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