| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
|---|
| 04/23/2013 | US8425184 Turbine shroud ring with rotation proofing recess |
| 04/23/2013 | CA2711914C Self-monitoring system for evaluating and controlling adjustment requirements of leakage restricting devices in rotodynamic pumps |
| 04/18/2013 | WO2013054043A1 Cooling for the retaining dovetail of a turbomachine blade |
| 04/18/2013 | US20130094946 Turbine shroud thermal distortion control |
| 04/18/2013 | US20130094945 Seal structure, turbine machine having the same, and power generating plant equipped with the same |
| 04/18/2013 | US20130094944 Bucket assembly for turbine system |
| 04/18/2013 | US20130091940 Method and System for Determining Gas Turbine Tip Clearance |
| 04/17/2013 | EP2581555A1 Turbomachine Component having a Flow Contour Feature |
| 04/17/2013 | EP2580434A1 Method for adjusting the radial gap between blade tips of turbine blades and a channel wall, and device for measuring a radial gap of an axially permeable turbomachine |
| 04/17/2013 | EP2580432A1 Turbine blade seal assembly |
| 04/17/2013 | EP2580428A1 Cooling fluid metering system for a turbine blade |
| 04/17/2013 | CN103052766A Component of a turbine with leaf seals and method for sealing against leakage between a vane and a carrier element |
| 04/17/2013 | CN103047015A System for sealing a shaft |
| 04/11/2013 | US20130089421 Gas turbine engine airfoil tip recesses |
| 04/11/2013 | US20130089414 Strip seals |
| 04/11/2013 | DE102012109479A1 Turbomaschinenrotor mit gemusterter Beschichtung Turbomachinery rotor having a patterned coating |
| 04/11/2013 | DE102011084125A1 Blade segment for turbomachine e.g. gas turbine for aircraft engine, has upper shroud which interconnects blades to each other, and lower shroud is divided into several portions which are firmly connected to the blades |
| 04/10/2013 | EP2578910A1 Strip seals |
| 04/10/2013 | EP2578811A1 Method for determining position of rotating blades having variable thickness. |
| 04/10/2013 | EP2578810A1 Seal structure, turbine machine equipped with same, and power plant equipped with said turbine machine |
| 04/10/2013 | EP2578806A2 Tip shroud assembly with contoured seal rail fillet |
| 04/10/2013 | EP2578804A1 Light weight abradable air seal, corresponding gas turbine engine and process of manufacturing |
| 04/10/2013 | EP2577117A1 Method for fastening a brush sealing element in a groove of a housing segment |
| 04/10/2013 | EP2576999A1 Compressor case lining |
| 04/10/2013 | EP2576994A1 Method and system for controlling the clearance at the blade tips of a turbine rotor |
| 04/10/2013 | EP2576993A2 Gas turbine engine sealing structure |
| 04/10/2013 | CN202866903U Brush type honeycomb vapor seal |
| 04/10/2013 | CN103032117A Installation comprising steam turbine modules with optimized efficiency |
| 04/10/2013 | CN103032107A Tip shroud assembly with contoured seal rail fillet |
| 04/10/2013 | CN103032106A Turbocharger variable-nozzle assembly with vane sealing arrangement |
| 04/10/2013 | CN101899994B Semi-drain steam turbine |
| 04/09/2013 | US8414255 Impingement cooling arrangement for a gas turbine engine |
| 04/09/2013 | US8414254 Sealing assembly for a turbine engine |
| 04/09/2013 | US8413992 Shaft seal and rotary machine with same |
| 04/09/2013 | CA2548894C Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine |
| 04/09/2013 | CA2507192C Method for coating gas turbine engine components |
| 04/05/2013 | CA2791040A1 Gas turbine engine airfoil tip recesses |
| 04/04/2013 | WO2013049456A2 A method of repairing rotating machine components |
| 04/04/2013 | WO2013048072A1 Reactive turbine apparatus |
| 04/04/2013 | US20130084169 Tip Shroud Assembly with Contoured Seal Rail Fillet |
| 04/04/2013 | US20130084168 Clearance flow control assembly having rail member |
| 04/04/2013 | US20130084167 Wear-resistant coating and use thereof |
| 04/04/2013 | US20130084165 Installation comprising steam turbine modules with optimized efficiency |
| 04/04/2013 | DE102011083814A1 Segmentiertes Bauteil Segmented component |
| 04/04/2013 | CA2848944A1 A method of repairing rotating machine components |
| 04/03/2013 | EP2574732A2 Gas turbine |
| 04/03/2013 | EP2574731A2 Segmented component |
| 04/03/2013 | EP2574728A1 Clearance flow control assembly having rail member and corresponding turbine |
| 04/03/2013 | EP2574727A1 Blade air seal with integral thermal barrier corresponding gas turbine engine and method of manufacturing |
| 04/03/2013 | EP2574545A2 Wear Resistant Coating and Use Thereof |
| 04/03/2013 | CN202851974U Tooth-shaped structure capable of self-restraining effective flow area |
| 04/03/2013 | CN202851091U Tooth top clearance local resistance-increasing seal tooth type structure |
| 04/03/2013 | CN103026004A Turbine including seal air valve system |
| 04/03/2013 | CN103016078A Air cycle machine shaft support assembly |
| 04/03/2013 | CN103016070A Turbocharger variable-nozzle assembly with vane sealing arrangement |
| 03/28/2013 | WO2013042660A1 Turbine |
| 03/28/2013 | WO2012022550A3 Sealing device |
| 03/28/2013 | US20130078085 Blade air seal with integral barrier |
| 03/28/2013 | US20130078084 Airfoil air seal assembly |
| 03/27/2013 | EP2573364A2 Turbocharger with variable nozzle having labyrinth seal for vanes |
| 03/27/2013 | EP2573330A2 Compliant mounting of an axial face seal assembly |
| 03/27/2013 | EP2573329A2 Air system architecture for a mid-turbine frame module |
| 03/27/2013 | EP2573326A1 Airfoil tip air seal assembly |
| 03/27/2013 | EP2572097A1 Airplane jet engine thrust reverser having gratings or cascades |
| 03/27/2013 | CN103003529A Method and system for controlling the clearance at the blade tips of a turbine rotor |
| 03/27/2013 | CN103003526A Internal cooling for a flow machine |
| 03/27/2013 | CN102996258A Non-continuous ring seal |
| 03/27/2013 | CN102996186A 320 MW steam turbine nozzle group |
| 03/27/2013 | CN101910586B Compressor for a gas turbine |
| 03/27/2013 | CN101220757B 汽轮机 Turbine |
| 03/26/2013 | US8403637 Thermal control system for turbines |
| 03/21/2013 | WO2013037849A1 Labyrinth seal |
| 03/21/2013 | US20130071235 Light weight abradable air seal |
| 03/21/2013 | US20130071234 Abradable panel and method of forming the same |
| 03/21/2013 | US20130071227 Blade outer air seal assembly leading edge core configuration |
| 03/21/2013 | US20130069313 Turbomachine secondary seal assembly |
| 03/21/2013 | CA2846090A1 Labyrinth seal |
| 03/20/2013 | EP2570704A1 Method for fabricating shaft sealing device and jig for fabricating shaft sealing device, and rotary machine provided with shaft sealing device |
| 03/20/2013 | EP2570615A1 Self-adjusting device for controlling the clearance between rotating and stationary components of a turbomachine |
| 03/20/2013 | EP2570614A2 Air cushion seal |
| 03/20/2013 | EP2570613A2 Blade Outer Air Seal Assembly Leading Edge Core Configuration |
| 03/20/2013 | EP2570612A1 Turbomachine secondary seal assembly |
| 03/20/2013 | EP2570611A2 Ceramic matrix composite airfoil for a gas turbine engine and corresponding method of forming |
| 03/20/2013 | EP2570610A2 Ceramic matrix composite vane structure for a gas turbine engine and corresponding low pressure turbine |
| 03/20/2013 | EP2570608A2 Ceramic matrix composite rotor module for a gas turbine engine, corresponding turbine assembly and method of assembling |
| 03/20/2013 | EP2570604A2 Ceramic matrix composite airfoil for a gas turbine engine, corresponding vane structure and method of forming |
| 03/20/2013 | EP2570603A2 Ceramic matrix composite platform assembly for an airfoil of a gas turbine engine and corresponding rotor disk assembly |
| 03/20/2013 | EP2570602A2 Ceramic matrix composite vane structure for a gas turbine engine, corresponding low pressure turbine and assembling method |
| 03/20/2013 | EP2569460A2 Abradable lining of a turbomachine and method of production |
| 03/20/2013 | CN202810959U Active gap control actuating mechanism and control system comprising same |
| 03/20/2013 | CN202810953U Worm wheel assembly |
| 03/20/2013 | CN102985641A Method for adjusting the radial gap between blade tips of turbine blades and a channel wall, and device for measuring a radial gap of an axially permeable turbomachine |
| 03/20/2013 | CN102985639A Sealing element for sealing a gap |
| 03/20/2013 | CN102985582A Method for producing a rotor/stator seal of a gas turbine |
| 03/20/2013 | CN102979585A Sealing structure |
| 03/19/2013 | US8397506 Turbo-alternator-compressor design for supercritical high density working fluids |
| 03/14/2013 | WO2013035638A1 Steam turbine facility |
| 03/14/2013 | WO2013034837A1 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 |
| 03/14/2013 | WO2013034655A1 Seal for a rotary machine |
| 03/14/2013 | WO2013034385A1 Guide device for a turbine |