Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
---|
04/13/2010 | CA2486237C Method and apparatus for arresting a crack within a body |
04/07/2010 | EP2171219A2 Variable geometry turbocharger |
04/07/2010 | EP2171216A2 Closed-loop control for a gas turbine with actively stabilized compressor |
04/07/2010 | CN101691844A Energy-saving system for power plant |
04/06/2010 | CA2353686C Sealing ring for non-hermetic fluid seals |
04/01/2010 | US20100080691 Magnetic adjustment of turbomachinery components |
04/01/2010 | US20100077612 Method of manufacturing a fairing with an integrated seal |
04/01/2010 | DE10259963B4 Wabendichtung Honeycomb seal |
03/31/2010 | EP2169345A1 Blade tip clearance measurement sensor |
03/31/2010 | EP2169026A2 Turbine friendly abradable material |
03/31/2010 | EP2167792A1 Turbocharger having a turbocharger housing |
03/31/2010 | CN101688448A Turbine arrangement and method of cooling a shroud located at the tip of a turbine blade |
03/31/2010 | CN101684736A Shroud for a turbomachine |
03/31/2010 | CN101684735A Gas turbine seal |
03/30/2010 | US7686570 Abradable coating system |
03/30/2010 | US7686569 Blade clearance system for a turbine engine |
03/30/2010 | CA2445237C Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
03/25/2010 | WO2010033139A1 Compressible ceramic seal |
03/25/2010 | WO2010031604A1 Device for sealing off a bearing housing of an exhaust-gas turbocharger |
03/25/2010 | US20100074734 Turbine Seal Assembly |
03/25/2010 | US20100074733 Ingestion Resistant Seal Assembly |
03/25/2010 | US20100074729 Compressible Ceramic Seal |
03/24/2010 | EP2166259A1 Device for sealing a storage housing of a waste gas turbocharger |
03/24/2010 | EP2166194A2 Dual stage turbine shroud |
03/24/2010 | EP2165049A1 Honeycomb structure |
03/24/2010 | CN101680307A Shaft seal for steam turbines |
03/24/2010 | CN101680306A Blade structure for turbine |
03/23/2010 | US7682130 Device and method for cooling a housing of a gas turbine or a combustion chamber |
03/23/2010 | CA2363632C Brush seal and method of making same |
03/18/2010 | WO2010030448A1 Intershaft seal system |
03/18/2010 | US20100068042 Brush seal for a turbo-machine |
03/18/2010 | US20100068041 Shroud for a turbomachine |
03/18/2010 | US20100066027 Intershaft Seal Assembly |
03/17/2010 | EP2163729A2 Turbine bucket with dovetail seal and related method |
03/17/2010 | EP2163725A2 Turbine blade damper arrangement |
03/17/2010 | CN201424967Y Backpressure steam turbine |
03/17/2010 | CN201424966Y Backpressure steam turbine |
03/11/2010 | US20100061842 Steam turbine rotating blade for a low pressure section of a steam turbine engine |
03/11/2010 | DE102009043865A1 Strömungssperre für das Gehäuse einer Turbomaschine Flow barrier for the casing of a turbomachine |
03/11/2010 | DE102008045657A1 Vorrichtung und Verfahren zur Reduzierung des Drucks auf eine Trennfuge zwischen wenigstens zwei Begrenzungsteilen Apparatus and method for reducing the pressure to a parting line between at least two limiting parts |
03/10/2010 | EP2161415A2 Device and method for reducing the pressure on a dividing fugue between at least two neighbouring sections |
03/04/2010 | WO2010023150A1 Guide vane support for a gas turbine |
03/04/2010 | WO2010023123A1 Turbine guide vane support for a gas turbine and method for operating a gas turbine |
03/04/2010 | US20100054924 Brush seal and turbine using the same |
03/04/2010 | US20100054922 Turbine airfoil clocking |
03/04/2010 | US20100054914 Gas turbine engine component having dual flow passage cooling chamber formed by single core |
03/04/2010 | US20100054912 Device, system and method for thermally activated displacement |
03/04/2010 | US20100054911 System and method for adjusting clearance in a gas turbine |
03/04/2010 | DE102009043832A1 System und Verfahren zur Einstellung des Spiels in einer Gasturbine System and method for setting the game in a gas turbine |
03/03/2010 | EP2159460A1 Preforms and related methods for repairing abradable seals of gas turbine engines |
03/03/2010 | EP2159382A1 Lead rotor holder for a gas turbine |
03/03/2010 | EP2159381A1 Turbine lead rotor holder for a gas turbine |
03/03/2010 | EP2159377A1 Stator vane support for a gas turbine and corresponding gas turbine plant |
03/03/2010 | EP2158381A2 Guide vane for a gas turbine |
03/03/2010 | CN101660431A System and method for adjusting clearance in a gas turbine |
03/03/2010 | CN101660430A Telescopic brush type gland ring |
03/02/2010 | US7670675 improve the cooling in a layer structure; used for turbine components of a turbomachine, such as a gas turbine; improved mechanical bonding of the pore walls to the substrate |
02/25/2010 | WO2010021566A1 Labyrinth shroud seal for a steam turbine |
02/25/2010 | DE102008039508A1 Charging device i.e. exhaust-gas turbocharger, for internal-combustion engine of motor vehicle, has annular disk for covering side parts of guide vanes, where disc has heat isolating and friction reducing material |
02/24/2010 | EP2157289A2 Pumping impeller oil seal |
02/24/2010 | EP2157288A2 Sealing means |
02/24/2010 | EP2156018A1 Adaptive labyrinth seal |
02/24/2010 | CN101657608A Impulse turbine |
02/23/2010 | US7665964 Turbine |
02/23/2010 | US7665960 Turbine shroud thermal distortion control |
02/23/2010 | US7665955 Vortex cooled turbine blade outer air seal for a turbine engine |
02/23/2010 | US7665739 Pressure-actuated seals for rotating members |
02/18/2010 | WO2010018174A1 Blade arrangement of a gas turbine |
02/18/2010 | WO2010018021A1 Reducing the thermal load of an external housing for a turbo-machine |
02/18/2010 | WO2010017893A1 Clearance and wear determination apparatus |
02/18/2010 | US20100040458 Axial fan casing design with circumferentially spaced wedges |
02/18/2010 | US20100040453 Apparatus and method for controlling a compressor |
02/18/2010 | DE10233881B4 Durch thermische Effekte radial veränderbares Ringelement By thermal effects radially variable ring element |
02/17/2010 | EP2154348A2 Engine braking method and system |
02/17/2010 | EP2154335A1 Ring seal attachment system |
02/17/2010 | EP2154334A2 Annulus filler between turbine blades |
02/17/2010 | EP2154332A1 Reduction of the thermal loading of an external casing for a fluid flow engine |
02/17/2010 | CN100590297C Expanding sealing strips for steam turbines |
02/16/2010 | US7661926 Turbomachine blade |
02/16/2010 | CA2430444C Simplified support device for nozzles of a gas turbine stage |
02/11/2010 | US20100034645 Rotor path arrangements |
02/11/2010 | US20100034644 Hybrid seal assembly for a fan-turbine rotor of a tip turbine engine |
02/11/2010 | DE102008036450A1 Labyrinth-sealing web-repairing process for gas turbine, comprises subjecting a metal melt on a component surface to be constructed, where the metal melt is produced by melting of particles of metal powder using laser beam |
02/10/2010 | CN101644172A Spring seal for blade dovetail |
02/09/2010 | US7658588 Optimized blade tip clearance process for a rub tolerant design |
02/04/2010 | WO2010012655A1 Leaf seal |
02/04/2010 | US20100025936 Leaf Seal Arrangement |
02/02/2010 | US7654791 Apparatus and method for controlling a blade tip clearance for a compressor |
01/28/2010 | WO2010009997A1 Shroud seal segments arrangement in a gas turbine |
01/28/2010 | WO2009067992A3 Active gap regulating device for a rotor housing |
01/26/2010 | US7651317 Multistage turbomachine compressor |
01/21/2010 | WO2010007323A1 Method of repairing or reworking a turbomachine disk and repaired or reworked turbomachine disk |
01/21/2010 | WO2010007137A1 Axial turbo engine with low gap losses |
01/21/2010 | WO2010006975A1 Axial turbo engine with low gap losses |
01/21/2010 | US20100014986 Sealing element for a gas turbine, a gas turbine including said sealing element and method for cooling said sealing element |
01/21/2010 | DE102008031980A1 Verfahren zum Betrieb einer Maschine mit einer Wellendichtung Method for operating a machine having a shaft seal |
01/21/2010 | CA2731092A1 Axial turbomachine with low tip clearance losses |
01/21/2010 | CA2730966A1 Method of repairing or reworking a turbomachine disk and repaired or reworked turbomachine disk |
01/20/2010 | EP2146055A1 Sealing element for a gas turbine, a gas turbine including said sealing element and method for cooling said sealing element |
01/20/2010 | EP2146053A1 Axial turbomachine with low tip leakage losses |