Patents
Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581)
06/2006
06/29/2006DE102004059858A1 Lamellendichtung, insbesondere für eine Gasturbine Lamellar seal, in particular for a gas turbine
06/28/2006EP1674659A2 Turbine nozzle with bullnose step-down platform
06/28/2006EP1673519A1 Sealing arrangement for a gas turbine
06/27/2006US7067181 Insulating ceramic based on partially filled shapes
06/27/2006US7066719 Bore and shaft assembly
06/27/2006US7066713 Rotor blade for a rotary machine
06/27/2006US7066470 Active seal assembly
06/22/2006WO2006046969A3 Turbine case reinforcement in a gas turbine jet engine
06/22/2006US20060131815 Honeycomb seal
06/21/2006EP1672172A1 Turbine engine rotor stack
06/21/2006EP1672171A2 Turbine engine rotor with stacked disks
06/21/2006CN2789416Y Reverse spiral-flow antiexciting steam sealing gland of turbine
06/20/2006US7063503 Turbine shroud cooling system
06/15/2006WO2006061324A1 Lamellar seal, especially for a gas turbine
06/15/2006US20060127660 Intermetallic material and use of said material
06/15/2006CA2590253A1 Leaf seal, in particular for a gas turbine
06/14/2006EP1668225A1 Variable geometry turbocharger
06/14/2006EP1114241B1 Sealing ring for non-hermetic fluid seals
06/14/2006DE102004059904A1 Moving blade e.g. for turbo machine, has blade point which faces stator in turbo machine and contacts into channel of stator with blade point provided in such way that blade contacts channel at its edges and into rotor
06/14/2006DE102004058487A1 Gasturbine Gas turbine
06/14/2006DE102004050739B4 Gas turbine has slits in radially outer ends of vanes of rotor to contain radially movable sealing element sealing gap between vane and housing
06/14/2006CA2528135A1 Clamp lock brush seal assembly
06/13/2006US7059835 Turbine, in particular a gas turbine, and a blade
06/13/2006US7059831 Turbine engine disk spacers
06/13/2006US7059829 Compressor system with movable seal lands
06/13/2006US7059827 Turbine power plant having minimal-contact brush seal augmented labyrinth seal
06/13/2006US7059821 Method and apparatus to facilitate sealing within turbines
06/10/2006CA2528730A1 Gas turbine gas path contour
06/08/2006WO2006060013A1 Seal assembly for a fan rotor of a tip turbine engine
06/08/2006WO2006059994A1 Seal assembly for a fan-turbine rotor of a tip turbine engine
06/08/2006US20060120861 Mounting structure for a packing ring seal segment in a turbine
06/08/2006US20060120860 Methods and apparatus for maintaining rotor assembly tip clearances
06/07/2006EP1666700A2 Gas turbine
06/07/2006EP1664489A1 Gas turbine and sealing means for a gas turbine
06/07/2006EP1343951B1 Turbine bucket cover and brush seal
06/07/2006CN2786283Y Turbine supercharger
06/07/2006CN1258638C Internal flow type turbine and internal flow type compressor
06/06/2006US7056087 Traction drive shaft seal
06/03/2006CA2768660A1 Rotor assembly with cooling air deflectors and method
06/01/2006WO2006057602A1 Axial flow turbine with overspeed preventing device
06/01/2006US20060115356 Casing arrangement
06/01/2006DE202005006522U1 Device for reducing of sealed gap losses has inter-engaging labyrinth seals for rotating component and casing, with gap width of labyrinth seal adjustable by movement of one half of seal
05/2006
05/31/2006EP1662093A1 Zusammenbau von Leitsegmente in einem axialen Kompressor
05/30/2006US7052527 Thermal spray composition and method of deposition for abradable seals
05/30/2006US7052240 Rotating seal arrangement for turbine bucket cooling circuits
05/30/2006US7052235 Turbine engine shroud segment, hanger and assembly
05/30/2006US7052234 Turbine vane collar seal
05/30/2006US7052231 Methods and apparatus for injecting fluids in gas turbine engines
05/30/2006US7052017 Rotary machine with seal
05/30/2006US7052015 Cooling arrangement for brush seal
05/25/2006US20060110255 Controlled leakage pin and vibration damper for active cooling and purge of bucket slash faces
05/25/2006US20060110254 Thermal barrier coating for turbine bucket platform side faces and methods of application
05/24/2006EP1658925A1 Process for producing a compressor housing
05/24/2006EP1658455A2 Fluid-cooled mechanical face seal rotor
05/24/2006DE19654471B4 Rotor einer Strömungsmaschine Rotor of a turbomachine
05/24/2006CN2782937Y Mechanical vane of impeller for inhibiting top gap leakage
05/23/2006US7048497 Gas turbine stator
05/23/2006US7048496 Turbine cooling, purge, and sealing system
05/18/2006WO2006029843A8 Shroud for a gas turbine
05/18/2006DE102004054930A1 Rotor einer Turbomaschine, insbesondere Gasturbinenrotor Rotor of a turbomachine, in particular a gas turbine rotor
05/17/2006EP1657407A1 Method and apparatus for the cooling of the outer shrouds of the rotor blades of a gas turbine
05/17/2006EP1657406A2 Static seal structure
05/17/2006EP1656493A1 Labyrinth seal in a stationary gas turbine
05/17/2006CN2780997Y Cellular contact glant sealing
05/17/2006CN1774560A Center-located cutter teeth on shrouded turbine blades
05/16/2006US7044710 Gas turbine arrangement
05/16/2006US7044709 Methods and apparatus for coupling ceramic matrix composite turbine components
05/16/2006CA2344137C Steam control apparatus for turbine
05/11/2006WO2006001825A3 Gas turbine cooled shroud assembly with hot gas ingestion suppression
05/11/2006US20060099069 Seal structure
05/11/2006DE102004025692B4 Brazing construction for abradable sealing material used in turbine, includes infiltration prevention agent which is filled on non-brazing side upto specific depth so as to restrict infiltration of brazing filler metals
05/10/2006EP1655455A1 Turbomachine having a guide vane support with adjustable radial clearance
05/10/2006EP1654441A1 Run-in coating for gas turbines composed of a titanium-aluminium material
05/10/2006EP1654440A1 Gas turbine having a sealing element between the vane ring and the moving blade ring of the turbine part
05/10/2006CN1769653A Element of turbomachinery with cool unit
05/10/2006CN1769652A Unit for sealing transition region between two parts cool passage of turbomachinery
05/09/2006US7040861 Method and apparatus for reducing self sealing flow in combined-cycle steam turbines
05/09/2006US7040857 Flexible seal assembly between gas turbine components and methods of installation
05/09/2006US7040098 Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions
05/09/2006CA2367711C Blade structure in a gas turbine
05/04/2006WO2006046969A2 Turbine case reinforcement in a gas turbine jet engine
05/04/2006US20060093484 Cooling system for a platform of a turbine blade
05/04/2006US20060091611 Nested can brush seal
05/04/2006CA2566359A1 Turbine case reinforcement in a gas turbine jet engine
05/03/2006EP0979961B1 Seal apparatus for rotary machines
05/03/2006CA2525045A1 Nested can brush seal
05/02/2006US7037079 Axial-flow thermal turbomachine
05/02/2006US7037071 Device for maintaining joints with sealing leaves
05/02/2006US7037067 Gas turbine engine
04/2006
04/27/2006WO2006043987A2 Method and system for improved blade tip clearance in a gas turbine jet engine
04/25/2006US7033138 Ring segment of gas turbine
04/25/2006US7032904 Inner air seal anti-rotation device
04/25/2006US7032903 Brush-seal designs for turbines and similar rotary apparatus
04/20/2006US20060083620 Cooling system for a seal for turbine vane shrouds
04/20/2006US20060083607 Turbine shroud segment seal
04/20/2006DE102004050739A1 Gas turbine has slits in radially outer ends of vanes of rotor to contain radially movable sealing element sealing gap between vane and housing
04/19/2006EP1647744A1 A sealing arrangement
04/19/2006CN1252376C Turbo-machine comprising sealing system for rotor
04/18/2006US7029232 Abradable seals
04/18/2006US7029228 Method and apparatus for convective cooling of side-walls of turbine nozzle segments
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