas turbine |
| 02/01/2006 | EP1299621B1 Drainage system for gas turbine supporting bearings |
| 02/01/2006 | CN1239811C Method and device for non-contact sealing between rotor and stator |
| 01/31/2006 | US6991429 Sealing structure of spindle bolt, and gas turbine |
| 01/31/2006 | US6991427 Casing section |
| 01/31/2006 | US6991235 Gas-buffered seal assembly and method therefor |
| 01/26/2006 | US20060016173 Securing arrangement |
| 01/25/2006 | EP1619355A1 Bearing and seal arrangement in a steam turbine |
| 01/25/2006 | EP1618287A1 Turbine bucket with curved aft shank walls for stress reduction |
| 01/25/2006 | CN1724851A Method and system for operating rotary machines |
| 01/24/2006 | US6988871 Heat sink attachment clip |
| 01/19/2006 | DE102004042258B3 Verfahren zur Herstellung eines Konturspalts sowie Strömungsmaschine mit einem Konturspalt A process for producing a contoured gap and flow machine with a contour gap |
| 01/19/2006 | DE102004031255A1 Einlaufbelag Inlet lining |
| 01/18/2006 | EP1617045A1 Skirted turbine blade |
| 01/18/2006 | CN1237258C 涡轮叶片 Turbine blades |
| 01/17/2006 | US6986253 Methods and apparatus for cooling gas turbine engine combustors |
| 01/12/2006 | US20060008347 Guide blade fixture in a flow channel of an aircraft gas turbine |
| 01/12/2006 | US20060006745 Integrated blower for cooling device |
| 01/12/2006 | US20060005529 Blade clearance control |
| 01/11/2006 | EP1614863A1 Fluid structure for a turbocompressor |
| 01/11/2006 | EP1614862A1 Gas turbine and gas turbine cooling and sealing method |
| 01/11/2006 | EP1613840A2 Impeller blades comprising different lengths and abrasive layers |
| 01/10/2006 | US6984106 Resilent seal on leading edge of turbine inner shroud |
| 01/09/2006 | CA2511635A1 Blade clearance control |
| 01/05/2006 | WO2006001825A2 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| 01/05/2006 | WO2006000174A1 Running-in coating |
| 01/05/2006 | US20060001218 Flexible bearing seal |
| 01/05/2006 | DE102005019823A1 Abriebbeschichtung für eine Turbine für niedrige/mittlere Temperatur Abrasion coating for a turbine for low / medium temperature |
| 01/05/2006 | CA2551016A1 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
| 01/03/2006 | US6981841 Triple circuit turbine cooling |
| 12/29/2005 | US20050287390 For gas turbine engines; mixture of metal-clad lubricant particles and another lubricant; powders |
| 12/29/2005 | US20050287002 Turbine vane collar seal |
| 12/29/2005 | US20050286995 Method and system for determining gas turbine tip clearance |
| 12/29/2005 | US20050285349 Dynamic bearing device |
| 12/29/2005 | US20050285345 Seal apparatus |
| 12/29/2005 | DE102005026318A1 Verfahren und Vorrichtung zur Herstellung von Gasturbinentriebwerken Method and apparatus for the production of gas turbine engines |
| 12/28/2005 | EP1609954A1 Securing arrangement |
| 12/28/2005 | EP1609953A1 Assembly method for a turbomachine |
| 12/28/2005 | EP1609952A1 Turbine vane collar seal |
| 12/28/2005 | CN1712674A Turbine vane collar seal |
| 12/22/2005 | US20050281694 Inner air seal anti-rotation device |
| 12/22/2005 | US20050281668 Low-mid turbine temperature abradable coating |
| 12/22/2005 | US20050280549 Proximity sensor |
| 12/22/2005 | DE102005024475A1 Verfahren zur Beschichtung von Gasturbinentriebwerkskomponenten A process for coating of gas turbine engine components |
| 12/22/2005 | DE102004025692A1 Brazing construction for abradable sealing material used in turbine, includes infiltration prevention agent which is filled on non-brazing side upto specific depth so as to restrict infiltration of brazing filler metals |
| 12/22/2005 | DE102004025142A1 Sealing arrangement for turbo-machine e.g. gas turbine has dynamic seal to seal gap between stator and rotor for primary leakage, first static seal for secondary leakage and second static seal for leakage between two seal carrier segments |
| 12/21/2005 | EP1607584A1 Control system and method to control the air flow in a gas turbine |
| 12/21/2005 | EP1607583A1 Method and system for operating rotary machines |
| 12/21/2005 | CN1711409A Shroud cooling assembly for a gas trubine |
| 12/21/2005 | CN1232761C Heat shielding device for hot fuel gas guide piece, particularly gas turbine structure piece |
| 12/21/2005 | CN1232720C Abradable seal |
| 12/20/2005 | US6976680 Shaft seal structure and turbine |
| 12/20/2005 | US6976679 Inter-fluid seal assembly and method therefor |
| 12/15/2005 | US20050276692 Lightened interblade platform for a turbojet blade support disc |
| 12/15/2005 | US20050276691 Inter-vane platform with lateral deflection for a vane support of a turbine engine |
| 12/15/2005 | US20050276690 System and method of controlling a flow of air in a gas turbine |
| 12/15/2005 | US20050276688 Shroud segment for a turbomachine |
| 12/15/2005 | US20050276687 Methods and apparatus for fabricating gas turbine engines |
| 12/15/2005 | CA2509488A1 System and process for monitoring airflow in a gas turbine |
| 12/14/2005 | CN1708598A Intermetallic material and use of said material |
| 12/08/2005 | US20050271505 Turbine engine shroud segment, hanger and assembly |
| 12/08/2005 | US20050271504 Seal system |
| 12/08/2005 | US20050271499 Methods and systems for operating rotary machines |
| 12/08/2005 | DE102004024080A1 Brush seal for use in e.g. static gas turbine, has interference units, fastenable to stator, concurring with interference recesses such that force is applied on each ring part, where force presses each ring part in stator |
| 12/08/2005 | CA2502805A1 Turbine engine shroud segment, hanger and assembly |
| 12/07/2005 | EP1602802A1 Seal system |
| 12/07/2005 | EP1601861A1 Sheet metal turbine or compressor static shroud |
| 12/07/2005 | CN1704561A Honeycomb contact steam seal |
| 12/06/2005 | US6971844 Horizontal joint sealing system for steam turbine diaphragm assemblies |
| 12/06/2005 | US6971841 Cellular materials |
| 12/01/2005 | WO2005114013A1 Sealing arrangement |
| 12/01/2005 | US20050265849 Turbine blade retainer seal |
| 12/01/2005 | US20050265847 Rotor assembly and annulus filler for gas turbine engine compressor |
| 12/01/2005 | US20050265831 Method for coating gas turbine engine components |
| 12/01/2005 | US20050265827 Passive clearance control |
| 12/01/2005 | US20050265826 Cellular materials |
| 12/01/2005 | US20050265825 Spacing arrangement |
| 12/01/2005 | US20050263643 Cowl structure for a gas turbine engine |
| 12/01/2005 | DE102004023130A1 Dichtungs- und Dämpfungssystem für Turbinenschaufeln Sealing and damping system for turbine blades |
| 11/30/2005 | EP1600607A2 Device to control the radial clearance of the rotor of a gas turbine |
| 11/30/2005 | EP1600606A1 Sealing and damping system for gas turbine blades |
| 11/30/2005 | EP1320662B1 Seal system |
| 11/30/2005 | EP1278943B1 Turbomachine with rotor-shroud seal structure |
| 11/29/2005 | US6969236 Fluid-cooled mechanical face seal rotor |
| 11/29/2005 | US6969231 Rotary machine sealing assembly |
| 11/29/2005 | US6968696 Part load blade tip clearance control |
| 11/25/2005 | CA2507192A1 Method for coating gas turbine engine components |
| 11/24/2005 | US20050260066 Turboshaft engine comprising two subassemblies assembled under axial stress |
| 11/22/2005 | US6966752 Casing ring |
| 11/22/2005 | US6966750 Gas turbine stationary blade |
| 11/22/2005 | US6966191 Device for supplying secondary air in a gas turbine engine |
| 11/17/2005 | US20050254940 Blade arrangement |
| 11/17/2005 | US20050254939 Arrangement for the automatic running gap control on a two or multi-stage turbine |
| 11/17/2005 | US20050253379 Threaded joint for gas turbine components |
| 11/17/2005 | US20050252000 Method and system for improved blade tip clearance in a gas turbine jet engine |
| 11/17/2005 | DE102004018994A1 Verfahren zur Herstellung einer Wabendichtung A process for producing a honeycomb seal |