Patents
Sitemap › F01 - Machines or engines in general; Engine plants in general; Steam engines › F01D - Non-positive-displacement machines or engines, e.g. steam turbines › F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages
Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581)
11/2005
11/16/2005EP1596037A2 Blade arrangement
11/16/2005EP1595058A1 Sealing arrangement, particularly for the blade segments of gas turbines
11/15/2005CA2228786C Ventilation system for platforms of moving vanes
11/15/2005CA2196642C Labyrinth disk with built-in stiffener for turbomachine rotor
11/10/2005WO2005106210A1 Exhaust gas turbocharger with adjustable slide ring
11/10/2005WO2005106208A1 Blade for a gas turbine
11/10/2005WO2005106207A1 Compressor blade and compressor
11/10/2005US20050249590 Turbomachine, for example a turbojet for an airplane
11/10/2005US20050249588 Seal assembly
11/10/2005US20050249443 Installation layout for two coaxial shaft lines
11/10/2005US20050248100 Stationary ring assembly for a gas turbine
11/10/2005US20050247061 Method of and apparatus for cooling a seal for machinery
11/10/2005DE102005017150A1 Flexible Dichtungsanordnung zwischen Gasturbinenkomponenten und Verfahren zur Installierung Flexible sealing arrangement between gas turbine components and method of installing
11/10/2005DE102005017148A1 Drehdichtungsanordnung für Kühlkreisläufe von Turbinenschaufeln Rotary seal assembly for cooling circuits of turbine blades
11/10/2005DE102004020378A1 Lamellendichtung, insbesondere für eine Gasturbine, sowie Verfahren zu deren Herstellung Lamellar seal, in particular for a gas turbine, as well as processes for their preparation
11/09/2005EP1593814A1 Feather seal configuration for a gas turbine shroud
11/08/2005US6962482 Turbine shroud segment
11/08/2005US6962342 System for sealing off a gap
11/08/2005CA2368555C Gas turbine split ring
11/03/2005WO2005103534A1 Leaf seal, particularly for a gas turbine, and method for the production thereof
11/03/2005WO2005102592A1 Method for producing a honeycomb seal
11/03/2005WO2005056878A3 Running-in coating for gas turbines and method for production thereof
11/03/2005US20050242526 Hot gas seal
11/03/2005US20050242522 Seal between the inner and outer casings of a turbojet section
11/03/2005US20050242520 Mixing equipment sealing device
11/02/2005EP1591626A1 Blade for gas turbine
11/02/2005EP1591624A1 Compressor blade and compressor.
11/02/2005EP1591623A2 Turbine engine and assembly method for this engine
11/02/2005EP1591622A2 Turbine Engine disk spacers
11/02/2005CN1690389A Rotating seal arrangement for turbine bucket cooling circuits
11/01/2005US6960060 Dual coolant turbine blade
11/01/2005CA2223156C Brush seal with a core ring wrapped by bristle bundles
10/2005
10/27/2005US20050238477 Stator of a high-pressure turbine of a turbomachine, and a method of assembling it
10/26/2005EP1589190A2 Steam turbine rotor cooling at oil deflector
10/25/2005CA2366758C Stationary blade shroud of a gas turbine
10/20/2005US20050233160 Thermal spray compositions for abradable seals
10/20/2005US20050232777 Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge
10/20/2005US20050232775 Device for fixing a rotor on a shaft
10/20/2005US20050232774 Turbine engine rotor retainer
10/20/2005US20050232773 Turbine engine disk spacers
10/20/2005US20050232772 Rotating seal arrangement for turbine bucket cooling circuits
10/20/2005US20050232764 Flexible seal assembly between gas turbine components and methods of installation
10/20/2005US20050232752 Turbine shroud cooling system
10/19/2005EP1586743A1 Turbine shroud
10/19/2005EP1586742A2 Method and apparatus for reducing self-sealing flow in combined-cycle steam turbines
10/19/2005EP1585888A1 Sealing means for a lubrication system in a turbocharger
10/19/2005CN1683772A Turbine shroud
10/19/2005CN1683766A Flexible seal assembly between gas turbine components and methods of installation
10/15/2005CA2503066A1 Turbine ring
10/15/2005CA2502810A1 Turbine shroud cooling system
10/13/2005WO2005095763A1 Seal for sealing a gap between two adjacent components
10/13/2005US20050226717 Flow control arrangement
10/13/2005DE102004014118A1 Anordnung zur Abdichtung eines Übergangs zwischen Kühlpassagen zweier Komponenten einer Turbomaschine Arrangement for sealing a transition between cooling passages of two components of a turbomachine
10/13/2005DE102004014117A1 Komponente einer Turbomaschine mit einer Kühlanordnung Component of a turbo engine with a cooling arrangement
10/12/2005EP1583850A1 Thermal spray composition and method of deposition for abradable seals
10/12/2005CN1682012A Gas turbine pressurizing air supply system
10/11/2005CA2367570C Split ring for gas turbine casing
10/06/2005US20050220622 Integral covered nozzle with attached overcover
10/06/2005US20050220612 Inner shroud for the stator blades of the compressor of a gas turbine
10/06/2005US20050220611 Hybrid seal and system and method incorporating the same
10/06/2005US20050220610 Sealing device and method for turbomachinery
10/06/2005US20050217272 Deoiler for a lubrication system
10/06/2005DE102004016222A1 Anordnung zur selbsttätigen Laufspalteinstellung bei einer zwei- oder mehrstufigen Turbine Arrangement for automatically running gap setting for a two- or multi-stage turbine
10/05/2005EP1582703A2 Deoiler for a lubrication system
10/05/2005EP1582700A2 Seal assembly for a turbomachine
10/05/2005EP1582699A2 Hybrid seal for a gas turbine
10/05/2005EP1582698A1 Integral covered nozzle with attached overcover
10/05/2005EP1581723A1 Grommeted bypass duct penetration
10/05/2005CN1678816A Recirculation structure for a turbocompressor
10/05/2005CN1676976A Hybrid seal assembly and system and method incorporating the same
10/05/2005CN1676885A Integral covered guider with attached overcover
09/2005
09/29/2005WO2005090755A1 Gas turbine with a compressor housing which is protected against cooling down and method for operating a gas turbine
09/29/2005US20050214112 Seal arrangement
09/29/2005US20050212299 Air cooling generator
09/29/2005DE102005009402A1 Dichtungsanordnung in Turbomaschinen Seal assembly in turbomachinery
09/29/2005DE102004011818A1 Housing for an exhaust gas turbocharger turbine wheel comprises a thermally sprayed layer on the inner housing surface
09/28/2005EP1580414A2 Turbomachine component with cooling arrangement
09/28/2005EP1580404A2 Arrangement for self adjusting the tip clearance in a two or multiple stage turbine
09/28/2005EP1580403A1 Annular sheet metal seal for sealing the space between an inner and an outer turbomachine casing
09/28/2005EP1580402A1 Turbomachine with two sub - parts being under axial pressure
09/28/2005EP1580401A2 Sealing for transition between cooling passages of two turbomachine components
09/28/2005EP1185766B1 Concentricity ring
09/28/2005CN1673491A Soldering structure and soldering method for machinable seal structual parts
09/26/2005CA2500965A1 Gasket between inner and outer casings of one section of turbojet engine
09/22/2005US20050206088 Bearing seal with backup device
09/22/2005US20050206087 Sealing arrangement using brush seals
09/22/2005US20050204746 Device for passive control of the thermal expansion of the extension casing of a turbo-jet engine
09/21/2005EP1577506A1 Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine
09/21/2005EP1577504A1 Bearing seal with backup device
09/21/2005EP1577502A1 Spraybar configuration to control the tip clearance in a gas turbine
09/21/2005EP1577501A1 High pressure turbine stator of a turbo-engine and his assembling process
09/21/2005EP1576258A1 Shroud cooling assembly for a gas turbine
09/21/2005CN1670349A Gas turbine engine component having bypass circuit
09/20/2005CA2228777C Gasket with stacked leaves sliding in receiving slots
09/15/2005WO2005085600A1 Ring structure with a metal design having a run-in lining
09/15/2005US20050201860 Cellular materials
09/15/2005US20050201859 Gas turbine ventilation circuitry
09/15/2005US20050200080 Seal for a turbine engine
09/15/2005DE102004010236A1 Metal ring structure for sealing gap between rotor blade tips and stator in e.g. gas turbine, has inner wall formed by metal fabric or felt
09/14/2005EP1574671A2 Dynamic seal for a turbine engine
1 ... 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 ... 106