Patents for F01D 9 - Stators (10,038) |
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02/01/2006 | CN1239810C High effective blade structure of turbine |
01/31/2006 | US6991427 Casing section |
01/25/2006 | EP1619353A1 Wall cooling circuit |
01/25/2006 | EP1618290A1 Turbine nozzle segment |
01/25/2006 | EP1556596A4 Effusion cooled transition duct with shaped cooling holes |
01/25/2006 | CN1724848A Fluid pressure actuating turbine device with deflector |
01/24/2006 | US6989174 vapor phase aluminizing of aircraft blades or turbines; protective coatings having oxidation and corrosion resistance |
01/24/2006 | US6988870 Casing for a centrifugal pump |
01/19/2006 | WO2006007057A1 Multi-zone tubing assembly and installing method for a transition piece of a gas turbine |
01/19/2006 | WO2006005199A1 Exhaust-gas turbine for a turbocharger comprising an air-cooled turbine disc |
01/19/2006 | US20060013682 Turbocharger with compressor stage flow conditioner |
01/19/2006 | US20060010879 Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine |
01/19/2006 | DE102004031986A1 Exhaust-gas turbocharger for internal combustion engine, has three studs arranged at fixed-blade carrier in circumferential direction and pass through notches formed in bearing housing to form bayonet lock for connecting carrier at housing |
01/19/2006 | DE102004030798A1 Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie Exhaust gas turbocharger for an internal combustion engine with variable turbine geometry |
01/18/2006 | EP1617043A1 Method for cooling a wall within a gas turbine engine |
01/18/2006 | EP1617041A1 Turbocharger with air cooled turbine disc |
01/18/2006 | CN1721660A Turbine airfoil trailing edge repair and methods therefor |
01/18/2006 | CN1721659A Hot gas path component with a meshed and dimpled cooling structure |
01/18/2006 | CN1721570A Method for aluminide coating a hollow article |
01/12/2006 | US20060008347 Guide blade fixture in a flow channel of an aircraft gas turbine |
01/12/2006 | US20060005546 Modulated flow turbine nozzle |
01/12/2006 | DE10357075B4 Verfahren zur Lärmreduzierung von Turbomaschinen Procedures for noise reduction of turbomachinery |
01/12/2006 | DE102005001864B3 Turbine housing for exhaust gas supercharger has spacing elements with recesses enabling direct application of exhaust gas flow to holding elements |
01/11/2006 | EP1614859A1 Film cooled turbine blade |
01/10/2006 | US6984102 Hot gas path component with mesh and turbulated cooling |
01/10/2006 | US6984101 Turbine vane plate assembly |
01/10/2006 | US6983608 Methods and apparatus for assembling gas turbine engines |
01/05/2006 | WO2006001825A2 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
01/05/2006 | US20060000077 A method of manufacturing a stator component |
01/05/2006 | DE102004029696A1 Plattformkühlanordnung für den Leitschaufelkranz einer Gasturbine Platform cooling arrangement for a gas turbine vane ring |
01/05/2006 | DE102004028133A1 Turbo-machine e.g. turbocharger, has flexible fixation provided with fitting bolt that comprises waisted shank and fitting pin, where pin is guided in flange part and/or hole of insert piece and spiral casing for receiving force |
01/05/2006 | CA2551016A1 Gas turbine cooled shroud assembly with hot gas ingestion suppression |
01/04/2006 | EP1612374A1 Turbine guide vane with improved cooling properties |
01/04/2006 | CN1717534A Turbine cooling vane of gas turbine engine |
01/04/2006 | CN1715618A Improved cooling stationary turbine blade |
01/03/2006 | US6981841 Triple circuit turbine cooling |
01/03/2006 | CA2401945C Joint structure of coolant passage, tube seal and gas turbine |
12/29/2005 | US20050287002 Turbine vane collar seal |
12/29/2005 | US20050286997 Airfoil insert with castellated end |
12/29/2005 | DE102004027594A1 Strömungsmaschine mit radial durchströmtem Verdichterrad Flow machine with radial compressor perfused |
12/28/2005 | EP1609952A1 Turbine vane collar seal |
12/28/2005 | EP1609950A2 Airfoil insert with castellated end |
12/28/2005 | EP1608846A1 A method of manufacturing a stator component |
12/28/2005 | CN1712674A Turbine vane collar seal |
12/27/2005 | US6978615 High efficiency turbocharger having secondary wastegate volute |
12/22/2005 | US20050281694 Inner air seal anti-rotation device |
12/22/2005 | US20050281674 Internal cooling system for a turbine blade |
12/22/2005 | US20050279099 Multi-zone tubing assembly for a transition piece of a gas turbine |
12/22/2005 | DE102005024475A1 Verfahren zur Beschichtung von Gasturbinentriebwerkskomponenten A process for coating of gas turbine engine components |
12/21/2005 | EP1607682A1 Gas tight joint between a gas turbine combustor and a turbine inlet guide conduit |
12/21/2005 | EP1607582A1 Mounting of a gas turbine combustor with integrated turbine inlet guide conduit |
12/21/2005 | EP1607581A1 Method and apparatus for fabricating a turbine nozzle assembly |
12/21/2005 | EP1607580A2 Platform cooling of vanes in a gas turbine |
12/21/2005 | EP1607575A1 Method for cooling an airfoil wall |
12/21/2005 | EP1309773B1 Turbine vane system |
12/15/2005 | WO2005119028A1 Gas turbine compression system and compressor structure |
12/15/2005 | US20050276692 Lightened interblade platform for a turbojet blade support disc |
12/15/2005 | DE102005024160A1 Innenkernprofil für ein Leitschaufelblatt einer Turbine Inner core profile for a turbine airfoil |
12/14/2005 | CN1707123A Turbo-machine with radial through-flow compressor rotor |
12/08/2005 | WO2005116405A1 A support structure in a turbine or compressor device and a method for assembling the structure |
12/08/2005 | US20050271505 Turbine engine shroud segment, hanger and assembly |
12/08/2005 | US20050268462 Methods and apparatus for fabricating a turbine nozzle assembly |
12/08/2005 | DE102004023214A1 Turbocharger for a combustion engine comprises a housing which contains a turbine wheel, a bearing housing, a flow channel section, and a scoop and carrier |
12/08/2005 | CA2502805A1 Turbine engine shroud segment, hanger and assembly |
12/07/2005 | EP1602804A2 Turbine nozzle support structure |
12/07/2005 | EP1602800A1 Method for cooling an airfoil wall |
12/07/2005 | EP1601861A1 Sheet metal turbine or compressor static shroud |
12/07/2005 | EP1601860A1 Turbine nozzle airfoil |
12/07/2005 | CN1704560A Methods and apparatus for fabricating a turbine nozzle assembly |
12/06/2005 | US6971847 Fastening system |
12/06/2005 | US6971845 Vane with modified base |
12/02/2005 | CA2508391A1 Methods and apparatus for fabricating a turbine nozzle assembly |
12/01/2005 | US20050265831 Method for coating gas turbine engine components |
12/01/2005 | US20050265830 Turbine nozzle support structure |
12/01/2005 | US20050265829 Internal core profile for a turbine nozzle airfoil |
12/01/2005 | US20050263199 Flow laminarizing device |
12/01/2005 | US20050262845 Combustion liner having improved cooling and sealing |
12/01/2005 | US20050262844 Combustion liner seal with heat transfer augmentation |
12/01/2005 | US20050262690 Gas turbine engine transition liner assembly and repair |
12/01/2005 | DE102004023279A1 Exhaust gas turbocharger for internal combustion engine, has turbine casings with two wall sections, in which one section is designed and arranged such that low-pass area is extended over entire length of section of flow channel unit |
11/30/2005 | CN1702302A Internal core profile for a turbine nozzle airfoil |
11/29/2005 | US6969239 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
11/29/2005 | US6969233 Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity |
11/29/2005 | US6969232 Flow directing device |
11/29/2005 | US6969230 Venturi outlet turbine airfoil |
11/29/2005 | US6968702 Nozzle bolting arrangement for a turbine |
11/29/2005 | CA2123135C Aluminide - silicide coatings, coating compositions, process for coating and improved coated products |
11/25/2005 | CA2507192A1 Method for coating gas turbine engine components |
11/24/2005 | WO2005111380A1 Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction |
11/24/2005 | US20050260346 Method for aluminide coating a hollow article |
11/24/2005 | DE102005020470A1 Cooling insert and nozzle assembly for use by gas turbine, has cooling insert having flexible edge portion which is inserted between adjacent ribs of nozzle |
11/23/2005 | EP1295014B1 Transition piece for non-annular gas turbine combustion chambers |
11/22/2005 | US6966750 Gas turbine stationary blade |
11/17/2005 | WO2005108748A2 Apparatus for bearing lubrication in turbine engines |
11/17/2005 | WO2005108747A1 Turbocharger with reduced thermal inertia and method of producing the same |
11/17/2005 | US20050254955 Friction stir welded hollow airfoils and method therefor |
11/17/2005 | US20050254944 Fastened vane assembly |
11/17/2005 | US20050254942 Method of joining ceramic parts and articles so formed |
11/17/2005 | US20050254939 Arrangement for the automatic running gap control on a two or multi-stage turbine |
11/17/2005 | DE102004018987A1 Protective device against bursting turbochargers comprises an endless looped belt of textile fiber material which has a high penetration resistance, and covers at least a part of the turbocharger circumference |