Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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03/14/2013 | US20130064645 Non-continuous ring seal |
03/14/2013 | US20130064638 Boundary Layer Blowing Using Steam Seal Leakage Flow |
03/14/2013 | DE112011101811T5 Steuerwellendichtung Control shaft seal |
03/14/2013 | CA2847977A1 Seal for a rotary machine |
03/14/2013 | CA2847239A1 Assembly consisting of a turbine nozzle or a compressor stator vane made of cmc for a turbine engine and an abradable support ring, and turbine or compressor including such an assembly |
03/13/2013 | EP2568202A1 Non-continuous ring seal |
03/13/2013 | EP2568121A1 Stepped conical honeycomb seal carrier and corresponding annular seal |
03/13/2013 | EP2567072A2 Brush ring seal |
03/13/2013 | CN202778746U Steam and water separator |
03/13/2013 | CN102966383A Air seal device and manufacturing method thereof |
03/12/2013 | US8393859 Card seal for a turbine |
03/12/2013 | CA2580472C Protection device for a turbine stator |
03/12/2013 | CA2520282C Turbine module for gas turbine engine |
03/12/2013 | CA2518355C Retention of centring keys of the rings under the variable setting stator blades of a gas turbine engine |
03/07/2013 | WO2011144567A3 Method and device for supplying cooling air to an engine, in particular an aircraft engine, gas turbine, or the like |
03/07/2013 | US20130058768 Gas turbine engines with abradable turbine seal assemblies |
03/07/2013 | US20130058767 Centrifugal pump, a shaft sleeve and a stationary seal member |
03/07/2013 | US20130058766 Systems, Methods, and Apparatus for a Labyrinth Seal |
03/07/2013 | US20130058765 Rotary machine seal assembly with butt gap seal elements |
03/07/2013 | US20130058764 Stepped, conical honeycomb seal carrier |
03/07/2013 | DE102012108123A1 Rotationsmaschinendichtungsanordnung mit Stoßlückendichtungselementen Rotating machinery sealing arrangement with shock gap sealing elements |
03/07/2013 | DE102012108122A1 Systeme, Verfahren und Vorrichtungen für eine Labyrinthdichtung Systems, methods and apparatus for a labyrinth seal |
03/06/2013 | EP2565378A2 Rotor casing liner assembly and corresponding power plant |
03/06/2013 | EP2564033A1 Gas turbine and method for operating a gas turbine |
03/06/2013 | EP2564032A1 Component of a turbine with leaf seals and method for sealing against leakage between a vane and a carrier element |
03/06/2013 | CN102959204A Shroud segment producing method and shroud segment |
03/06/2013 | CN102959184A Turbine |
03/06/2013 | CN102959183A Combined sealing and balancing arrangement for a turbine disc |
03/06/2013 | CN102953771A Labyrinth damping sealing device with low leakage and high damping performance |
03/06/2013 | CN102953770A Turbomachine seal assembly |
03/05/2013 | US8388313 Extraction cavity wing seal |
03/05/2013 | US8388311 Turbomachinery |
03/05/2013 | US8388303 Gas turbine having a rotor including a turbine rotor, expanded shaft and a compressor rotor |
03/05/2013 | US8388300 Turbine ring segment |
03/05/2013 | US8387910 Rotary seal |
02/28/2013 | WO2013026870A1 Turbomachine comprising a coated rotor blade tip and a coated inner housing |
02/28/2013 | WO2012149925A3 Cover device, integrally bladed main rotor body, method and turbomachine |
02/28/2013 | WO2012125387A3 Gas pressure biased sealing method for an actuating shaft |
02/28/2013 | US20130051993 Rotating turbomachine seal |
02/28/2013 | US20130051991 Universal seal |
02/28/2013 | US20130051972 Blade outer air seal with multi impingement plate assembly |
02/28/2013 | DE102011111702A1 Turbine for supercharger for reciprocating piston internal combustion engine of passenger car, has seal element arranged between wall regions of respective walls, where wall regions limit gap along axial direction of turbine wheel |
02/28/2013 | CA2776075A1 Turbine shroud segment with integrated impingement plate |
02/28/2013 | CA2776065A1 Turbine shroud segment with inter-segment overlap |
02/28/2013 | CA2776064A1 Turbine shroud segment |
02/28/2013 | CA2776058A1 Manufacturing of turbine shroud segment with internal cooling passages |
02/27/2013 | EP2562365A2 Blade outer air seal with multi impingement plate assembly |
02/27/2013 | EP2562364A1 Rotating Turbomachine Seal |
02/27/2013 | EP2562363A2 Flap seal for gas turbine engine movable nozzle flap |
02/27/2013 | EP2562362A2 Metallic fan blade platform |
02/27/2013 | EP2562355A2 Coupled blade platforms and methods of sealing |
02/27/2013 | CN202756027U Blade tip seal modification device |
02/27/2013 | CN102943694A Clapboard-type labyrinth structure for moving blade tip |
02/26/2013 | US8382436 Non-integral turbine blade platforms and systems |
02/26/2013 | US8382424 Turbine vane mate face seal pin with impingement cooling |
02/21/2013 | WO2013025454A1 Near net-shape panels and processes therefor |
02/21/2013 | WO2013025385A1 Panels and processes therefor |
02/21/2013 | WO2013025384A1 Rotor seal wire groove repair |
02/21/2013 | US20130045091 Rotatable component, coating and method of coating the rotatable component of an engine |
02/21/2013 | US20130045090 Turbomachine seal assembly |
02/21/2013 | US20130045089 Gas turbine engine seal assembly having flow-through tube |
02/21/2013 | US20130045088 Airfoil seal |
02/21/2013 | DE102012107320A1 Bürstendichtung mit Stützplattenzahn Brush seal with backing plate tooth |
02/21/2013 | CA2844646A1 Rotor seal wire groove repair |
02/21/2013 | CA2844624A1 Panels and processes therefor |
02/21/2013 | CA2843969A1 Near net-shape panels and processes therefor |
02/20/2013 | EP2559861A2 Rotatable component, coating and method of coating the rotatable component of an engine |
02/20/2013 | EP2559860A2 Turbomachine seal assembly |
02/20/2013 | EP2559859A1 Seal end attachment |
02/20/2013 | EP2559853A2 Gasturbine engine airfoil seal |
02/20/2013 | EP2559849A2 Gas turbine engine seal assembly having flow-through tube |
02/14/2013 | US20130039743 Method and apparatus for measuring turbine shell clearance |
02/13/2013 | EP2557274A2 Turbine airfoil and method for controlling a temperature of a turbine airfoil |
02/13/2013 | EP2557273A2 Seal assembly of a gas turbine |
02/13/2013 | EP2557268A2 System and method for controlling flow in turbomachinery |
02/13/2013 | CN202732000U Durable type steam seal structure of steam turbine |
02/13/2013 | CN102926872A Sealing arrangement between a variable-nozzle assembly and a turbine housing of a turbocharger |
02/13/2013 | CN101542073B Blade arrangement |
02/12/2013 | US8371807 Protection device for a turbine stator |
02/07/2013 | US20130034424 Tip clearance control device |
02/07/2013 | US20130033005 Gas turbine exhaust nozzle divergent flap seal |
02/07/2013 | DE102012107134A1 Unterteilte Dichtungsbaugruppe Subdivided seal assembly |
02/06/2013 | EP2554798A2 Rotor blade tip clearance control device and method |
02/06/2013 | EP2554797A2 System and method for passively controlling clearance in a gas turbine engine |
02/06/2013 | EP2554796A1 Turbine |
02/06/2013 | EP2553221A1 Sealing device for jet engine oil chamber |
02/06/2013 | CN202718710U Subcritical 600 million watt (MW) steam turbine nozzle |
02/06/2013 | CN102918308A Axial seal structure and rotation mechanism provided with same |
02/06/2013 | CN102913290A System and method for passively controlling clearance in a gas turbine engine |
02/06/2013 | CN102913289A Outward bristle brush seal design for gas turbine application |
02/05/2013 | US8366382 Mid-turbine frame buffer system |
01/31/2013 | WO2013014106A1 Centrifugal impeller and turbomachine |
01/31/2013 | WO2013013975A1 Airfoil arrangement comprising a sealing element made of metal foam |
01/31/2013 | US20130028717 Flap seal and sealing apparatus |
01/31/2013 | US20130028713 Seal for turbomachine segments |
01/31/2013 | US20130028704 Blade outer air seal with passage joined cavities |
01/31/2013 | CA2842033A1 Centrifugal impeller and turbomachine |
01/30/2013 | EP2551492A1 Seal structure for turbine rotor |
01/30/2013 | EP2551468A1 Blade outer air seal assembly with passage joined cavities and corresponding operating method |
01/30/2013 | EP2551467A1 Gas turbine engine active clearance control system and corresponding method |