Patents
Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581)
01/2010
01/20/2010CN100582532C Leaf seal, particularly for a gas turbine, and method for the production thereof
01/20/2010CN100582441C Structural cover for gas turbine engine bolted flanges
01/14/2010WO2010003875A2 Method for operating a machine comprising a shaft seal
01/14/2010WO2010003405A1 Turbo-machine
01/14/2010US20100008782 Compliant Seal for Rotor Slot
01/14/2010US20100008773 Turbine blade and gas turbine equipped with a turbine blade
01/14/2010US20100008769 Sealing Mechanism with Pivot Plate and Rope Seal
01/14/2010US20100008756 Steam turbine and method of cooling steam turbine
01/14/2010US20100007091 Method of Forming a Brush Seal
01/14/2010DE102009026057A1 Dichtungsmechanismus mit Schwenkplatte und Seildichtung Seal mechanism with swivel plate and rope seal
01/14/2010DE102009026050A1 Nachgiebige Dichtung für einen Rotorschlitz Compliant seal for a rotor slot
01/14/2010DE102008032661A1 Strömungsmaschine Flow machine
01/13/2010EP2143889A2 Active tip clearance control for a gas turbine engine
01/13/2010EP2143888A2 Steam turbine and method of cooling steam turbine
01/13/2010EP2143887A2 Spring seal for blade dovetail
01/13/2010EP2143885A1 Gas Assisted Turbine Seal
01/13/2010EP2143881A2 Labyrinth seal for turbine blade dovetail root and corresponding sealing method
01/13/2010EP2143821A1 Discharge surface treatment method and repairing method
01/13/2010EP2142762A1 Shaft seal for steam turbines
01/13/2010CN101627184A Turbine ring assembly for gas turbine
01/13/2010CN101627183A Turbine ring assembly for gas turbine
01/13/2010CN101624921A Method, system, and apparatus for reducing a turbine clearance
01/13/2010CN101624920A Labyrinth seal for turbine blade dovetail root and corresponding sealing method
01/13/2010CN101624919A Gas assisted turbine seal
01/13/2010CN101624918A Sealing mechanism with pivot plate and rope seal
01/13/2010CN101624917A Compliant seal for rotor slot
01/12/2010US7645117 Rotary machines and methods of assembling
01/12/2010CA2465837C Fan blade with embrittled tip
01/07/2010WO2010001656A1 Cooling air supply structure of gas turbine and gas turbine
01/07/2010WO2010000795A1 Sealing system between a shroud segment and a rotor blade tip and manufacturing method for such a segment
01/07/2010WO2010000637A1 Seal and seal arrangement for confining leakage flows between adjacent components of turbo-maschines, in particular gas turbines
01/07/2010US20100003122 Turbo engine
01/06/2010EP2141392A2 A seal arrangement
01/06/2010EP2141363A2 Seal for turbomachine
01/06/2010EP2141328A1 Sealing system between a shroud segment and a rotor blade tip and manufacturing method for such a segment
01/06/2010EP2140973A1 Method and apparatus for selectively removing portions of an abradable coating using a water jet
01/05/2010US7641446 Turbine blade
01/05/2010US7641442 Device for controlling clearance in a gas turbine
12/2009
12/31/2009US20090324396 Accessory gearbox system with compressor driven seal air supply
12/31/2009US20090324394 Sealing arrangement in a gas turbine engine
12/31/2009US20090322035 Sealing device
12/31/2009US20090322031 Windback device
12/31/2009US20090322028 Seal arrangement
12/30/2009EP2138747A1 A sealing device
12/30/2009EP2138727A2 Blade shrouds with outlet
12/30/2009EP2138676A1 Method and device for cooling a component of a turbine
12/30/2009EP2137384A1 Turbine ring assembly for gas turbine
12/30/2009EP2137383A1 Hydrodynamic brush seal
12/29/2009CA2361103C Stator ring ventilation assembly
12/24/2009US20090319150 Method, system, and apparatus for reducing a turbine clearance
12/24/2009US20090317228 Apparatus and method for controlling a blade tip clearance for a compressor
12/24/2009DE102008029528A1 Gas i.e. cooling air, guiding device for use in gas turbine of aircraft engine, has two guiding elements provided at two adjacent rotor disks and dimensioned such that pre-determined gap is formed between guiding elements
12/23/2009EP2134951A1 Grid thrust reverser cover comprising a seal support and associated seal
12/23/2009EP2134926A1 Impulse turbine
12/22/2009US7635251 Stator assembly for a rotary machine
12/22/2009US7635250 Apparatus and method for controlling leakage in steam turbines
12/17/2009WO2009150905A1 Seal structure of rotary machine
12/16/2009EP2132414A1 Shiplap arrangement
12/15/2009CA2545954C Layer system and process for producing a layer system
12/15/2009CA2445770C Arrangement for mounting two coaxial shaftlines
12/10/2009WO2009148787A1 Non-contact seal for a gas turbine engine
12/10/2009WO2009126191A3 Sealing arrangement for turbine engine having ceramic components
12/10/2009US20090304498 Multistage turbomachine compressor
12/10/2009US20090304497 Guide blade segment of a gas turbine and method for its production
12/10/2009US20090304493 Axially oriented shingle face seal for turbine rotor and related method
12/10/2009DE102008027021A1 Sealing arrangement for sealing gap between two components, particularly rotor and stator of turbo-engine, has brush seal with bristles, which is arranged partially in receiving space of housing
12/10/2009DE102008026941A1 Device for connecting honeycomb seal with seal carrier for gas turbine, has lifting plunger with contour that is adapted to honeycomb seal, where honeycomb seal and seal carrier are compressible with crimping force using plunger
12/10/2009CA2726549A1 Non-contact seal for a gas turbine engine
12/09/2009EP2129875A2 Turbo engine
12/09/2009EP2129874A2 Sealing ring for turbo engines
12/09/2009EP2129873A2 Ceramic matrix composite abradable via reduction of surface area
12/09/2009CN101600854A Seal for a turbine engine
12/03/2009WO2009146258A1 Non-contact seal for a gas turbine engine
12/03/2009WO2009144191A1 High pressure turbine for turbine engine with improved mounting of the housing for controlling the radial clearance of mobile blades
12/03/2009US20090297330 Blade clearance arrangement
12/03/2009DE102009025835A1 Fluidische Abdichtung für Turbomaschinen Fluidic seal for turbomachinery
12/03/2009CA2725864A1 High pressure turbine for turbine engine with improved mounting of the housing for controlling the radial clearance of mobile blades
12/02/2009EP2125292A1 Method and device for the surface peening of a partial element of a component of a gas turbine
12/02/2009CN101595277A Hydraulic seal for a turbocharger
12/02/2009CN101592080A Annular bending type turbine engine
12/01/2009US7625177 Simple axial retention feature for abradable members
12/01/2009US7625171 Cooling system for a gas turbine engine
12/01/2009US7625170 CMC vane insulator and method of use
12/01/2009US7625169 Variable displacement turbine liner
11/2009
11/26/2009WO2009125078A3 Sectored distributor for turbomachine
11/26/2009WO2009118490A3 Turbine distributor for turbine engine
11/25/2009EP2123951A1 Leaf seal apparatus
11/24/2009US7621719 Multiple cooling schemes for turbine blade outer air seal
11/24/2009US7621716 Turbine case cooling
11/19/2009WO2008086782A3 Turbo engine having active clearance control
11/19/2009US20090285676 Continuous-flow machine, turbine, or compressor
11/19/2009US20090285675 Systems and Methods for Modifying Modal Vibration Associated with a Turbine
11/19/2009US20090285671 Vortex cooled turbine blade outer air seal for a turbine engine
11/18/2009EP2119874A1 Continuous-flow machine, in particular a turbine or compressor
11/18/2009EP2118448A2 Turbine ring assembly for gas turbine
11/18/2009CN201347775Y FW honeycomb type sealing structure with adjustment function
11/17/2009CA2430739C System to feed cooling air into a gas turbine rotor
11/17/2009CA2414992C Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
11/17/2009CA2413422C Draining and cooling system for gas turbine bearings
11/12/2009WO2009137319A1 In-line flow mixer
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