| Patents for F01D 9 - Stators (10,038) |
|---|
| 07/11/2013 | US20130177400 Stator vane integrated attachment liner and spring damper |
| 07/11/2013 | US20130177397 Slotted turbine airfoil |
| 07/11/2013 | US20130177396 Impingement Cooling System for Use with Contoured Surfaces |
| 07/11/2013 | US20130177384 Turbine nozzle compartmentalized cooling system |
| 07/11/2013 | DE102005019896B4 Drallerzeugungseinrichtung Swirler |
| 07/11/2013 | CA2857171A1 Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure |
| 07/10/2013 | EP2613041A2 Turbine to operate at part-load |
| 07/10/2013 | EP2613005A1 Turbomachine Component including a Cover Plate |
| 07/10/2013 | EP2613004A2 Turbine nozzle assembly methods |
| 07/10/2013 | EP2613003A2 Transition duct for a gas turbine |
| 07/10/2013 | EP2613002A2 Methods and systems for cooling a transition nozzle |
| 07/10/2013 | EP2612998A2 Stator Vane Integrated Attachment Liner and Spring Damper |
| 07/10/2013 | EP2612986A2 Reaction-type turbine |
| 07/10/2013 | EP2611991A1 Fuel cell system having an integral turbine/compressor unit |
| 07/10/2013 | CN103201460A Stator blade unit of rotary machine, method for producing stator blade unit of rotary machine, and method for joining stator blade unit of rotary machine |
| 07/10/2013 | CN103201459A Reaction-type turbine |
| 07/10/2013 | CN103195746A Impeller tube assembly |
| 07/10/2013 | CN103195584A Turbine to operate at part-load |
| 07/10/2013 | CN103195507A Turbine nozzle compartmentalized cooling system |
| 07/10/2013 | CN103195497A Nozzle used for gas turbine and seal carrier |
| 07/10/2013 | CN103195496A Turbine nozzle assembly methods |
| 07/10/2013 | CN103195495A Slotted turbine airfoil |
| 07/10/2013 | CN103195494A Gas turbine stator assembly |
| 07/10/2013 | CN103195493A Turbine assembly and method for controlling a temperature of an assembly |
| 07/10/2013 | CN101936193B Method for manufacturing integral nozzle block of large-sized steam turbine |
| 07/05/2013 | CA2799999A1 Stator vane spring damper |
| 07/05/2013 | CA2799984A1 Stator vane integrated attachment liner and spring damper |
| 07/04/2013 | WO2013101761A1 Airfoil cooling circuit |
| 07/04/2013 | US20130170977 Gas Turbine Nozzle with a Flow Groove |
| 07/04/2013 | US20130170969 Turbine Diffuser |
| 07/04/2013 | DE112011103045T5 Verfahren zur Herstellung eines Turboladers A process for producing a turbocharger |
| 07/03/2013 | EP2610442A1 Gas turbine |
| 07/03/2013 | CN203035268U Dissymmetrical-arranged four-valve turbine injector set structure |
| 07/03/2013 | CN103184899A Turbine engine and method for flowing air in a turbine engine |
| 07/03/2013 | CN103184898A Gas turbine nozzle with a flow groove |
| 07/03/2013 | CN103184897A Gas turbine nozzle with a flow fence |
| 07/03/2013 | CN103184896A Turbine guide blade |
| 07/03/2013 | CN103183519A Method of forming a ceramic matrix composite and a ceramic matrix composite component |
| 07/02/2013 | US8475124 Exhaust hood for a turbine and methods of assembling the same |
| 07/02/2013 | CA2682489C Wall of turbo machine and turbo machine |
| 06/27/2013 | WO2013095212A1 Gas turbine engine component |
| 06/27/2013 | WO2013095211A1 Support structure for a gas turbine engine |
| 06/27/2013 | WO2013095209A1 Gas turbine engine component |
| 06/27/2013 | WO2013095202A1 Method for manufacturing of a gas turbine engine component |
| 06/27/2013 | WO2013093337A1 Turbomachine compressor guide vanes assembly |
| 06/27/2013 | US20130164488 Airfoils for wake desensitization and method for fabricating same |
| 06/27/2013 | US20130164118 Gas turbine engine duct blocker that includes a duct blocker rotor with a plurality of roller elements |
| 06/27/2013 | US20130164117 Gas turbine engine duct blocker with rotatable vane segments |
| 06/26/2013 | EP2607634A1 Method for operating a combined cycle power plant |
| 06/26/2013 | EP2607626A1 Turbomachine and stage of a turbomachine |
| 06/26/2013 | EP2607625A1 Turbomachine and stage of turbomachine |
| 06/26/2013 | EP2607624A1 Vane for a turbomachine |
| 06/26/2013 | EP2606203A1 Transonic gas turbine stage and method |
| 06/26/2013 | CN203022830U Connecting structure of low-pressure guide vanes and partition plate |
| 06/26/2013 | CN103180617A Transonic blade |
| 06/25/2013 | US8469662 Guide vane architecture |
| 06/25/2013 | US8469661 Fabricated gas turbine vane ring |
| 06/20/2013 | WO2013089500A1 Thermoplastic elastomer composition having low hardness, and diaphragm comprising same |
| 06/20/2013 | WO2013089255A1 Turbine blade |
| 06/20/2013 | WO2013089251A1 Turbine blade |
| 06/20/2013 | WO2013089250A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013089173A1 Impingement cooling mechanism, turbine blade and combustor |
| 06/20/2013 | WO2013088078A1 Flow straightener sector for a turbomachine compressor which is produced by brazing a platform of its vanes to a shell ring |
| 06/20/2013 | US20130156563 Turbomachine and turbomachine stage |
| 06/20/2013 | US20130156562 Turbomachine and turbomachine stage |
| 06/20/2013 | US20130156549 Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components |
| 06/20/2013 | DE102012003902A1 Inlet for gas turbine, has inlet wall, bypass-channel formed at inner side of inlet wall, and bypass flow-stator arranged at end of bypass-channel, where inner side of bypass-channel is limited by bypass-channel wall that has drain holes |
| 06/20/2013 | DE102011121330A1 Turbine für einen Abgasturbolader Turbine for an exhaust gas turbocharger |
| 06/20/2013 | CA2858020A1 Turbine blade |
| 06/20/2013 | CA2798821A1 Fan blade with composite core and wavy wall trailing edge cladding |
| 06/19/2013 | EP2604813A2 Gas Turbine Engine Part Retention |
| 06/19/2013 | EP2604801A1 Brazed steam turbine guide vane module |
| 06/19/2013 | EP2604800A2 Nozzle vane for a gas turbine engine |
| 06/19/2013 | EP2603668A1 Blade ring segment, turbomachine and method for producing same |
| 06/19/2013 | CN103168149A Assembly of a blade and a composite carrier, obtained by sealing |
| 06/19/2013 | CN103161515A Airflow driving device |
| 06/19/2013 | CN103161514A Case assemblies with common controls |
| 06/19/2013 | CN103161513A Improved nozzle vane for a gas turbine engine |
| 06/19/2013 | CN103161512A Steam turbine, blade, and method |
| 06/19/2013 | CN103161511A Stationary blade cascade, assembling method of stationary blade cascade, and steam turbine |
| 06/19/2013 | CN101743406B Outflow device of radial compressors and exhaust driven supercharger |
| 06/19/2013 | CN101497976B Method for manufacturing a turbomachine element and resulting device |
| 06/19/2013 | CN101408114B Apparatus and method for clearance control of turbine blade tip |
| 06/19/2013 | CN101315032B Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes |
| 06/18/2013 | CA2642505C Cooling structure |
| 06/18/2013 | CA2521983C Process for air circulation in a turbine engine compressor, compressor arrangement putting it into play, stage of compression and compressor comprising such an arrangement, and aircraft engine equipped with such a compressor |
| 06/15/2013 | CA2798307A1 Mounting apparatus for low-ductility turbine shroud |
| 06/13/2013 | WO2013086315A1 Structural platforms for fan double outlet guide vane |
| 06/13/2013 | WO2013086305A1 Quick engine change assembly for outlet guide vanes |
| 06/13/2013 | WO2013086296A1 Double fan outlet guide vane with structural platforms |
| 06/13/2013 | WO2013086291A1 Fan hub frame double outlet guide vane |
| 06/13/2013 | WO2013085435A1 Gas turbine engine component |
| 06/13/2013 | WO2013083937A1 Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting element |
| 06/13/2013 | US20130149136 Stationary blade cascade, assembling method of stationary blade cascade, and steam turbine |
| 06/13/2013 | US20130149135 Stator vane array |
| 06/13/2013 | US20130149133 Stator vane shroud having an offset |
| 06/13/2013 | US20130149124 Turbine |
| 06/13/2013 | US20130149106 Steam turbine, blade, and method |
| 06/13/2013 | US20130149100 Gas turbine engine |
| 06/13/2013 | DE102011120880A1 Turbine for exhaust gas turbocharger of internal combustion engine e.g. lifting cylinder internal combustion engine, has movable adjustment device which adjusts amount of exhaust gas flowing through the bypass passage of bypass device |