Patents for F01D 9 - Stators (10,038) |
---|
03/15/2012 | WO2012031558A1 Compressed gas engine |
03/15/2012 | WO2012031381A1 Composite nozzle device for turbocharger |
03/15/2012 | WO2011054812A3 Turbomachine with axial compression or expansion |
03/15/2012 | DE102011053405A1 Turbinenabgasraum Turbine exhaust gas space |
03/15/2012 | CA2810184A1 Turbojet engine blade, in particular a guide blade, and turbojet engine receiving such blades |
03/15/2012 | CA2810181A1 Turbojet casing and turbojet receiving such casings |
03/14/2012 | EP2428648A2 Gas turbine engine |
03/14/2012 | EP2428647A1 Transitional Region for a Combustion Chamber of a Gas Turbine |
03/14/2012 | EP2427659A1 Housing for a stator of an aircraft turbine engine, comprising slits for the mechanical offloading of blades |
03/14/2012 | EP2427635A1 Supporting structure for a gas turbine engine |
03/14/2012 | EP2427634A1 A strut and a gas turbine structure comprising the strut |
03/14/2012 | CN202165129U 一种带有分流叶片的径流式透平 A radial turbine blades with split |
03/14/2012 | CN102373970A Air turbine starter inlet housing assembly airflow path |
03/14/2012 | CN102373965A Adjustable fixed blade assembly of high-temperature high-dust-content flue gas turbine |
03/14/2012 | CN102373964A Combustor transition piece with dilution sleeves and related method |
03/14/2012 | CN102373963A Air turbine starter turbine nozzle airfoil |
03/13/2012 | US8133018 High-pressure turbine of a turbomachine |
03/13/2012 | US8133015 Turbine nozzle for a gas turbine engine |
03/08/2012 | WO2012030052A2 Reaction-type turbine |
03/08/2012 | US20120057960 Ring segment with forked cooling passages |
03/07/2012 | CN202157837U 一种利用炉体余热的汽轮机 A use of furnace waste heat steam turbine |
03/01/2012 | WO2011137004A3 Turbocharger with turbine nozzle vanes and an annular rotary bypass valve |
03/01/2012 | US20120051901 Airfoil shape for compressor |
03/01/2012 | DE102010036071A1 Gehäuseseitige Struktur einer Turbomaschine Housing-side structure of a turbomachine |
03/01/2012 | DE102005024160B4 Innenkernprofil für ein Leitschaufelblatt einer Turbine Inner core profile for a turbine airfoil |
02/29/2012 | EP2423446A2 Turbine housing assembly with wastegate |
02/29/2012 | EP2423445A2 Turbine housing assembly |
02/29/2012 | EP2423444A2 Turbine nozzle with contoured band |
02/29/2012 | EP2423443A2 Composite vane mounting |
02/29/2012 | EP2423437A2 Turbine assembly with end-wall-contoured airfoils and preferential clocking |
02/29/2012 | EP2422052A1 A method for fabricating a gas turbine engine component and a gas turbine engine component |
02/29/2012 | CA2749476A1 Composite vane mounting |
02/29/2012 | CA2743654A1 Turbine nozzle with contoured band |
02/29/2012 | CA2743355A1 Turbine assembly with end-wall-contoured airfoils and preferential clocking |
02/28/2012 | US8123474 Repair of industrial gas turbine nozzle diaphragm packing |
02/23/2012 | DE102010034569A1 Blade ring carrier arrangement for e.g. steam turbine, has cam bolt with threaded section that is screwed into screw thread of blade ring carrier and support unit, so that relative position between carrier and support unit is changeable |
02/21/2012 | US8118549 Gas turbine transition duct apparatus |
02/16/2012 | DE102011006658A1 Control stage for turbine, has stator with guide vanes and two flow channels, where former flow channel is configured such that working fluid impinges with fluid parameters and mass flow of former guide vane |
02/15/2012 | EP2418358A2 Power device with a supply chamber |
02/14/2012 | US8113786 Stator vane profile optimization |
02/14/2012 | US8113773 Airfoil shape for a compressor vane |
02/09/2012 | US20120034078 Impeller and centrifugal compressor including the same |
02/09/2012 | DE102010038909A1 Turbine housing for exhaust gas turbocharger for internal-combustion engine, has spiral channel for exhaust gas system, by which exhaust gas is conducted on turbine wheel |
02/09/2012 | DE102010033327A1 Eingehäusige Dampfturbine mit Zwischenüberhitzung Single casing steam turbine with reheat |
02/09/2012 | DE102009041027B4 Leitschaufel für einen Turbolader, Leitschaufelanordnung, Turbolader, Kraftfahrzeug und Verfahren Vane for a turbocharger vane assembly, turbochargers, automotive and procedures |
02/08/2012 | CN102348867A Turbine vane with dusting hole at the base of the blade |
02/08/2012 | CN101460706B 用于流体机械、尤其是用于蒸汽涡轮机的导向叶片 For fluid machinery, in particular, guide vanes for steam turbine |
02/07/2012 | US8109719 Annular component |
02/07/2012 | US8109715 Variable nozzle turbocharger |
02/07/2012 | CA2663063C Thermal and external load isolating impeller shroud |
02/07/2012 | CA2509935C Grommeted bypass duct penetration |
02/07/2012 | CA2448465C Fabricated repair of cast nozzle |
02/02/2012 | WO2012016106A2 Nozzled turbocharger turbine |
02/02/2012 | US20120027578 Systems and apparatus relating to diffusers in combustion turbine engines |
02/02/2012 | US20120027568 Low-pressure steam turbine and method for operating thereof |
02/02/2012 | DE102010032319A1 Flanschverbindung Flange |
02/01/2012 | EP2412932A2 Blade outer air seal and repair method |
02/01/2012 | EP2412931A2 Composite Vane Mounting |
02/01/2012 | EP2412930A2 Turbine nozzle segment and method of repairing same |
02/01/2012 | EP2412929A1 Cmc turbine stator vane |
02/01/2012 | EP2412928A1 Cmc turbine stator vane |
02/01/2012 | EP2412925A1 Turbine blade and gas turbine |
02/01/2012 | CN102341569A Device for repairing the casing holder of an aeronautical engine |
01/31/2012 | US8105019 3D contoured vane endwall for variable area turbine vane arrangement |
01/31/2012 | US8105016 Damping arrangement for guide vanes |
01/28/2012 | CA2746284A1 Composite vane mounting |
01/26/2012 | WO2012012330A1 A seal assembly for controlling fluid flow |
01/26/2012 | WO2012011986A1 Diffuser having detachable vanes with positive lock |
01/26/2012 | WO2010085541A3 Structural attachment system for transition duct outlet |
01/26/2012 | US20120020768 Cooled constructional element for a gas turbine |
01/26/2012 | DE102011052077A1 Turbinenleitapparatsegment mit bogenförmiger konkaver Vorderkante Turbine nozzle arcuate concave front edge |
01/26/2012 | CA2747278A1 An optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the third stage of a turbine |
01/26/2012 | CA2747274A1 An optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the second stage of a turbine |
01/26/2012 | CA2746882A1 An optimized aerodynamic profile for a turbine vane, in particular for a nozzle of the fourth stage of a turbine |
01/25/2012 | EP2410154A2 Systems and methods for controlling the startup of a gas turbine |
01/25/2012 | EP2410130A2 Fan outlet guide vanes of a turbofan engine |
01/25/2012 | EP2410125A1 Gas turbine |
01/25/2012 | EP2409002A2 Tandem blade design |
01/25/2012 | CN102333935A Turbine blade and gas turbine |
01/25/2012 | CN102330571A Turbine blade with enhanced wake mixing via fluidic-generated vortices |
01/24/2012 | CA2472324C Cooled blade of a gas turbine starter |
01/24/2012 | CA2465071C Diametrically energized piston ring |
01/19/2012 | WO2012007716A1 Vane assembly for an axial flow turbine |
01/19/2012 | WO2012007499A1 Exhaust gas diffuser for a gas turbine and a method for operating a gas turbine that comprises such an exhaust gas diffuser |
01/19/2012 | WO2012007250A1 Nozzle guide vane with cooled platform for a gas turbine |
01/19/2012 | WO2012006925A1 Multistage compressed gas engine and motor vehicle |
01/19/2012 | US20120014776 Method and apparatus for enhancing compressor performance |
01/19/2012 | DE102011016528A1 Turbine for exhaust-gas turbocharger of internal combustion engine of motor vehicle i.e. passenger car, has first flooded part arranged separately from second and third flooded parts in circumferential direction |
01/19/2012 | DE102010027588A1 Fan-Nachleitradschaufel eines Turbofantriebwerks Fan downstream guide vane of a turbofan engine |
01/19/2012 | DE102010027110A1 Compressor for supercharger of diesel engine in commercial motor vehicle, has guide device arranged in wheel inlet region along flow direction of medium upstream, where pre-rotation of medium flow is generated by guide device |
01/19/2012 | DE102009038623B4 Leitschaufelkranz für den Verdichter einer Fluggasturbine Guide vane for the compressor of an aircraft gas turbine |
01/19/2012 | CA2805143A1 Multistage compressed gas engine and motor vehicle |
01/19/2012 | CA2746397A1 High pressure turbine vane cooling hole distribution |
01/18/2012 | EP2407640A2 Integral lubrication tube and nozzle combination |
01/18/2012 | EP2407639A1 Platform part for supporting a nozzle guide vane for a gas turbine |
01/18/2012 | EP2407638A1 Exhaust gas diffuser for a gas turbine and method for operating a gas turbine with such an exhaust gas diffuser |
01/18/2012 | EP2407247A1 Turbine of a rotary dispenser |
01/18/2012 | EP2406466A1 Turbine ring assembly |
01/18/2012 | EP2406463A1 Turbine vane with dusting hole at the base of the blade |
01/18/2012 | CN102322298A Turbine guider and turbine |