| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 09/08/2009 | US7584924 High speed vertical take-off and land aircraft with active fan balancing system |
| 09/08/2009 | US7584618 Controlling air flow to a turbine shroud for thermal control |
| 09/03/2009 | WO2009108142A1 Gas turbine stage |
| 09/03/2009 | WO2009106045A1 Device and method for redirecting a leakage current |
| 09/03/2009 | US20090218771 Bristle and plate subassembly fixture and manufacturing method |
| 09/03/2009 | DE102008011746A1 Vorrichtung und Verfahren zur Umleitung eines Leckagestroms Apparatus and method for redirecting a leakage current |
| 09/03/2009 | CA2716878A1 Device and method for redirecting a leakage current |
| 09/02/2009 | EP2096316A2 Housing structuring for axial compressor in the hub area |
| 09/02/2009 | EP2096266A1 Nozzle-synchronising ring assembly for a turbomachine |
| 09/02/2009 | EP2096262A1 Axial flow turbine with low shroud leakage losses |
| 09/02/2009 | EP2094946A1 Blade arrangement |
| 09/02/2009 | CN201301730Y Steam seal pressure adjusting device for steam seal system of turbine |
| 09/02/2009 | CN100534778C High temperature layered system for heat dissipation and method for making it |
| 09/01/2009 | US7582362 Thermal spray compositions for abradable seals |
| 09/01/2009 | US7581931 Gas turbine belly band seal anti-rotation structure |
| 09/01/2009 | US7581923 Gas turbine engine with purge air pump and guide |
| 09/01/2009 | US7581921 Methods and apparatus for controlling rotary machines |
| 08/27/2009 | WO2009085580A3 Turbine nozzle segment and method for repairing a turbine nozzle segment |
| 08/27/2009 | US20090214824 Apparatus and method for coating a compressor housing |
| 08/27/2009 | US20090212501 Self-Balancing Face Seals and Gas Turbine Engine Systems Involving Such Seals |
| 08/27/2009 | CA2655916A1 Split annular ring for turbine engine rotating part |
| 08/27/2009 | CA2655910A1 Diffuser-stator assembly for a turbine engine |
| 08/26/2009 | EP2093401A2 Seal assembly for a gas turbine |
| 08/26/2009 | EP2093384A2 Filter system for blade outer air seal |
| 08/26/2009 | EP2093380A2 Single channel inner diameter shroud with lightweight inner core in a gas turbine |
| 08/26/2009 | EP2092164A1 Turbomachine, particularly a gas turbine |
| 08/26/2009 | CN101514640A Rotor of turbomachine and method for replacing rotor blades of the rotor |
| 08/25/2009 | US7578653 Ovate band turbine stage |
| 08/25/2009 | US7578509 Seal assembly and rotary machine containing such seal |
| 08/20/2009 | US20090208330 Sealing assembly for a turbine engine |
| 08/20/2009 | US20090208322 Gas turbine engine systems and methods involving blade outer air seals |
| 08/20/2009 | US20090208321 Turbine blade tip clearance system |
| 08/20/2009 | US20090206554 Steam turbine engine and method of assembling same |
| 08/20/2009 | DE102009003480A1 Dampfturbine und Verfahren zum Zusammenbau derselben Steam turbine and method of assembling the same |
| 08/20/2009 | DE102008009824A1 Dichtungsanordnung für eine Gasturbine A seal assembly for a gas turbine |
| 08/19/2009 | EP2090754A2 Gas turbine engines and methods involving blade outer air seals |
| 08/19/2009 | EP2090753A2 Sealing assembly for a turbine engine and corresponding operating method |
| 08/19/2009 | EP2089647A2 Floating sealing ring |
| 08/19/2009 | CN201292865Y Low-pressure shaft seal sealing device for steam turbine |
| 08/19/2009 | CN101512107A Sealing means of adjustable guide vanes |
| 08/18/2009 | US7575412 Anti-stall casing treatment for turbo compressors |
| 08/13/2009 | US20090202343 Turbocharger shaft bearing system |
| 08/13/2009 | US20090202341 Turbomachine module provided with a device to improve radial clearances |
| 08/13/2009 | DE102008007321A1 Device, particularly gas turbine, has rotor and housing encompassing rotor, where rubbing seal is arranged between rotor and wall section of housing opposite rotor |
| 08/12/2009 | EP2087208A1 Turbo engine |
| 08/12/2009 | CN201288590Y Integration type clapboard radial packing apparatus for steam turbine |
| 08/12/2009 | CN101506553A Brush seal for a turbomachine |
| 08/11/2009 | US7572099 Seal for turbine engine |
| 08/11/2009 | US7571614 Turboshaft engine comprising two subassemblies assembled under axial stress |
| 08/06/2009 | WO2009095402A1 Combination of a brush seal with a piston ring for large sealing gaps |
| 08/06/2009 | WO2009095386A1 Exhaust gas turbocharger |
| 08/06/2009 | US20090196743 Turbocharger |
| 08/06/2009 | US20090196742 Retractable compliant plate seals |
| 08/06/2009 | US20090196730 Gas turbine with a compressor with self-healing abradable coating |
| 08/06/2009 | DE102009003423A1 Zurückziehbare elastische Plattendichtungen Retractable elastic plate seals |
| 08/06/2009 | DE102008006833A1 Sonde für eine kapazitive Sensoreinrichtung und Spaltmesssystem Probe for a capacitive sensor device and gap measurement system |
| 08/05/2009 | EP2085575A1 Combination of a brush seal with piston ring for large seal gaps |
| 08/05/2009 | CN201284667Y Novel turbine sealing device |
| 08/05/2009 | CN101498228A Invertible contact steam seal |
| 07/30/2009 | WO2009093512A1 Seal structure |
| 07/30/2009 | WO2009092797A1 Seal assembly |
| 07/30/2009 | US20090191050 Sealing band having bendable tang with anti-rotation in a turbine and associated methods |
| 07/30/2009 | US20090191049 Turbojet compressor |
| 07/30/2009 | DE102008006486A1 Bürstendichtung und Verfahren zur Montage einer Bürstendichtung A brush seal and method of assembling a brush seal |
| 07/30/2009 | DE102008006485A1 Bürstendichtung und Verfahren zur Montage einer Bürstendichtung A brush seal and method of assembling a brush seal |
| 07/30/2009 | DE102008005482A1 Gas turbine has compressor, which has set of shovels and running-in layer, which is connected with fluid supply device and provided with liquid flow through opening, where upper layer of running-in layer is made of liquid-tight material |
| 07/30/2009 | DE102008005480A1 Gas turbine, has running-in layer connected with material feeder, which contains air-hardening material, where running-in layer is provided with material openings that are formed by pores of material of running-in layer |
| 07/30/2009 | DE102008005479A1 Gas turbine has compressor with set of blades, where blades are provided with free end in each case, and adjacent intake layer is formed on free end of blades at circular housing area |
| 07/29/2009 | EP2083200A1 Seal assembly |
| 07/29/2009 | EP2083149A1 Exhaust gas turbine |
| 07/29/2009 | EP2083148A2 Gas turbine with a compressor with run-in coating and method of lapping the free extremities of compressor blades in a gas turbine |
| 07/29/2009 | CN201280954Y Rear gland sealing steam supply device for condensing steam turbine |
| 07/29/2009 | CN100520012C Easy-to-assemble heat-screening device for connecting cooling tube and through hole |
| 07/28/2009 | US7565729 Methods of manufacturing a segmented brush seal for sealing between stationary and rotary components |
| 07/23/2009 | WO2009042069A3 Improved ring segment coolant seal configuration |
| 07/23/2009 | US20090184477 Blade seal |
| 07/23/2009 | DE112007002151T5 Dichtung für einen Turbinenmotor Seal for a turbine engine |
| 07/23/2009 | CA2711914A1 Self-monitoring system for evaluating and controlling adjustment requirements of leakage restricting devices in rotodynamic pumps |
| 07/22/2009 | EP2079902A1 Seal arrangement |
| 07/22/2009 | EP2079901A1 Turbomachine and method for turning a turbomachine |
| 07/22/2009 | EP1697617A4 Improved leakage control in a gas turbine engine |
| 07/21/2009 | US7563079 Bore and shaft assembly |
| 07/21/2009 | US7563071 Pin-loaded mounting apparatus for a refractory component in a combustion turbine engine |
| 07/16/2009 | WO2009086982A1 Compressor for a gas turbine |
| 07/16/2009 | US20090180865 Vane tip clearance management structure for gas turbine |
| 07/16/2009 | US20090180863 Protection device for a turbine stator |
| 07/16/2009 | US20090180860 Protection device for a turbine stator |
| 07/15/2009 | EP2078837A1 Bleed air apparatus for a compressor of a gas turbine engine |
| 07/15/2009 | EP2078825A2 Turbocharger |
| 07/15/2009 | EP2078822A1 Gas-turbine engine with valve for connecting two enclosures |
| 07/15/2009 | EP2078587A1 Dimensional restoration of stationary shroud segments |
| 07/14/2009 | US7559741 Turbomachine having an axially displaceable rotor |
| 07/14/2009 | US7559554 Sealing arrangement using brush seals |
| 07/09/2009 | WO2009085949A1 Turbine nozzle segment |
| 07/09/2009 | WO2009085620A1 Turbine nozzle segment and assembly |
| 07/09/2009 | WO2009085580A2 Turbine nozzle segment and method for repairing a turbine nozzle segment |
| 07/09/2009 | WO2009085467A1 Compressor blade tip clearance control system with a plasma actuator, compressor and gas turbine engine with such a control system |
| 07/09/2009 | US20090175717 Multistage Turbocompressor |
| 07/09/2009 | DE102008055593A1 Verfahren und Systeme zur neuronalen Netzwerkmodellierung von Turbinenkomponenten Methods and systems for neural network modeling of turbine components |
| 07/09/2009 | DE102007037311B4 Wellendichtung für eine Turbine für eine ORC-Anlage, ORC-Anlage mit einer derartigen Turbinenwellendichtung und Verfahren zum Betreiben einer ORC-Anlage Shaft seal for a turbine for an ORC system, ORC system with such a turbine shaft seal and method for operating an ORC system |