| Patents for F01D 9 - Stators (10,038) |
|---|
| 02/24/2011 | WO2011021693A1 Turbine cooling structure and turbine |
| 02/24/2011 | WO2010063271A3 Turbo engine |
| 02/24/2011 | DE102009037413A1 Turbinengehäuse mit Wandverkleidung Turbine housing with wall paneling |
| 02/23/2011 | CN201751539U Turbine guider lower edge plate cooling flow guiding structure |
| 02/23/2011 | CN201751538U Sectioned guider centering connection structure |
| 02/22/2011 | US7891943 Stator cascade of turbo type fluid machine |
| 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 | WO2011019422A2 Method of operating a heated guide vane assembly |
| 02/17/2011 | WO2011018413A1 Turbine diaphragms |
| 02/17/2011 | WO2011018299A1 Turbo engine having steam tapping |
| 02/17/2011 | US20110038732 Gas turbine engine composite blade |
| 02/17/2011 | DE102009037620A1 Strömungsmaschine Flow machine |
| 02/17/2011 | CA2774856A1 Method of operating a heated guide vane assembly |
| 02/16/2011 | EP2283218A2 Thermal insulation structure for structural member, and scroll structure |
| 02/10/2011 | WO2011015767A1 Rectifier stage for a turbine engine |
| 02/09/2011 | EP2282124A1 Method for retrofitting a combustion chamber of a gas turbine |
| 02/09/2011 | EP2282014A1 Ring-shaped flow channel section for a turbo engine |
| 02/09/2011 | EP2282013A2 Moisture removal provisions for steam turbine |
| 02/09/2011 | EP2282012A1 Guide vane of a gas turbine and method for replacing a cover plate of a guide vane of a gas turbine |
| 02/09/2011 | EP2282011A2 Cross-sectional profile of the supports or of the cover of the supports with supply lines of a Turbofan |
| 02/09/2011 | CN101970804A Sectored distributor for turbomachine |
| 02/09/2011 | CN101967996A Adjustable guide vane |
| 02/02/2011 | EP2280150A1 Gas turbine engine with integrated starter-generator and corresponding operating method |
| 02/02/2011 | CN1875169B Turbine cascade structure |
| 02/02/2011 | CN101963104A Power raising method for turboprop aero-engine |
| 01/27/2011 | US20110020118 Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
| 01/27/2011 | DE102009033753A1 Hollow turbine blade i.e. hollow guide vane, film cooling method, involves passive-controlling flow separation at blade, and bending nozzles under angle in transverse direction to mainstream direction of gas and under another angle |
| 01/26/2011 | EP2278125A2 Turbine nozzle assembly including radially-compliant spring member for gas turbine engine |
| 01/26/2011 | EP2276920A2 Subsonic and stationary ramjet engines |
| 01/26/2011 | EP2179143B1 Gap cooling between combustion chamber wall and turbine wall of a gas turbine installation |
| 01/26/2011 | EP2178752B1 Rear section of aircraft nacelle and nacelle equipped with such rear section |
| 01/26/2011 | CN201723256U Novel steam turbine |
| 01/26/2011 | CN101956606A Radial turbine engine |
| 01/26/2011 | CN101956576A Radial inlet guide vane adjuster |
| 01/26/2011 | CN101087928B Static gas turbine component and method for repairing such a component |
| 01/25/2011 | US7874794 Blade row for a rotary machine and method of fabricating same |
| 01/25/2011 | US7874791 Turbomachine |
| 01/25/2011 | CA2548973C Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine |
| 01/25/2011 | CA2528724C Internally cooled airfoil for a gas turbine engine and method |
| 01/20/2011 | WO2011008333A1 Heated guide vane |
| 01/20/2011 | WO2011007366A1 An improved turbine and method thereof |
| 01/20/2011 | US20110014043 System for controlling the cowl of a turbojet engine nacelle thrust reverser |
| 01/20/2011 | US20110014041 Rotary Drum of an Axial Compressor Having a Composite Web |
| 01/20/2011 | US20110014040 Fluid flow machine with blade row group |
| 01/20/2011 | DE102009033591A1 Strömungsarbeitsmaschine mit Schaufelreihengruppe Flow machine with blade row group |
| 01/20/2011 | DE102009031229A1 Guide vane for e.g. variable turbine of supercharger, in motor vehicle, has turning points provided between nose circle and largest construction circle that is placed in flow direction behind nose circle, where vane has dolphin shape |
| 01/20/2011 | CA2766446A1 Heated guide vane |
| 01/19/2011 | EP2275647A2 Flow working machine with rotor series group |
| 01/19/2011 | EP1400755B1 Flanged hollow structure |
| 01/19/2011 | CN101952574A Thermal insulation structure for structural member, and scroll structure |
| 01/19/2011 | CN101952556A Rotary machine scroll structure and rotary machine |
| 01/19/2011 | CN101949306A Bidirectional-starting pressure limited type high-speed engine for hydraulic air-jet fly-wheel gas-turbine rotor |
| 01/19/2011 | CN101949305A Turbocharger composite nozzle device |
| 01/19/2011 | CN101575989B Turbine nozzle and design method thereof |
| 01/19/2011 | CN101324193B Radial double-flow turbine |
| 01/18/2011 | US7871242 Single actuator controlled rotational flow balance system |
| 01/18/2011 | CA2374753C Apparatus for reducing combustor exit duct cooling |
| 01/13/2011 | WO2011005337A1 Composite turbine nozzle segment |
| 01/13/2011 | WO2011005336A1 Composite nozzle segment and support frame assembly |
| 01/13/2011 | WO2010019175A3 Transition duct for gas turbine combustor with inlet and outlet circumferentially offset |
| 01/13/2011 | US20110008163 Composite article and support frame assembly |
| 01/13/2011 | US20110008157 Turbine stator airfoils with individual orientations |
| 01/13/2011 | US20110008156 Composite turbine nozzle |
| 01/13/2011 | DE102009032452A1 Loading device i.e. exhaust gas turbocharger, for motor vehicle, has rotatably supported guide vanes, and adjusting ring e.g. translationally supported adjusting slider, for adjusting guide vanes orthogonal to axis of device |
| 01/12/2011 | EP2273071A2 Turbine stator airfoils with individual crystallographic orientations |
| 01/12/2011 | EP2271843A1 Fluid intake assembly |
| 01/12/2011 | EP2271828A1 Turbine nozzle box for a turbomachine |
| 01/12/2011 | CN101946063A Gas turbine |
| 01/12/2011 | CN101943030A Variable geometry vane assembly for a turbocharger |
| 01/12/2011 | CN101943029A System, method, and apparatus for linking machine stator |
| 01/11/2011 | US7866041 Method of manufacturing a duct for a gas turbine engine |
| 01/11/2011 | CA2412898C Connecting system for a transition duct in a gas turbine |
| 01/06/2011 | WO2011002605A1 Nickel base superalloy compositions and superalloy articles |
| 01/06/2011 | CA2766552A1 Nickel base superalloy compositions and superalloy articles |
| 01/05/2011 | EP2268902A1 Strut for an intermediate turbine housing, intermediate turbine housing, and method for producing an intermediate turbine housing |
| 01/05/2011 | EP2134925B1 Exhaust gas turbocharger and method for the operation thereof |
| 01/05/2011 | DE19926949B4 Kühlungsanordnung für Schaufeln einer Gasturbine Cooling arrangement for a gas turbine blades |
| 01/05/2011 | CN101936193A Method for manufacturing integral nozzle block of large-sized steam turbine |
| 01/05/2011 | CN101936192A Cantilever blade machining method |
| 01/04/2011 | US7862295 Device for guiding a stream of air entering a combustion chamber of a turbomachine |
| 01/04/2011 | US7861525 Dual volute turbocharger |
| 12/30/2010 | US20100329836 Method of operating a heated guide vane assembly |
| 12/30/2010 | DE112008003452T5 Turbinenleitapparatsegment und -anordnung Turbine nozzle and arrangement |
| 12/29/2010 | WO2010149528A1 Annular flow channel section for a turbomachine |
| 12/29/2010 | EP2267273A2 Adjustable camber aerofoil |
| 12/29/2010 | EP2265799A1 Guide vane for a gas turbine |
| 12/29/2010 | CN201687527U Spray nozzle of turboexpander |
| 12/29/2010 | CN1952353B Optimized nozzle box steam path |
| 12/28/2010 | US7857580 Turbine vane with end-wall leading edge cooling |
| 12/23/2010 | WO2010146288A1 Turbine distributor element made of cmc, method for making same, distributor and gas turbine including same |
| 12/23/2010 | WO2010105597A3 Tandem blade design |
| 12/23/2010 | US20100322760 Interlocked CMC Airfoil |
| 12/23/2010 | US20100322755 Use of non-uniform nozzle vane spacing to reduce acoustic signature |
| 12/23/2010 | US20100319352 Prechorded turbine nozzle |
| 12/23/2010 | DE102010017314A1 In Sehnenrichtung vorgeformter Turbinenleitapparat Chordwise preformed turbine nozzle |
| 12/23/2010 | CA2765021A1 Turbine distributor element made of cmc, method for making same, distributor and gas turbine including same |
| 12/22/2010 | EP2264284A1 Method for manufacturing vanes built into a shroud ring and stator ring obtained according to the method |
| 12/22/2010 | EP2264282A2 Cooled gas turbine stator assembly |
| 12/22/2010 | EP2263862A1 Method for manufacturing braided preforms |