| Patents for F01D 9 - Stators (10,038) |
|---|
| 05/06/2004 | WO2004038182A1 Sheet metal turbine or compressor static shroud |
| 05/06/2004 | WO2004038181A1 Aerodynamic method to reduce noise level in gas turbines |
| 05/06/2004 | WO2004038180A1 Apparatus and method for reducing the heat load of an airfoil |
| 05/06/2004 | US20040086635 Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
| 05/06/2004 | US20040086383 Turbine nozzle retention apparatus at the carrier horizontal joint face |
| 05/06/2004 | US20040086382 Gas turbine engine axial stator compressor |
| 05/06/2004 | US20040084423 Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
| 05/06/2004 | EP1416123A2 Vortex inlet vanes |
| 05/06/2004 | EP1416063A1 Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding |
| 05/04/2004 | US6729842 Methods and apparatus to reduce seal rubbing within gas turbine engines |
| 05/04/2004 | US6729134 Variable geometry turbocharger having internal bypass exhaust gas flow |
| 04/30/2004 | CA2446343A1 Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
| 04/29/2004 | US20040081548 Flow directing device |
| 04/29/2004 | US20040079084 Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine |
| 04/28/2004 | EP1413771A1 Casing, compressor, turbine and gas turbine engine having such casing |
| 04/28/2004 | EP1413713A2 Self-aspirating high-area-ratio interstage turbine duct assembly for use in a gas turbine engine |
| 04/28/2004 | EP1412618A1 Seal element for sealing a gap and combustion turbine having a seal element |
| 04/28/2004 | EP1212167B1 Method for replacing a turbine vane airfoil |
| 04/28/2004 | CN1492128A Method and device for support high temperature pipeline |
| 04/28/2004 | CN1492065A Nickel base alloy |
| 04/27/2004 | US6726442 Disc turbine inlet to assist self-starting |
| 04/23/2004 | CA2446035A1 Flow directing device |
| 04/22/2004 | WO2004033871A2 Leak resistant vane cluster |
| 04/22/2004 | WO2004033858A1 Turbocharger |
| 04/22/2004 | US20040076520 Turbine and stationary blade for a turbine |
| 04/22/2004 | US20040076511 Gas turbine |
| 04/22/2004 | DE10239534A1 Heißgas führendes Gassammelrohr Hot gas leading gas manifold |
| 04/21/2004 | EP1411209A2 Cooled stationary blades in a gas turbine |
| 04/21/2004 | EP1409926A1 Baffle cooling device |
| 04/21/2004 | EP1409848A1 Third-stage turbine nozzle airfoil |
| 04/21/2004 | EP1409846A1 Second-stage turbine nozzle airfoil |
| 04/21/2004 | CN1490497A 燃气轮机 Gas turbine |
| 04/20/2004 | US6722848 Turbine nozzle retention apparatus at the carrier horizontal joint face |
| 04/20/2004 | US6722119 Turbojet power plant with heat exchanger |
| 04/15/2004 | US20040071550 Turbine efficiency tailoring |
| 04/15/2004 | DE10344843A1 Integrierte Rotier-Messerkanten-Injektionsanordnung Integrated Rotier knife edge injection assembly |
| 04/14/2004 | EP1408199A1 Leak resistant vane cluster |
| 04/14/2004 | EP1408198A1 ASSEMBLY TYPE NOZZLE DIAPHRAGM, AND METHOD OF ASSEMBLING THE SAME |
| 04/14/2004 | EP1068428B1 Apparatus for cooling a gas turbine airfoil and method of making same |
| 04/14/2004 | EP0934456B1 Vane segment support and alignment device |
| 04/14/2004 | CN1488839A Cooling structure of stationary blade, and gas turbine |
| 04/13/2004 | US6719528 Stator vane arrangement for rotating machinery |
| 04/13/2004 | US6719524 Method of forming a thermally isolated gas turbine engine housing |
| 04/08/2004 | US20040067131 Leak resistant vane cluster |
| 04/07/2004 | CN1144935C Axial flow turbine |
| 04/06/2004 | US6715988 Turbine airfoil for gas turbine engine |
| 04/06/2004 | US6715983 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow |
| 04/06/2004 | US6715297 Methods and apparatus for supporting high temperature ducting |
| 04/01/2004 | WO2004027219A1 Variable geometry turbocharger having internal bypass exhaust gas flow |
| 04/01/2004 | US20040062652 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
| 04/01/2004 | US20040062637 Integral swirl knife edge injection assembly |
| 04/01/2004 | US20040060298 Dynamically uncoupled can combustor |
| 04/01/2004 | DE10258466B4 Turbolader Turbocharger |
| 03/31/2004 | EP1403582A2 Dynamically uncoupled can combustor |
| 03/31/2004 | CN1485529A Fastening system |
| 03/31/2004 | CN1143946C Housing for blade mechanism |
| 03/30/2004 | US6712588 Turbomachine with a vaneless rotating diffuser and nozzle |
| 03/25/2004 | US20040057825 Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine |
| 03/25/2004 | US20040055311 Methods and apparatus for supporting high temperature ducting |
| 03/25/2004 | DE10336994A1 Brennkraftmaschine mit Aufladung sowie zugeordneter Luftverdichter Internal combustion engine with supercharging and associated air compressor |
| 03/24/2004 | EP1400755A1 Flanged hollow structure |
| 03/24/2004 | EP1400681A2 Methods and apparatus for supporting high temperature ducting |
| 03/24/2004 | EP1400659A1 Methods and apparatus for sealing gas turbine engine variable vane assemblies |
| 03/24/2004 | EP1399647A1 Segmented turbine vane support structure |
| 03/24/2004 | CN1143056C Discharge header for guiding hot gas in gas turbine |
| 03/23/2004 | US6709235 Turbine housing for high exhaust temperature |
| 03/23/2004 | US6709233 Aerofoil for an axial flow turbomachine |
| 03/18/2004 | US20040052638 Cover for lp first stage diaphragm and method for improving inflow to first stage diaphragm |
| 03/18/2004 | US20040052636 Methods and apparatus for sealing gas turbine engine variable vane assemblies |
| 03/17/2004 | EP1398465A1 Turbocharger with rotor casing |
| 03/17/2004 | EP1398462A1 Gas turbine and transition piece |
| 03/16/2004 | US6705834 Axial flow turbine type rotor machine for elastic fluid operation |
| 03/16/2004 | US6705831 Linked, manufacturable, non-plugging microcircuits |
| 03/16/2004 | US6705829 Cover for LP first stage diaphragm and method for improving inflow to first stage diaphragm |
| 03/16/2004 | US6705011 Turbine element manufacture |
| 03/11/2004 | US20040047726 Ceramic matrix composite component for a gas turbine engine |
| 03/11/2004 | US20040047725 Ring segment of gas turbine |
| 03/09/2004 | US6702550 Turbine shroud segment and shroud assembly |
| 03/09/2004 | US6702547 Gas turbine |
| 03/09/2004 | US6701717 Cycle gas turbine engine |
| 03/04/2004 | US20040042898 Methods and apparatus to reduce seal rubbing within gas turbine engines |
| 03/03/2004 | EP1394366A1 Turbomachine housing |
| 03/03/2004 | EP1394361A1 Gas turbine |
| 03/03/2004 | EP1392956A2 Ceramic composite vane with metallic substructure |
| 03/02/2004 | US6699011 Linking arrangement of a turbine stator ring to a support strut |
| 03/02/2004 | US6699010 Nozzle adjustment mechanism for variable-capacity turbine |
| 02/26/2004 | WO2004016911A1 Method for manufacturing a stator or rotor component |
| 02/26/2004 | WO2004016910A1 Method for manufacturing a stator component |
| 02/26/2004 | US20040037699 Connecting system for a transition duct in a gas turbine |
| 02/26/2004 | US20040036230 Sealing structure for combustor liner |
| 02/26/2004 | US20040035116 Gas collection pipe carrying hot gas |
| 02/26/2004 | US20040034998 Vane and method of construction thereof |
| 02/25/2004 | EP1391583A1 Air cooled transition duct |
| 02/25/2004 | EP1391582A2 Sealing structure for combustor liner |
| 02/25/2004 | EP1391527A1 Nickel-base alloy |
| 02/25/2004 | CN1477298A Gas collecting pipe for transporting hot gas |
| 02/19/2004 | US20040033137 Machined fan exit guide vane attachment pockets for use in a gas turbine |
| 02/19/2004 | US20040033132 Simplified support device for nozzles of a gas turbine stage |
| 02/19/2004 | US20040031271 Convoluted seal with enhanced wear capability |
| 02/19/2004 | US20040031270 Coated seal article with multiple coatings |