| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 01/08/2004 | US20040003585 Cooled variable geometry exhaust nozzle |
| 01/08/2004 | US20040003583 Combined cycle gas turbine system |
| 01/08/2004 | DE10325599A1 Brennkammerdichtungsring und Brennkammer, die einen solchen Ring aufweist Combustion chamber sealing ring and the combustion chamber, having such a ring |
| 01/08/2004 | CA2490619A1 Gas turbine ventilation circuitry |
| 01/08/2004 | CA2490488A1 Orbiting combustion nozzle engine |
| 01/08/2004 | CA2487370A1 Power fluctuation suppressing method and power generation facility using same |
| 01/07/2004 | EP1378651A2 Cooled variable geometry exhaust nozzle |
| 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 | EP1378587A1 High-temperature articles and method for making |
| 01/07/2004 | EP1378583A1 Method of forming a hollow channel on the surface of a metal substrate, and related articles |
| 01/07/2004 | EP1378579A1 Precipitation hardened Co-Ni based heat-resistant alloy and production method therefor |
| 01/07/2004 | EP1378553A1 Method for re-bonding a dislodged part |
| 01/06/2004 | US6673709 Formation of an aluminide coating, incorporating a reactive element, on a metal substrate |
| 01/06/2004 | US6672838 Method for making a metallic article with integral end band under compression |
| 01/06/2004 | US6672145 Apparatus and method for testing jet engine fuel manifold flow distribution |
| 01/06/2004 | US6672075 Liquid cooling system for gas turbines |
| 01/06/2004 | US6672074 Gas turbine |
| 01/06/2004 | US6672072 Pressure boosted compressor cooling system |
| 01/06/2004 | US6672071 Methods for operating gas turbine engines |
| 01/06/2004 | US6672069 Method and device for increasing the pressure of a gas |
| 01/06/2004 | US6672068 Ramjet for a supersonic and hypersonic aircraft |
| 01/06/2004 | US6672049 Emergency device for relighting a windmilling turbojet |
| 01/06/2004 | CA2289420C High temperature corrosion-resistant and abrasion-resistant coating member, and manufacturing method thereof |
| 01/02/2004 | EP1377140A2 Improved film cooling for microcircuits |
| 01/02/2004 | EP1376534A1 Manufacturing process for a double resonator acoustic panel |
| 01/02/2004 | EP1375983A2 Replaceable brush seal elements |
| 01/02/2004 | EP1375867A2 Intercooling process and intercooled gas turbine engine |
| 01/02/2004 | EP1375866A2 Inlet bleed heater for heating inlet air to a compressor and methods of fabricating and transporting the heater |
| 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 | EP1374252A1 A nuclear power plant and a method of conditioning its power generation circuit |
| 01/02/2004 | EP1373702A1 Tortuous path exhaust eductor system |
| 01/02/2004 | EP1373686A1 Rotor gap control module |
| 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 | US20040001751 Inlet bleed heater for heating inlet air to a compressor and methods of fabricating and transporting the heater |
| 01/01/2004 | US20040000761 Replaceable brush seal elements |
| 01/01/2004 | US20040000656 Dual actuator air turbine starter valve |
| 01/01/2004 | US20040000148 Gas turbine engine |
| 01/01/2004 | US20040000146 Gas turbine combustor and operating method thereof |
| 01/01/2004 | US20040000050 Method of repairing shroud tip overlap on turbine buckets |
| 12/31/2003 | WO2004001208A1 Flow divider and ecology valve |
| 12/31/2003 | CN2596036Y High pressure shutoff valve used for gas combustion |
| 12/31/2003 | CN2596035Y Mini combustion turbine heat regenerator |
| 12/31/2003 | CN1464960A Flanged hollow structure |
| 12/31/2003 | CN1464937A Plate like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner |
| 12/31/2003 | CN1464912A Ni base sintered alloy |
| 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 | US6670021 Monolithic ceramic attachment bushing incorporated into a ceramic matrix composite component and related method |
| 12/30/2003 | US6669914 Internal combustion engine having a catalytic reactor |
| 12/30/2003 | US6669393 Connector assembly for gas turbine engines |
| 12/30/2003 | US6668906 Shaped core for cast cooling passages and enhanced part definition |
| 12/30/2003 | US6668559 Fastening a CMC combustion chamber in a turbomachine using the dilution holes |
| 12/30/2003 | US6668540 Gas turbine exhaust passage and damper system for same |
| 12/30/2003 | US6668538 Steam cooled gas turbine system with regenerative heat exchange |
| 12/30/2003 | CA2352022C Turbocharger support |
| 12/30/2003 | CA2117241C Improvements in or relating to gas turbine engines |
| 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 |
| 12/25/2003 | US20030233823 Flow divider and ecology valve |
| 12/24/2003 | WO2003107325A1 Method for making a soundproofing panel with at least one double resonator |
| 12/24/2003 | WO2003106817A1 Method for operating a gas turbine installation, and gas turbine installation |
| 12/24/2003 | CN1463407A Managing method for filter and filter to be managed by same |
| 12/24/2003 | CN1463345A Combustor for gas turbine |
| 12/24/2003 | CN1463299A Method for repairing component made from Ni-based alloy |
| 12/23/2003 | US6666029 Gas turbine pilot burner and method |
| 12/23/2003 | US6666028 Operation method for combined plant |
| 12/23/2003 | US6666027 Turbine power generation systems and methods using off-gas fuels |
| 12/23/2003 | US6666026 Process for preheating suction air by waste heat in power engines |
| 12/23/2003 | US6666014 Two-level pressurization valve controlled by a fuel metering unit |
| 12/23/2003 | CA2352021C Turbocharger shaft dual phase seal |
| 12/19/2003 | CA2432492A1 Linked manufacturable, non-plugging microcircuits |
| 12/19/2003 | CA2432490A1 Improved film cooling for microcircuits |
| 12/18/2003 | WO2003104630A1 A turbine and a component |
| 12/18/2003 | WO2003104629A1 Gas turbine group |
| 12/18/2003 | WO2003104511A2 Thermal spray compositions for abradable seals |
| 12/18/2003 | WO2003104164A1 Heat resistant product |
| 12/18/2003 | US20030233248 Gas turbine intake air filter selecting system |
| 12/18/2003 | US20030231955 Failsafe film cooled wall |
| 12/18/2003 | US20030230690 Dual extrusion snap closed ceiling sign hanger |
| 12/17/2003 | EP1371906A2 Gas turbine engine combustor can with trapped vortex cavity |
| 12/17/2003 | EP1371815A1 Abradable metallic or ceramic material; articles, casings comprising said material and its process for preparing |
| 12/17/2003 | EP1371439A1 Method of weld repairing a component with a refractory metal backing material |
| 12/17/2003 | EP1214172B1 Laser cladding a turbine engine vane platform |
| 12/17/2003 | EP0894943B1 Gas turbine rotor for steam cooling |
| 12/16/2003 | US6663530 Zero twist carrier |
| 12/16/2003 | US6663346 Compressor stator inner diameter platform bleed system |
| 12/16/2003 | US6662568 Hollow structure with flange |
| 12/16/2003 | US6662567 Transition duct mounting system |
| 12/16/2003 | US6662547 Combustor |