| Patents for F01D 11 - Preventing or minimising internal leakage of working fluid, e.g. between stages (10,581) |
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| 04/03/2002 | CN1082131C Device for monitoring turbomachine radial gaps |
| 04/02/2002 | US6365236 Alternating the temperature during electron beam vapor deposition, layers are applied at different temperature conditions for different porosities |
| 03/28/2002 | WO2002025066A1 Steam-type gas turbine subassembly and method for enhancing turbine performance |
| 03/28/2002 | WO2002025065A1 Seal system |
| 03/26/2002 | US6361274 Fastening devices for heat-protection shields |
| 03/26/2002 | US6361273 Heat shield for a gas turbine |
| 03/21/2002 | US20020033578 Brush seals |
| 03/19/2002 | US6358002 Article having durable ceramic coating with localized abradable portion |
| 03/19/2002 | US6357752 Brush seal |
| 03/14/2002 | WO2002021027A1 Heat-resistance magnetic silicone rubber body for brush seals in turbomachinery and methods of application |
| 03/14/2002 | US20020031427 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor |
| 03/14/2002 | DE10140419A1 Flüssigkristallines Medium mit niedriger Doppelbrechung Liquid-crystalline medium having low birefringence |
| 03/14/2002 | DE10043906A1 Vordralldüsenträger Vordralldüsenträger |
| 03/13/2002 | EP1186812A2 Brush seal segment end bristle protection and flexibility maintenance device and methods of forming the segment |
| 03/13/2002 | EP1186746A2 Swirl nozzle |
| 03/13/2002 | EP1185766A1 Concentricity ring |
| 03/13/2002 | CN1080815C Brush seal |
| 03/12/2002 | US6354803 Blade damper and method for making same |
| 03/07/2002 | WO2002003024A8 Play measuring sensor by multiple depth abrasion |
| 03/07/2002 | US20020028136 Pre-swirl nozzle carrier |
| 03/07/2002 | DE10122464C1 Mantle ring for low pressure turbine stage of gas turbine uses segments each having seal carrier and relatively spaced security element with minimum contact between them |
| 03/06/2002 | EP1183444A1 Turbomachine and sealing element for a rotor thereof |
| 03/06/2002 | EP1183442A1 Cast on-board injection nozzle with adjustable flow area |
| 03/05/2002 | US6352264 Abradable seal having improved properties |
| 03/05/2002 | CA2264282C Gas turbine air separator |
| 02/28/2002 | WO2002016740A1 Labyrinth helical seal |
| 02/27/2002 | EP1036255B1 Seal assembly for a gas turbine engine |
| 02/26/2002 | US6350102 Shroud leakage flow discouragers |
| 02/21/2002 | WO2001031235A3 Oil sump buffer seal |
| 02/21/2002 | US20020021962 Centrifugal compressor and centrifugal turbine |
| 02/21/2002 | DE10038452A1 Abdichtung einer thermischen Turbomaschine Sealing a thermal turbomachinery |
| 02/20/2002 | EP1180623A2 Brush seal |
| 02/20/2002 | EP1180580A1 Device for mounting an annular flask at a radial side of a bladed rotor |
| 02/20/2002 | EP1180577A2 Cooling method for a turbine rotor |
| 02/20/2002 | EP1180197A1 Sealing system for a rotor of a turbo engine |
| 02/20/2002 | EP1180196A1 Turbo-machine comprising a sealing system for a rotor |
| 02/19/2002 | US6347508 Combustor liner support and seal assembly |
| 02/14/2002 | US20020018719 Rotor blade retaining apparatus |
| 02/13/2002 | EP1179654A2 Honeycomb seal for a thermal turbomachine |
| 02/12/2002 | US6345494 Side seal for combustor transitions |
| 02/12/2002 | CA2246856C Seal device between fastening bolt and bolthole in gas turbine disc |
| 02/12/2002 | CA2229883C Gas turbine shroud and platform seal system |
| 02/12/2002 | CA2077842C Gas turbine engine case counterflow thermal control |
| 02/07/2002 | WO2001055273A3 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 02/07/2002 | US20020015641 Sealing of a thermal turbomachine |
| 02/07/2002 | DE10044848A1 Dichtung zwischen statischen Turbinenteilen Seal between static turbine components |
| 02/06/2002 | EP1178182A1 Gas turbine split ring |
| 02/06/2002 | EP1177367A1 Seal for sealing a gap, in particular in a turbine, and a turbine |
| 02/05/2002 | US6343912 Gas turbine or jet engine stator vane frame |
| 02/05/2002 | US6343792 Shaft seal and turbine using the same |
| 02/05/2002 | CA2259383C High differential pressure end rotor seal |
| 01/30/2002 | EP1176343A2 Sealing between static turbine components |
| 01/29/2002 | US6341938 Methods and apparatus for minimizing thermal gradients within turbine shrouds |
| 01/24/2002 | US20020009361 Shaft bearing for a turbomachine, turbomachine, and method of operating a turbomachine |
| 01/22/2002 | US6340286 Rotary machine having a seal assembly |
| 01/22/2002 | US6340285 End rail cooling for combined high and low pressure turbine shroud |
| 01/22/2002 | CA2047275C Fully floating inlet flow guide for double-flow low pressure steam turbines |
| 01/17/2002 | WO2001051771A3 Array for regulating the diameter of a stator of a gas turbine |
| 01/17/2002 | US20020006330 Labyrinth seal for rotating shaft |
| 01/17/2002 | US20020005038 Method and apparatus for the cooling of jet-engine turbine casings |
| 01/17/2002 | DE10032454A1 Vorrichtung zum Kühlen eines ungleichmäßig stark temperaturbelasteten Bauteiles Apparatus for cooling an uneven strongly temperature-loaded component |
| 01/16/2002 | EP1172524A2 Method for deploying shroud segments of different thickness in a turbine engine |
| 01/15/2002 | CA2065679C Shroud cooling assembly for gas turbine engine |
| 01/10/2002 | WO2002003024A1 Play measuring sensor by multiple depth abrasion |
| 01/10/2002 | WO2002002913A1 Drainage system for gas turbine supporting bearings |
| 01/10/2002 | WO2002002912A1 Draining and cooling system for gas turbine cushions |
| 01/10/2002 | US20020004006 Intermediate-stage seal arrangement |
| 01/10/2002 | US20020004003 Device for cooling a component subject to temperature stress of nonuniform intensity |
| 01/10/2002 | US20020004002 Turbo machines |
| 01/09/2002 | EP1170571A1 Sensor to measure play by multi-stage abrasion |
| 01/09/2002 | EP1170464A2 Cooling device for an element with an unequal thermal charge |
| 01/09/2002 | EP1169587A1 Positive biased packing ring brush seal combination |
| 01/09/2002 | EP1169586A1 Brush seals for steam turbine applications |
| 01/09/2002 | EP1169585A1 Self-centering brush seal |
| 01/09/2002 | EP0723625B1 Active tip flow bypass in stator vane channel |
| 01/08/2002 | US6336790 Axial flow power tool turbine machine |
| 01/08/2002 | CA2252274C Gas turbine spindle bolt seal device |
| 01/03/2002 | WO2002001046A1 Sealing system for gas turbine |
| 01/03/2002 | WO2002001036A1 Drilling turbine |
| 01/03/2002 | US20020001519 Control arrangement |
| 01/03/2002 | DE10030820A1 Labyrinthdichtung für eine rotierende Welle Labyrinth seal for a rotating shaft |
| 01/02/2002 | EP1167696A2 Labyrinth seal for a rotating shaft |
| 01/02/2002 | EP1167695A1 Gas turbine and gas turbine guide vane |
| 01/02/2002 | EP1167691A2 Blade damper and method for making same |
| 01/02/2002 | EP1167188A1 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lrps), hybrid multifunction booster rocket with cruising lrps and development test therefor |
| 01/02/2002 | EP1165941A1 High temperature erosion resistant, abradable thermal barrier composite coating |
| 01/01/2002 | US6334756 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor |
| 01/01/2002 | US6334617 Suited for use in the compressor sections of gas turbine engines |
| 01/01/2002 | CA2251192C Gas turbine stationary blade double cross type seal device |
| 12/27/2001 | US20010055652 Method of making abradable seal having improved properties |
| 12/25/2001 | US6332617 Leaktight seal of a circular vane stage |
| 12/20/2001 | WO2001048887A3 Brush seal |
| 12/20/2001 | US20010052375 Abradable coatings for turbine engine shrouds formed from biscuits of silicon-diffused powdered alloys processed with a fluoropolymer binder which forms hydrogen fluoride(HF), the HF strips oxides from the coating during processing |
| 12/20/2001 | DE10019437A1 Verfahren und Vorrichtung zum Kühlen der Gehäuse von Turbinen von Strahltriebwerken Method and apparatus for cooling the housing of turbines of jet engines |
| 12/19/2001 | EP1164320A2 Multi-clearance labyrinth seal design and related process |
| 12/19/2001 | EP1164253A1 Cooling system for the shroud of paired rotor blades |
| 12/19/2001 | EP1164250A2 Floating connector for an impingement insert |
| 12/19/2001 | EP1163463A1 Shaft seal |
| 12/19/2001 | EP1163430A1 Covering element and arrangement with a covering element and a support structure |
| 12/19/2001 | EP1163429A1 Sealing device for segmented stator ring |