| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 03/23/2011 | CN201771723U Shaft end combined seal for compressor/turbine |
| 03/22/2011 | US7909566 Rotor thrust balance activated tip clearance control system |
| 03/22/2011 | US7909334 Sealing arrangement and method for the production thereof |
| 03/22/2011 | CA2619081C Seal structure of gas turbine combustor |
| 03/22/2011 | CA2528668C Rotor assembly with cooling air deflectors and method |
| 03/22/2011 | CA2413126C Structure for separating the high and low pressure turboexpanders of a gas turbine |
| 03/17/2011 | WO2011030051A1 Clearance control at the blade tips of a turbomachine |
| 03/17/2011 | WO2011029420A1 Deflecting device for a leakage flow in a gas turbine, and gas turbine |
| 03/17/2011 | US20110064566 Apparatus for impeller sealing in centrifugal pumps |
| 03/17/2011 | DE102009040758A1 Umlenkvorrichtung für einen Leckagestrom in einer Gasturbine und Gasturbine Deflection for a leakage current in a gas turbine and gas turbine |
| 03/17/2011 | CA2773047A1 Clearance control at the blade tips of a turbomachine |
| 03/16/2011 | EP2295778A2 Energy absorbing fan blade spacer |
| 03/16/2011 | EP2295727A2 A sealing assembly |
| 03/16/2011 | EP2295722A1 Blade of a Turbine |
| 03/16/2011 | EP1893846B1 Ring seal attachment system |
| 03/16/2011 | CN101985889A System and method for clearance control in a rotary machine |
| 03/10/2011 | WO2011026921A1 Device for supporting a turbine ring, turbine having such a device, and turbine engine having such a turbine |
| 03/10/2011 | WO2011026468A2 Turbomachine, and method for producing a structured abradable coating |
| 03/10/2011 | WO2010007137A8 Axial turbo engine with low gap losses |
| 03/10/2011 | US20110058965 In-line flow mixer |
| 03/10/2011 | US20110058933 Device and method for redirecting a leakage current |
| 03/10/2011 | DE102009040299A1 Intake surface for rotor of turbo machine, particularly gas turbine, has profiled upper surface, which has multiple elongated, axially running recesses at distance from one another |
| 03/10/2011 | DE102009040298A1 Strömungsmaschine und Verfahren zur Erzeugung eines strukturierten Einlaufbelags Flow machine and method for generating a structured intake coating |
| 03/10/2011 | CA2772763A1 Device for supporting a turbine ring, turbine having such a device, and turbine engine having such a turbine |
| 03/09/2011 | EP2292897A1 Axial flow turbine |
| 03/09/2011 | EP2129875B1 Turbo engine with active clearance control |
| 03/09/2011 | EP1861584B1 Heat accumulation segment for sealing a flow channel of a turbine engine |
| 03/09/2011 | EP1706592B1 Turbine blade and gas turbine equipped with a turbine blade of this type |
| 03/09/2011 | CN201756983U Lateral honeycombed steam seal |
| 03/03/2011 | WO2011025484A1 Hydrodynamic circumferential seal system for large translations |
| 03/03/2011 | WO2011024242A1 Split ring cooling structure and gas turbine |
| 03/03/2011 | WO2010054884A3 Shaft unit comprising a sealing device |
| 03/03/2011 | US20110052367 Sealing and cooling at the joint between shroud segments |
| 03/03/2011 | US20110049809 Hydrodynamic Circumferential Seal System for Large Translations |
| 03/02/2011 | EP2290196A2 Adjustable fan case liner and mounting method |
| 02/24/2011 | WO2010136018A3 Clearance control system, turbomachine and method for adjusting a running clearance between a rotor and a casing of a turbomachine |
| 02/24/2011 | US20110044804 Blade outer air seal support |
| 02/24/2011 | US20110044803 Blade outer air seal anti-rotation |
| 02/24/2011 | US20110044802 Blade outer air seal support cooling air distribution system |
| 02/24/2011 | US20110044801 Blade outer air seal cooling |
| 02/24/2011 | US20110044800 Compressor Blade and Production and Use of a Compressor Blade |
| 02/23/2011 | EP2287500A1 Seal structure of rotary machine |
| 02/23/2011 | EP2287446A2 A rotor assembly for a gas turbine |
| 02/23/2011 | EP2286119A1 Non-contact seal for a gas turbine engine |
| 02/23/2011 | EP2286066A2 Sealing arrangement for turbine engine having ceramic components |
| 02/23/2011 | CN201751539U Turbine guider lower edge plate cooling flow guiding structure |
| 02/18/2011 | CA2713284A1 Blade outer air seal cooling |
| 02/18/2011 | CA2712952A1 Blade outer air seal support |
| 02/18/2011 | CA2712758A1 Blade outer air seal support cooling air distribution system |
| 02/18/2011 | CA2712756A1 Blade outer air seal anti-rotation |
| 02/17/2011 | WO2011018425A1 Vibration-damping shim for a fan blade |
| 02/17/2011 | US20110038743 Centrifugal fan |
| 02/17/2011 | US20110038718 Fluid Flow Machine |
| 02/17/2011 | DE102009037393A1 Strömungsmaschine Flow machine |
| 02/17/2011 | DE102005060961B4 Gasturbine Gas turbine |
| 02/17/2011 | CA2769781A1 Vibration-damping shim for a fan blade |
| 02/16/2011 | EP2284426A2 Turbomachine |
| 02/16/2011 | EP2283169A1 Segmented thermal barrier coating |
| 02/16/2011 | EP1642007B1 Turbine shroud segment |
| 02/16/2011 | CN201747416U Steam turbine changed from condensing steam type into back pressure type |
| 02/16/2011 | CN101978197A Rotating machine and additional ring |
| 02/13/2011 | CA2704349A1 Fluid flow machine |
| 02/10/2011 | US20110033283 Turbomachine rotor comprising an anti-wear plug, and anti-wear plug |
| 02/10/2011 | DE102009036407A1 Abreibbarer Schaufelspitzenbelag Abradable coating blade tip |
| 02/09/2011 | EP2282015A1 Turbo machine with an Improved Seal |
| 02/09/2011 | EP2282014A1 Ring-shaped flow channel section for a turbo engine |
| 02/09/2011 | CN201738956U Device for replacing gas sealing strip |
| 02/09/2011 | CN101970805A Turbine distributor for turbine engine |
| 02/09/2011 | CN101970804A Sectored distributor for turbomachine |
| 02/08/2011 | US7883315 Seal assembly for a fan rotor of a tip turbine engine |
| 02/08/2011 | US7883314 Seal assembly for a fan-turbine rotor of a tip turbine engine |
| 02/08/2011 | CA2457892C Gas turbine stator housing |
| 02/08/2011 | CA2388778C Turbomachine rotor assembly with two bladed-discs separated by a spacer |
| 02/03/2011 | US20110027068 System and method for clearance control in a rotary machine |
| 02/03/2011 | DE102010036494A1 System und Verfahren zur Abstandssteuerung in einer Rotationsmaschine System and method for distance control in a rotary machine |
| 02/02/2011 | EP2280151A1 Method for operating a gas turbine and rotor of a gas turbine |
| 02/02/2011 | EP2280149A1 Shroud integral type moving blade and split ring of gas turbine |
| 02/02/2011 | EP2279364A1 Non-contact seal for a gas turbine engine |
| 02/02/2011 | CN201730644U Low-entropy turbine |
| 01/27/2011 | WO2011009433A1 Abradable coating to be arranged on a gas turbine component |
| 01/27/2011 | US20110020113 Seal Structure for Preventing Leakage of Gases Across a Gap Between Two Components in a Turbine Engine |
| 01/27/2011 | DE102009034025A1 Einlaufbelag zur Anordnung an einem Gasturbinenbauteil Abradable coating for placement on a gas turbine component |
| 01/26/2011 | EP2278127A2 Turbocharger having nozzle ring locating pin and an integrated locator and heat shield |
| 01/26/2011 | EP2278125A2 Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
| 01/26/2011 | EP2087208B1 Turbo engine |
| 01/26/2011 | EP1766193B1 Run-in coating |
| 01/26/2011 | CN101054909B Steam turbine variable clearance packing |
| 01/25/2011 | US7874803 Gas turbine rotor |
| 01/25/2011 | US7874793 Blade clearance arrangement |
| 01/25/2011 | CA2548973C Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine |
| 01/25/2011 | CA2466215C Gas turbine stator |
| 01/20/2011 | WO2011008440A1 Spiral wound brush seal |
| 01/20/2011 | WO2011008411A2 Multi-stage turbocharger arrangement |
| 01/20/2011 | US20110014050 Turbine blade assembly and seal strip |
| 01/20/2011 | US20110014035 High-reliability turbine metal sealing material |
| 01/19/2011 | EP2275723A1 Seal support |
| 01/19/2011 | CN201714437U Steam turbine with steam extraction back pressure type changed from double-steam-extraction condensing type |
| 01/19/2011 | CN201714430U Rotor blade sealing device for flue gas turbine |
| 01/18/2011 | US7871244 Ring seal for a turbine engine |
| 01/18/2011 | CA2464124C Gasket with two concentric lips |