| Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148) |
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| 04/28/2005 | US20050089396 Cooling arrangement |
| 04/28/2005 | US20050089392 Rotor and bearing system for a turbomachine |
| 04/28/2005 | US20050087319 Refractory metal core wall thickness control |
| 04/28/2005 | US20050086943 Turbine compartment ventilation control system and method using variable speed fan |
| 04/28/2005 | US20050086942 Approach to extending life of gas turbine engine |
| 04/28/2005 | US20050086788 Valve tooling system and method of employing same |
| 04/27/2005 | CN1609411A Method and apparatus for controlling steam turbine inlet flow to limit shell and rotor thermal stress |
| 04/27/2005 | CN1608771A Refractory metal core wall thickness control |
| 04/27/2005 | CN1199003C Device for cooling or heating circular housing |
| 04/26/2005 | US6884036 Complementary cooled turbine nozzle |
| 04/26/2005 | US6884024 Arrangement for the fastening of struts serving as bearing carriers for the rotor of an aeronautical gas turbine to the casing structure of the aeronautical gas turbine |
| 04/26/2005 | US6883807 Multidirectional turbine shim seal |
| 04/26/2005 | US6883527 Inserting cleaning head into a compressor through an inlet at a predetermined circumferential location; manipulating cleaning head in pitch and yaw directions while inserting the cleaning head to locate the cleaning head; actuating cleaning |
| 04/26/2005 | US6883303 Aircraft engine with inter-turbine engine frame |
| 04/26/2005 | US6883224 Gas turbine impeller alignment tool and method |
| 04/26/2005 | CA2372623C Axial flow turbine having stepped portion formed in axial-flow turbine passage |
| 04/26/2005 | CA2113376C Device for securing rotor blades axially and for eliminating rotor imbalances in axial-flow compressors or turbines |
| 04/21/2005 | WO2005035946A1 Rotor balancing device and method |
| 04/21/2005 | US20050085949 Method and apparatus for controlling steam turbine inlet flow to limit shell and rotor thermal stress |
| 04/21/2005 | US20050084396 Grooved shaft member and associated turbocharger and method |
| 04/21/2005 | US20050084371 Base material with cooling air hole |
| 04/21/2005 | US20050081525 Cooling of liquid fuel components to eliminate coking |
| 04/21/2005 | US20050081507 Fluid system |
| 04/21/2005 | DE10232738B4 Anordnung zumindest zweier Abgasturbolader Arrangement of at least two exhaust gas turbochargers |
| 04/21/2005 | DE102004012929B3 Noise reduction system for gas turbine engine for aircraft has surface cladding for hot gas channel downstream of turbine, with circular perforated plates covering large ends of frustoconical spaces |
| 04/20/2005 | EP1524817A1 Method and apparatus for selective data control |
| 04/20/2005 | EP1523609A1 Improved low cycle fatigue life (lcf) impeller design concept |
| 04/20/2005 | CN1607766A Method and apparatus for selective data control |
| 04/19/2005 | US6881035 Draft inducer having single piece metal impeller and improved housing |
| 04/19/2005 | US6881032 Exit stator mounting |
| 04/19/2005 | US6881029 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing |
| 04/19/2005 | US6881027 Gearless/oilless gas turbine engine |
| 04/19/2005 | US6881024 System for decoupling a fan from a turbojet by means of an explosive charge |
| 04/19/2005 | US6880338 Lead-in structure and a fixing flange for a turbo generator |
| 04/16/2005 | CA2485152A1 Refractory metal core wall thickness control |
| 04/14/2005 | WO2005033600A1 Device and method for cryogenically separating a gas mixture |
| 04/14/2005 | US20050079050 Gas turbine engine and method of producing the same |
| 04/14/2005 | US20050079047 Rotation-locking of sectors of rectifier blades by bars in the parting planes of the housing |
| 04/14/2005 | US20050076642 Seal element for sealing a gap and combustion turbine having a seal element |
| 04/14/2005 | US20050076523 Methods and apparatus for securing components for inspection |
| 04/14/2005 | DE19813779B4 Anordnung zur Kühlung der Plattformen von Leitschaufeln einer Gasturbine Arrangement for cooling the platforms of stator blades of a gas turbine |
| 04/14/2005 | DE102004045058A1 Verfahren zum Messen von auf ein Turbinengehäuse einwirkenden Rohrleitungskräften A method of measuring force acting on a turbine casing piping forces |
| 04/13/2005 | EP1522772A1 Turbine containing two components connected by a sealing |
| 04/13/2005 | EP1522695A1 Combustor cooling for gas turbine engines |
| 04/13/2005 | EP1522062A1 Device and method for active soundproofing, and power unit for aeroplanes |
| 04/13/2005 | EP1019116B1 A rotary pump with hydrodynamically suspended impeller |
| 04/13/2005 | EP0891218B1 An engine arrangement with a soot filter |
| 04/13/2005 | CN1605718A 蒸汽涡轮机 Steam turbine |
| 04/13/2005 | CN1605717A Super-supercritical air cooling steam turbine |
| 04/13/2005 | CN1605716A Supercritical air cooling steam turbine |
| 04/12/2005 | US6878041 Method for removing a metallic layer of a layer-system |
| 04/12/2005 | US6877950 Method and device for minimizing oil consumption in a gas turbine engine |
| 04/12/2005 | US6877901 Bearing system for high-speed rotating machinery |
| 04/12/2005 | US6877321 Method and system for reducing turbine exhaust turbulence |
| 04/07/2005 | US20050074325 Cooling jets |
| 04/07/2005 | US20050074049 Shaft-misalignment-measuring device, a shaft-misalignment-measuring method, a single-shaft combined plant using the shaft-misalignment-measuring device and a start-up method of the single-shaft combined plant |
| 04/07/2005 | US20050072162 Ejector for cooling air supply pressure optimization |
| 04/07/2005 | US20050072157 Steam turbine |
| 04/07/2005 | DE10342208A1 Heat shield for gas turbine has end faces of heat shields which are adjacent in circumferential direction each having surface extending at angle to radial direction of gas turbine and extend at least partially parallel to one another |
| 04/07/2005 | CA2527504A1 Slide in hook and fold out ceiling fan blades |
| 04/06/2005 | EP1520961A2 Methods for controlling lubrication oil draining in gas turbine engines |
| 04/06/2005 | EP1520960A2 Cooling air supply |
| 04/06/2005 | EP1520957A1 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
| 04/06/2005 | EP1520062A1 Highly oxidation resistant component |
| 04/06/2005 | EP1200744B1 Device and method for controlling a cooling air flow of a gas turbine and gas turbine with a cooling air flow |
| 04/06/2005 | CN1603578A Jp2005106738 |
| 04/05/2005 | US6875464 Using ceramic paste containing zirconia particles in binder; heating |
| 04/05/2005 | US6875292 Oxidation, corrosion resistant protective coatings; surface treatment; controlling temperature |
| 04/05/2005 | US6874998 Turbocharger in which at least part of wall of internal space through which lubricant flows is coated with oil repelling and/or heat insulating coating, thus promoting oil drainage from turbocharger lubricant drain gallery |
| 04/05/2005 | US6874324 Gas turbine and gas turbine power generator |
| 04/05/2005 | CA2352029C Turbocharger thermal isolation connection |
| 04/05/2005 | CA2330470C High temperature bolting system |
| 03/31/2005 | WO2005028876A1 Compressor cleaning system |
| 03/31/2005 | WO2005028815A2 Device for the generation of mechanical or electrical energy using any thermal potential |
| 03/31/2005 | WO2005028119A1 Nozzle and method for washing gas turbine compressors |
| 03/31/2005 | US20050069439 Device for detection of an unbalanced oil mass in a rotor, rotor fitted with such a device, and machine equipped with such a rotor |
| 03/31/2005 | US20050069427 Housing for a fluid flow engine |
| 03/31/2005 | US20050069411 Turbine comprising at least four stages and use of a turbine blade with a reduced mass |
| 03/31/2005 | US20050066647 Exhaust diffuser assembly with tunable velocity profile |
| 03/31/2005 | DE19546722B4 Leitschaufelträger für eine Gasturbine Guide vane for a gas turbine |
| 03/30/2005 | EP1519179A1 Device for oil unbalance detection in a rotor, rotor with such a device, and apparatus comprising such a rotor |
| 03/30/2005 | EP1519009A1 Turbomachine with cabin bleed air through a tube with ball joint |
| 03/30/2005 | EP1519007A1 Gas turbine |
| 03/30/2005 | CN1601067A Turbomachine with cabin bleed air through a tube with bi-ball joint |
| 03/29/2005 | US6872047 Steam-cooling-type turbine |
| 03/29/2005 | US6872046 Enclosure for oil lubricated, rotating elements |
| 03/29/2005 | US6872003 Oil-damped rolling bearing |
| 03/29/2005 | US6871504 Turbine power plant, installation process and removal process of the turbine power plant |
| 03/29/2005 | CA2330751C Gas turbine |
| 03/25/2005 | CA2482144A1 Device for detection of an unbalanced oil mass in a rotor, rotor fitted with such a device, and machine equipped with such a rotor |
| 03/24/2005 | US20050064229 Rhenium-containing protective layer for protecting a component against corrosion and oxidation at high temperatures |
| 03/24/2005 | US20050063821 Low pressure steam turbine exhaust hood |
| 03/24/2005 | US20050061005 Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 03/23/2005 | EP1517008A2 Cooling of a coated wall by a network of cooling channels |
| 03/23/2005 | EP1517006A1 Gas turbine brush seal arrangement for cabin air supply |
| 03/23/2005 | EP1517005A1 Gas turbine sealing joint having lamellar structure |
| 03/23/2005 | EP1516690A1 Method of manufacturing or repairing a bladed rotor disc |
| 03/23/2005 | EP1466079B1 Turbine comprising at least four stages and use of a turbine blade with a reduced mass |
| 03/23/2005 | CN1598477A Method for measuring piping forces acting on a turbine casing |
| 03/23/2005 | CN1598272A Gas turbine brush seal arrangement for cabin air supply |