| 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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| 04/06/2004 | US6715296 Method for starting a power plant |
| 04/01/2004 | WO2004027976A1 Improved torque generation for salient-pole synchronous machine for start-up of a prime mover |
| 04/01/2004 | WO2004027234A1 Internally mounted radial flow intercooler for a combustion air charger |
| 04/01/2004 | WO2004026689A1 Torsionally de-coupled engine mount system |
| 04/01/2004 | US20040062865 Gas distributor for vapor coating method and container |
| 04/01/2004 | US20040062864 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure |
| 04/01/2004 | US20040062639 Turbine engine shroud assembly including axially floating shroud segment |
| 04/01/2004 | US20040062637 Integral swirl knife edge injection assembly |
| 04/01/2004 | US20040062460 Oil-damped rolling bearing |
| 04/01/2004 | US20040060347 Method and system for detecting damage to the rotor of an aircraft engine |
| 04/01/2004 | US20040060302 Turbine power plant, installation process and removal process of the turbine power plant |
| 04/01/2004 | US20040060295 Gas turbine combustor |
| 04/01/2004 | US20040060280 Acoustic-structural LPC splitter |
| 04/01/2004 | US20040060278 Passive cooling system for auxiliary power unit installation |
| 04/01/2004 | US20040060277 Gas turbine electric power generation equipment and air humidifier |
| 04/01/2004 | US20040060276 Gas turbine installation |
| 04/01/2004 | DE10342777A1 Betriebssteuer- bzw. -regelvorrichtung und Betriebssteuer- bzw. -regelverfahren für ein kombiniertes Einwellen-Kraftwerk Operation control regulating system and operation control -regelverfahren for a combined single-shaft power plant |
| 04/01/2004 | DE10244192A1 Gasturbine mit Vorrichtung zur Arbeitsentnahme zur Kühlung von Scheiben Gas turbine with a device to work removing the cooling of discs |
| 04/01/2004 | CA2499376A1 Internally mounted radial flow intercooler for a combustion air charger |
| 03/31/2004 | EP1403486A2 Acoustic-structural LPC splitter |
| 03/31/2004 | EP1403469A2 Method for selective surface protection of a gas turbine blade |
| 03/31/2004 | EP1403397A1 Cobalt-based alloy for the coating of components subject to erosion by liquid |
| 03/31/2004 | EP1403395A1 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure |
| 03/31/2004 | EP1403003A2 Methods and apparatus for securing components for manufacture |
| 03/31/2004 | EP1403002A2 Methods and apparatus for securing components for manufacture |
| 03/31/2004 | EP1402161A1 Power generator with low co2 emissions and associated method |
| 03/31/2004 | EP1402152A1 Securing system for the rotor blades of axial flow turbo engines |
| 03/31/2004 | EP1152851A4 Die casting of high temperature material |
| 03/31/2004 | CN1485571A Backlight assembly and liquid crystal display device using the same |
| 03/31/2004 | CN1143954C 燃气轮机 Gas turbine |
| 03/31/2004 | CN1143953C Method for operating exhaust gas recirculation type gas turbine |
| 03/31/2004 | CN1143949C Gas and turbine installation and method for operating an installation of this type |
| 03/31/2004 | CN1143948C Method of operating waste-heat steam generator, and waste-heat steam geneartor operated by this method |
| 03/30/2004 | US6713892 Automatic turbogenerator restarting system |
| 03/30/2004 | US6712120 Device and method for casting a workpiece and workpiece |
| 03/30/2004 | US6711952 Method and system for monitoring bearings |
| 03/30/2004 | US6711902 Integrated cycle power system and method |
| 03/30/2004 | US6711889 Gas turbine engine |
| 03/30/2004 | US6711888 Gas turbine |
| 03/25/2004 | WO2004025147A1 Multidirectional turbine shim seal |
| 03/25/2004 | WO2004025102A1 A gas turbine fogging system and methods for its control and trouble detection |
| 03/25/2004 | WO2004025086A1 Gas turbine sealing air supply system |
| 03/25/2004 | WO2004024971A1 Property recovering method for nickel superalloy |
| 03/25/2004 | US20040058200 Method of forming a ceramic coating on a substrate by electron-beam physical vapor deposition |
| 03/25/2004 | US20040057881 Apparatus and method for initiating a combustion reaction with slurry fuel |
| 03/25/2004 | US20040057832 Gas turbine blade |
| 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 | US20040057257 Electric start for a prime mover |
| 03/25/2004 | US20040056487 Torque generation for salient-pole synchronous machine for start-up of a prime mover |
| 03/25/2004 | US20040056399 Methods and apparatus for securing components for manufacture |
| 03/25/2004 | US20040055900 Apparatus and methods for sampling and analyzing inlet air associated with combustion turbine |
| 03/25/2004 | US20040055740 Internally mounted radial flow intercooler for a combustion air charger |
| 03/25/2004 | US20040055736 Method of making turbine blades having cooling channels |
| 03/25/2004 | US20040055310 Control system for positioning compressor inlet guide vanes |
| 03/25/2004 | US20040055308 Burner apparatus for burning fuel and air |
| 03/25/2004 | US20040055273 Gas turbine control system |
| 03/25/2004 | US20040055272 Operation control apparatus and operation control method for single-shaft combined plant |
| 03/25/2004 | US20040055271 Installation for the generation of energy |
| 03/25/2004 | US20040055270 Premixed burner with profiled air mass stream, gas turbine and process for burning fuel in air |
| 03/25/2004 | US20040055134 Methods and apparatus for securing components for manufacture |
| 03/25/2004 | DE4431291B4 Hochtemperatursonde High temperature probe |
| 03/25/2004 | DE10010117B4 Beschichtete Kompressorleiteinrichtung Coated Kompressorleiteinrichtung |
| 03/24/2004 | EP1400756A1 Gas turbine combustor |
| 03/24/2004 | EP1400755A1 Flanged hollow structure |
| 03/24/2004 | EP1400754A1 Premixed pilot burner for a combustion turbine engine |
| 03/24/2004 | EP1400752A1 Premixed burner with profiled air mass stream, gas turbine and process for burning fuel in air |
| 03/24/2004 | EP1400750A2 Double wall combustor liner segment with cooling channels |
| 03/24/2004 | EP1400669A1 Gas turbine engine with apparatus for generation of mechanical work for cooling of discs |
| 03/24/2004 | EP1400610A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides |
| 03/24/2004 | EP1400300A1 Layered heat-resistant alloy plate and method of producing the same |
| 03/24/2004 | EP1399659A1 Method and installation for energy production by means of a gas turbine associated with an air separation unit |
| 03/24/2004 | EP0828925B1 A liquefied natural gas (lng) fueled combined cycle power plant and an lng fueled gas turbine plant |
| 03/24/2004 | CN1484836A A nuclear power plant and method of operating the same |
| 03/24/2004 | CN1143056C Discharge header for guiding hot gas in gas turbine |
| 03/24/2004 | CN1143054C Electric power generation by combined plant with one gas turbine and noe steam turbine |
| 03/23/2004 | US6709492 Planar membrane deoxygenator |
| 03/23/2004 | US6709237 Turbine blade or vane and process for producing a turbine blade or vane |
| 03/23/2004 | US6709024 Method and apparatus for assembling couplings for transferring fluids |
| 03/23/2004 | US6708711 Air inlet for commercial aircraft jet engine nacelle |
| 03/23/2004 | US6708568 Combustion chamber dynamic pressure transducer tee probe holder and related method |
| 03/18/2004 | WO2004023042A1 Gas turbine combustion chamber |
| 03/18/2004 | WO2004022948A1 Jet motor or turbine motor |
| 03/18/2004 | WO2004022927A1 Fan case design with metal foam between kevlar |
| 03/18/2004 | US20040051254 Multidirectional turbine shim seal |
| 03/18/2004 | US20040050909 Diffusion bond mixture for healing single crystal alloys |
| 03/18/2004 | US20040050071 Methods and apparatus for supporting variable bypass valve systems |
| 03/18/2004 | US20040050070 Fluid injector and injection method |
| 03/18/2004 | US20040050066 System and method for efficient load following control logic for a turbogenerator operating in stand-alone mode |
| 03/18/2004 | US20040050065 Gas compression system and method for microturbine application |
| 03/18/2004 | US20040050061 Compact swirl augmented afterburners for gas turbine engines |
| 03/18/2004 | US20040050060 Thermal sheild stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine |
| 03/18/2004 | US20040050059 Double wall combustor liner segment with enhanced cooling |
| 03/18/2004 | US20040050049 Heat engines and associated methods of producing mechanical energy and their application to vehicles |
| 03/18/2004 | DE10243389A1 Exhaust gas turbo charger for an internal combustion engine (ICE) has a turbine to make a torque-proof link via a turbine shaft to a compressor for sucking in/delivering compressed gases to the ICE |
| 03/17/2004 | EP1398571A2 Fabricated cowl for double annular combustor of a gas turbine engine and method of making same |
| 03/17/2004 | EP1398569A1 Gas turbine |
| 03/17/2004 | EP1398566A2 Fluid injector and injection method |
| 03/17/2004 | EP1398474A2 Compressor bleed case |
| 03/17/2004 | EP1398473A1 Acoustic attenuation layer for an acoustic attenuation panel, and a panel with such a layer |
| 03/17/2004 | EP1398472A1 Tubular acoustic attenuation piece for the air inlet of an aircraft engine |