Patents
Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581)
08/2012
08/08/2012CN102630268A Insulation of a circumferential edge of an outer casing of a turbine engine from a corresponding ring sector
08/02/2012WO2012101380A1 Turbine engine stage
08/02/2012WO2012052961A8 Gas turbine provided with a cooling circuit for tip sections of rotor blades
08/02/2012US20120195743 Flexible seal for turbine engine
08/02/2012US20120195742 Turbine bucket for use in gas turbine engines and methods for fabricating the same
08/02/2012DE112010002761T5 Mehrstufige Turboladeranordnung Multi-stage turbocharger assembly
08/02/2012DE112009002594T5 Mantelringaufhängung mit verbreitetem Kühlkanal Shell ring with suspension-spread cooling channel
08/02/2012DE102012100771A1 Verfahren und Vorrichtung für einen Labyrinthdichtungspackungsring Method and apparatus for a labyrinth packing ring
08/02/2012CA2825260A1 Turbine engine stage
08/01/2012EP2481890A2 Seal in a gas turbine engine component having a coating with abradability proportional to interaction rate
08/01/2012EP2481889A2 Plasma actuation systems to produce swirling flows
08/01/2012EP2481888A2 Flexible seal for use between turbine engine segments
08/01/2012EP2481887A2 Intershaft seal with support linkage
08/01/2012EP2481886A1 Brush seal with rear cutting
08/01/2012EP2054588B1 Turbine blade assembly
08/01/2012CN202360153U Cooling and sealing device for turbine disc of stack gas turbine
08/01/2012CN102619577A Device for inhibiting clearance leakage of blade tip and reducing steam flow exciting force
08/01/2012CN102619576A Flexible seal for turbine engine
08/01/2012CN102619568A Shell distribution type pneumatic motor with spherical blades
07/2012
07/28/2012CA2765666A1 Plasma actuation systems to produce swirling flows
07/26/2012WO2012099938A1 Seal with stacked sealing elements
07/26/2012WO2012097798A1 Intermediate housing of a gas turbine with an outer bounding wall, having upstream of a supporting rib a contour that changes in the circumferential direction, for reducing secondary flow losses
07/26/2012US20120189435 Assembly for preventing fluid flow
07/26/2012US20120189426 Blade outer air seal assembly and support
07/26/2012DE102012100521A1 Anordnung zur Verhinderung eines Fluiddurchflusses Arrangement for preventing fluid flow
07/26/2012DE102011003173A1 Gassystem zur Verdichtung eines Prozessgases Gas system for compressing a process gas
07/26/2012CA2824292A1 Seal with stacked sealing elements
07/25/2012EP2479385A2 Blade outer air seal assembly and support
07/25/2012EP2479384A2 Mateface Cooling Feather Seal Assembly
07/25/2012EP2478188A1 Sealing segment for a continuous-flow machine
07/25/2012CN102606226A Vapour turbine
07/25/2012CN102606225A Assembly for preventing fluid flow
07/25/2012CN102606223A Flue gas turbine
07/25/2012CN102606217A Pneumatic motor with cylindrical blades
07/24/2012US8226362 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine
07/24/2012CA2509743C Turbine vane collar seal
07/24/2012CA2480584C Turbine engine with two sections connected by a joint
07/19/2012US20120183393 Assembly and method for preventing fluid flow
07/19/2012DE102011055611A1 Dichtungsanordnung zur Verwendung in Turbomaschinen und Verfahren zur Montage derselben Seal assembly for use in turbomachinery and method of assembling same
07/19/2012DE102011055152A1 Anordnung und Verfahren zur Verhinderung eines Fluidflusses Apparatus and method for preventing fluid flow
07/18/2012EP2475847A1 Clearance control at the blade tips of a turbomachine
07/18/2012CN102597583A Hydrodynamic circumferential seal system for large translations
07/18/2012CN102597425A Method for protecting the passage of air in a drive part coupling in an unprotected environment, coupling for implementation, and rotor line fitted with such couplings
07/18/2012CN102588008A Three-point centring adjustment device for low-pressure shaft end steam seal of steam turbine
07/18/2012CN102588007A Combination method for steam seals of steam turbine
07/18/2012CN102588006A Systems, methods, and apparatus for a turbine interstage rim seal
07/18/2012CN102588005A Assembly and method for preventing fluid flow
07/18/2012CN102587995A Rotor of steam turbine for driving water feeding pump of boiler with power lower than 300MW (megawatt) and starting method of rotor
07/17/2012US8221062 Device and system for reducing secondary air flow in a gas turbine
07/12/2012WO2012093217A1 Method for damping a gas-turbine blade, and vibration damper for implementing same
07/12/2012US20120177486 Runner for circumferential seals
07/12/2012US20120177485 Cover plate with interstage seal for a gas turbine engine
07/12/2012US20120177483 System for adjusting brush seal segments in turbomachine
07/12/2012CA2823504A1 Method for damping a gas-turbine blade, and vibration damper for implementing same
07/11/2012EP2474762A1 Elliptical sealing system
07/11/2012EP2474711A2 Runner for circumferential seals
07/11/2012EP2474708A2 Interstage seal for a gas turbine engine and corresponding assembly method
07/11/2012EP2473713A1 Device for supporting a turbine ring, turbine having such a device, and turbine engine having such a turbine
07/11/2012CN102575526A Gas turbine nozzle arrangement and gas turbine
07/11/2012CN102562299A System and method to eliminate a hard rub and optimize a purge flow in a gas turbine
07/11/2012CN102562171A Spherical blade pneumatic motor
07/10/2012US8215903 Use of a thermal barrier coating for a housing of a steam turbine, and a steam turbine
07/10/2012CA2649515C Shroud segment arrangement for gas turbine engines
07/10/2012CA2523192C Turbine shroud segment seal
07/05/2012WO2012090793A1 Shaft sealing device, and rotary machine equipped therewith
07/05/2012WO2012045034A3 Aircraft engine systems and methods for operating same
07/05/2012WO2012030783A3 Turbocharger housing seal
07/05/2012US20120171023 Mounting apparatus for low-ductility turbine shroud
07/05/2012US20120167584 Controlling blade tip clearances in a turbine engine
07/05/2012DE102011057130A1 Systeme, Verfahren und Vorrichtungen für eine Turbinenzwischenstufenranddichtung Systems, methods and apparatus for a turbine interstage seal edge
07/04/2012EP2472065A1 Damper coverplate and sealing arrangement for turbine bucket shank
07/04/2012CN202300537U 低齿刷式汽封 Low tooth brush steam seal
07/04/2012CN102536882A Abradable for stator inner shroud
07/04/2012CN102536338A Cloth seal for turbo-machinery
07/03/2012CA2503149C Sheet metal turbine or compressor static shroud
06/2012
06/30/2012CA2762613A1 Structural low-ductility turbine shroud apparatus
06/30/2012CA2762609A1 Mounting apparatus for low-ductility turbine shroud
06/28/2012WO2012086757A1 Turbine
06/28/2012US20120163955 System and method to eliminate a hard rub and optimize a purge flow in a gas turbine
06/27/2012EP2469037A2 Water self-sufficient turbine system
06/27/2012EP2469036A2 Flue gas diverter damper seal land
06/27/2012EP2469034A2 Turbine stator vane having a platform with a cooling circuit and corresponding manufacturing method
06/27/2012CN102518477A Finger sealing device
06/27/2012CN102518476A Zero leakage sealing device for oil cylinder piston rod of steam turbine
06/27/2012CN101148993B Methods and apparatus for fabricating turbine engines
06/26/2012US8206092 Gas turbine engines and related systems involving blade outer air seals
06/26/2012US8206083 Carbon hydrostatic face seal
06/26/2012US8206082 Packing seal rotor lands
06/26/2012CA2491666C Improvements to the device to control the play in a gas turbine
06/26/2012CA2484944C Miniature gas turbine engine with unitary rotor shaft for power generation
06/26/2012CA2483391C Attachment of a ceramic shroud in a metal housing
06/24/2012CA2762694A1 Gas turbine engine flow path member
06/21/2012WO2012082221A1 Buffer air for a labyrinth seal
06/21/2012US20120156012 Flow machine for a fluid having a radial sealing gap and a stationary wear ring
06/21/2012US20120156011 Air cycle machine seal land
06/21/2012US20120156008 Air cycle machine seal plate and seal land
06/21/2012DE102011081323B3 Fluid-flow machine i.e. axial-flow gas turbine, has abradable abrasion layer arranged at blade tip adjacent to radial inner side of housing and made of specific mass percent of zirconium oxide stabilized ytterbium oxide
06/21/2012DE102010063594A1 Sealing arrangement for use in airplane thruster to prevent leakage in gap between e.g. guide vanes, has high temperature-fixed sealing web arranged between component portions of two static components to seal gap between component portions
06/20/2012EP2466075A2 Clearance control arrangement for a gas turbine engine
06/20/2012EP2466074A1 Gas turbine engine with piston ring sealing device
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