Patents for F01D 9 - Stators (10,038)
01/2012
01/17/2012US8096758 Circumferential shroud inserts for a gas turbine vane platform
01/17/2012US8096757 Methods and apparatus for reducing nozzle stress
01/17/2012US8096746 Radial loading element for turbine vane
01/12/2012WO2012005324A1 Turbine blade and engine component
01/12/2012DE102011051573A1 Kompressible Halterungen für Gasturbinen Compressible holders for gas turbines
01/12/2012CA2804632A1 Turbine blade and engine component
01/11/2012EP2405102A1 Gas turbine with bellows seal
01/11/2012EP2404039A1 Device for repairing the casing holder of an aeronautical engine
01/11/2012CN102317634A Axial turbo compressor for a gas turbine having low radial gap losses and diffuser losses
01/11/2012CN102317582A Three-shelled steam turbine having valve
01/11/2012CN102317581A Valve connection to a three-shelled turbo machine
01/11/2012CN102317580A Three-shelled steam turbine
01/11/2012CN102312726A Turboexpander and method for using moveable inlet guide vanes at compressor inlet
01/11/2012CN102312684A Steam and air mixed cooling turbine guide blade
01/10/2012CA2500493C Turbine engine high-pressure turbine stator and assembly process
01/04/2012EP2402659A1 Combustion chamber external jacket
01/04/2012EP2402615A1 Axial compressor diffuser architecture
01/04/2012CN1525048B Gas turbine engine turbine nozzle bifurcated impingement baffle
01/03/2012US8087884 Advanced booster stator vane
01/03/2012US8087878 Powerless diversion plate of a ceiling air-conditioning circulation machine
01/03/2012CA2478890C Device to stop the rotation of straightening blades with connectors in the mating surfaces of the housing
12/2011
12/29/2011WO2011160601A1 Improved impeller chamber and compressed air engine
12/29/2011WO2010027382A3 Combustor device and transition duct assembly
12/29/2011US20110314808 Vanes for directing exhaust to a turbine wheel
12/29/2011CA2744571A1 Compressor rectifier architecture
12/29/2011CA2743521A1 Liner aft end support mechanisms and spring loaded liner stop mechanisms
12/28/2011CN202090962U 一种冲动式汽轮机隔板 An impulse turbine separators
12/28/2011CN202090961U 一种冲动式汽轮机镶入式隔板静叶 Insert an impulse turbine vanes Bulkhead
12/28/2011CN202090960U 一种湿蒸汽余热发电汽轮机 One kind of wet steam turbine cogeneration
12/28/2011CN1621661B 安装涡轮静止叶片的方法和具有径向加载销的涡轮结构 Installation method for a turbine stationary blades and turbine structure having radial loading pin
12/28/2011CN102301128A 环形多转子双壁涡轮机 Multi double-walled annular rotor turbine
12/28/2011CN102297016A 双叶片喷嘴系统的涡轮增压器 Dual blade nozzle system of the turbocharger
12/28/2011CN102296992A 多翼型翼片 Multi-wing flaps
12/28/2011CN102296990A 改进的压缩气体发动机 Improved compression of the gas engine
12/27/2011US8083465 Repaired turbine exhaust strut heat shield vanes and repair methods
12/22/2011WO2011157971A1 Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine
12/22/2011WO2011157962A1 Airflow-straightening structure for the nacelle of an aircraft engine
12/22/2011WO2011157957A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector
12/22/2011WO2011157956A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector
12/22/2011WO2011157549A1 Platform segment for supporting a nozzle guide vane for a gas turbine and method of cooling thereof
12/22/2011US20110312246 Multiple Airfoil Vanes
12/22/2011CA2802821A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector
12/22/2011CA2802590A1 Airflow-straightening structure for the nacelle of an aircraft engine
12/22/2011CA2802397A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector
12/22/2011CA2801222A1 Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine
12/21/2011EP2397654A2 Vane assembly
12/21/2011EP2397653A1 Platform segment for supporting a nozzle guide vane for a gas turbine and method of cooling thereof
12/21/2011EP2396555A1 Axial turbo compressor for a gas turbine having low radial gap losses and diffuser losses
12/21/2011EP2396518A1 Three-shelled steam turbine having valve
12/21/2011EP2396517A1 Three-shelled steam turbine
12/21/2011EP2396516A1 Valve connection to a three-shelled turbo machine
12/21/2011CN202081965U Supercharger with changeable nozzle blade
12/21/2011CN202081918U 一种600mw汽轮机喷嘴 One kind of 600mw turbine nozzle
12/20/2011US8079817 Advanced firtree and broach slot forms for turbine stage 3 buckets and rotor wheels
12/15/2011WO2011156078A1 Cooled conduit for conveying combustion gases in a gas turbine engine
12/15/2011WO2011154195A1 Cooled vane of a turbine and corresponding turbine
12/15/2011WO2011124985A3 Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine
12/15/2011US20110305564 Local exhaust apparatus
12/15/2011US20110304230 Fan, electric motor, and machine tool
12/15/2011US20110303141 Floating flue
12/15/2011CA2743413A1 Aggregate vane assembly
12/14/2011EP2395214A1 Exhaust housing for a gas turbine and method for producing the same
12/14/2011EP2395201A2 A spring loaded seal assembly for turbines
12/14/2011CN202073602U 一种高耗能汽轮机的节汽装置 Section of a high-energy steam turbine unit
12/14/2011CN202073601U 透平膨胀机静叶系统及静叶调节缸 Turboexpander vanes systems and stationary blade adjustment cylinder
12/14/2011CN102282345A 带有渐增横截面排气壳体的涡轮增压器以及用于涡轮增压的方法 The method of increasing cross-section with the housing of the exhaust gas turbocharger and a turbocharged
12/14/2011CN102282340A 具有分段的导向叶片外圈的涡轮机导向叶片系统 With a segmented outer guide vane turbine guide vane system
12/14/2011CN102282339A 涡轮增压器和用于涡轮增压器的制造方法 Turbocharger and the manufacturing method for the turbocharger
12/14/2011CN102282338A 汽轮机 Turbine
12/14/2011CN102278146A 涡轮机导向叶片调节器 Turbine guide vane regulator
12/14/2011CN102278144A 多级压缩气体发动机及机动车 Multi-stage compression of the gas engine and vehicle
12/13/2011US8075264 Blade angle setting for a turbomachine
12/13/2011US8075259 Turbine vane airfoil with turning flow and axial/circumferential trailing edge configuration
12/13/2011US8075254 Developments relating to a rotor arrangement
12/08/2011WO2011151596A1 Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg
12/08/2011WO2011150979A1 Transonic gas turbine stage and method
12/08/2011WO2011128551A3 Flow straightener device for turbomachine
12/08/2011US20110299982 Method for repairing a guide blade segment for a jet engine
12/08/2011US20110299980 Gas turbine engine and a gas turbine engine component
12/08/2011CA2800262A1 Turbo machine with a device for preventing a segment of nozzle guide vanes assembly from rotating in a casing; rotation-proofing peg
12/07/2011EP2392775A1 Blade for use in a fluid flow of a turbine engine and turbine engine
12/07/2011EP2391804A1 Fluid expansion device and method with noise attenuation
12/07/2011CN202065055U Turbocharger
12/07/2011CN202065013U 汽轮机叶片 Turbine blades
12/07/2011CN102272419A 涡轮环组件 Turbine ring assembly
12/07/2011CN101240719B 带有反转高压和低压涡轮的燃气涡轮 With a reverse pressure and low-pressure turbine gas turbine
12/06/2011US8070432 Static gas turbine component and method for repairing such a component
12/06/2011US8070431 Fully contained retention pin for a turbine nozzle
12/06/2011US8070429 Turbine singlet nozzle assembly with mechanical and weld fabrication
12/06/2011US8070427 Gas turbines having flexible chordal hinge seals
12/06/2011US8070420 Airflow-cooling apparatus for a ceiling air-conditioning circulation machine
12/06/2011CA2622013C Vane assembly with grommet
12/06/2011CA2528049C Airfoil platform impingement cooling
12/06/2011CA2480393C Impingement cooling of gas turbine blades or vanes
12/01/2011WO2011150025A1 Gas turbine engine vane assembly with anti - rotating pin retention system
12/01/2011WO2011147510A2 Turbine for an exhaust gas turbocharger
12/01/2011WO2011124214A3 Guide blade of a turbomachine
12/01/2011WO2011095892A3 Turbocharger and turbocharger wheel housing
12/01/2011DE102010047252A1 Diffuser for gas flowing to exhaust gas turbine, has multiple guide vanes, of which one is designed to be adjustable for influencing flow of gas, where each of adjustable guide vanes is divided into two sections in direction of flow
12/01/2011DE102010047251A1 Control device for controlling gas flowing through exhaust gas turbocharger turbine for turbo compound system for e.g. passenger car, has wall and tension ring relatively rotated against each other by adjusting guide vanes
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