| 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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| 01/28/2004 | CN1470746A Method and apparatus for turbine nozzle locking piece |
| 01/27/2004 | US6682321 Thermally decoupled flange for mounting to a turbine housing |
| 01/27/2004 | US6682304 Cooled gas turbine blade |
| 01/27/2004 | US6682300 Seal element for sealing a gap and combustion turbine having a seal element |
| 01/27/2004 | US6682297 Vane for a stator of a variable-geometry turbine, in particular for aeronautical engines |
| 01/27/2004 | US6682222 Bi-directional oil scoop for bearing lubrication |
| 01/27/2004 | US6682219 Anisotropic support damper for gas turbine bearing |
| 01/27/2004 | US6682022 Boundary layer control of aerodynamic airfoils |
| 01/27/2004 | US6681888 Silencing apparatus, notably for a turbo engine |
| 01/27/2004 | US6681579 Air turbine starter with fluid flow control |
| 01/22/2004 | WO2004007927A2 Method for influencing and controlling the oxide layer on metallic components of a hot co2/h2o circulating system |
| 01/22/2004 | WO2004007915A1 Rotor recentring after decoupling |
| 01/22/2004 | WO2004007913A1 Improved low cycle fatigue life (lcf) impeller design concept |
| 01/22/2004 | US20040013522 Endface gap sealing of steam turbine packing seal segments and retrofitting thereof |
| 01/22/2004 | US20040013519 Cradle mounted turbine nozzle |
| 01/22/2004 | US20040013516 System to feed cooling air into a gas turbine rotor |
| 01/22/2004 | US20040012149 Seal structure, turbine having the same, and leak-preventing seal system for rotating shaft |
| 01/22/2004 | US20040011056 Design and control strategy for catalytic combustion system with a wide operating range |
| 01/22/2004 | US20040011037 Configuration of at least two exhaust gas turbochargers |
| 01/22/2004 | US20040011012 Rotary machine |
| 01/22/2004 | DE10231879A1 Verfahren zur Beeinflussung und Kontrolle der Oxidschicht auf metallischen Bauteilen heisser CO2/H2O-Kreislaufsysteme A method for influencing and controlling the oxide layer on metallic components hot CO2 / H2O-loop systems |
| 01/21/2004 | EP1382816A2 Arrangement of at least two turbo compressors |
| 01/21/2004 | EP1382805A2 Frangible coupling |
| 01/21/2004 | EP1382801A2 Cradle mounted turbine nozzle |
| 01/21/2004 | EP1382798A2 Rotary machine |
| 01/20/2004 | US6679757 Shaping tool and method for shaping curved surfaces on workpieces |
| 01/20/2004 | US6679679 Internal stator shroud |
| 01/20/2004 | US6679047 Combined cycle gas turbine system |
| 01/20/2004 | US6679045 Flexibly coupled dual shell bearing housing |
| 01/15/2004 | WO2004005674A1 Scroll for the compressor of a turbosupercharger and process of manufacturing thereof |
| 01/15/2004 | WO2004005581A1 Highly oxidation resistant component |
| 01/15/2004 | WO2004005580A1 Highly oxidation resistant component |
| 01/15/2004 | US20040010387 Diagnosis method for detecting ageing symptoms in a steam turbine |
| 01/15/2004 | US20040009060 Low cycle fatigue life (LCF) impeller design concept |
| 01/15/2004 | US20040007878 Turbine power generator including supplemental parallel cooling and related methods |
| 01/15/2004 | US20040007422 Device for connecting two tubular pieces of an aircraft turbine engine |
| 01/15/2004 | US20040006967 Frangible coupling |
| 01/14/2004 | EP1381143A1 Turbine power generator including supplemental parallel cooling and related methods |
| 01/14/2004 | EP1380740A2 Fuel supply system for an electricity generating system |
| 01/14/2004 | EP1380727A1 Gas turbine power plant with a by-pass stack |
| 01/14/2004 | EP1380723A1 Cooling method and pre-swirler for gas turbine blades as well as a turbine comprising such a pre-swirler |
| 01/14/2004 | EP1380672A1 Highly oxidation resistant component |
| 01/14/2004 | CN1468351A Connecting device for housing-parts of turbochargers |
| 01/14/2004 | CN1467366A Failsafe film cooled wall |
| 01/14/2004 | CN1467365A Structural cover for gas turbine engine bolted flanges |
| 01/13/2004 | US6676374 Air-driven rotating and cutting device for use in medical and dental procedures |
| 01/13/2004 | US6676372 Gas turbine with axially mutually displaceable guide parts |
| 01/13/2004 | US6676370 Shaped part for forming a guide ring |
| 01/13/2004 | US6675586 Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines |
| 01/08/2004 | WO2004003425A1 Flange connection and method for mounting such a flange connection |
| 01/08/2004 | WO2004003346A1 Steam turbine |
| 01/08/2004 | US20040005238 For the production of single-crystal components or components with a directionally solidified microstructure such as for example blades or vanes for gas turbines; can also be used for conventionally cast components. |
| 01/08/2004 | US20040005231 Enclosure for oil lubricated, rotating elements |
| 01/08/2004 | US20040005217 Methods and apparatus for turbine nozzle locks |
| 01/08/2004 | US20040005216 Gas turbine shroud structure |
| 01/08/2004 | US20040003968 Bearing lubrication system for a turbomachine |
| 01/08/2004 | US20040003585 Cooled variable geometry exhaust nozzle |
| 01/08/2004 | US20040003583 Combined cycle gas turbine system |
| 01/07/2004 | EP1378706A1 Flange joint and method of assembling the same |
| 01/07/2004 | EP1378651A2 Cooled variable geometry exhaust nozzle |
| 01/07/2004 | EP1378634A2 Method of producing a bearing housing from a worn housing, and fixture implementing such a method |
| 01/07/2004 | EP1378633A2 Methods and apparatus for operating gas turbine engines |
| 01/07/2004 | EP1378632A2 Easy-fit heat screening device for connecting a cooling pipe and a through-hole formed in a nozzle support ring of a gas turbine |
| 01/07/2004 | EP1378631A2 Methods and apparatus for turbine nozzle locks |
| 01/07/2004 | EP1378630A1 Steam turbine |
| 01/07/2004 | EP1378587A1 High-temperature articles and method for making |
| 01/07/2004 | EP1377729A1 Turbine installation, especially steam turbine installation |
| 01/07/2004 | CN2597814Y In-line purifier for oil system of steam turbine |
| 01/07/2004 | CN2597669Y Disk pushing spindle device for repairing steam turbine |
| 01/06/2004 | US6672825 Method and apparatus for increasing power generated by a steam turbine by controlling the electric charge in steam exiting the steam turbine |
| 01/06/2004 | US6672630 Flange for connection between an axial compressor and high-pressure rotor disc unit in a gas turbine |
| 01/06/2004 | US6672072 Pressure boosted compressor cooling system |
| 01/06/2004 | US6671938 Pneumatic press vane lift installation tool |
| 01/05/2004 | CA2433132A1 Method of producing a bearing housing from a worn housing, and fixture implementing such a method |
| 01/02/2004 | EP1377140A2 Improved film cooling for microcircuits |
| 01/02/2004 | EP1375825A1 Failsafe film cooled wall |
| 01/02/2004 | EP1375824A2 Linked, non-plugging cooling microcircuits |
| 01/02/2004 | EP1375823A2 A method for repairing shroud tip overlap on turbine buckets |
| 01/02/2004 | EP1375348A2 Aircraft engine mount with single thrust link |
| 01/02/2004 | EP1375111A2 Segmented mould, particularly for the manufacturing of an air intake without connecting link |
| 01/02/2004 | EP1374253A1 A nuclear power plant and method of operating the same |
| 01/02/2004 | EP1373685A1 Gas turbine blade |
| 01/02/2004 | EP1373593A2 Method and device for gas phase diffusion coating of metal components |
| 01/01/2004 | US20040001965 High-temperature articles and method for making |
| 01/01/2004 | US20040001753 Air and steam cooled platform of a turbine blade or vane |
| 01/01/2004 | US20040000050 Method of repairing shroud tip overlap on turbine buckets |
| 12/31/2003 | WO2004001090A1 Ceramic particle-containing self-melting alloy thermal spraying material |
| 12/31/2003 | CN2596019Y Inlaid push-and-pull key type self-lubrication steam turbine bearing box |
| 12/30/2003 | USRE38373 Compliant foil fluid film thrust bearing with a tilting pad underspring |
| 12/30/2003 | US6670046 Metal substrate with composite ceramic-comprising coating embedded in recess capable of withstanding temperatures in excess of 1500 degrees F., second ceramic-comprising coating over edge of substrate adjacent periphery of first coating |
| 12/30/2003 | US6669393 Connector assembly for gas turbine engines |
| 12/30/2003 | US6669372 Turbocharger thrust bearing |
| 12/30/2003 | US6668540 Gas turbine exhaust passage and damper system for same |
| 12/30/2003 | CA2352027C Turbocharger with nozzle ring coupling |
| 12/30/2003 | CA2352022C Turbocharger support |
| 12/28/2003 | CA2432851A1 Aircraft engine mount with single thrust link |
| 12/27/2003 | CA2430175A1 Key moulding tools notably for the production of air inlet with no splices |
| 12/25/2003 | US20030235494 Linked, manufacturable, non-plugging microcircuits |
| 12/25/2003 | US20030233834 Arrangement for the cooling of the casing of an aircraft gas turbine engine |
| 12/23/2003 | US6666645 Arrangement for adjusting the diameter of a gas turbine stator |