| 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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| 03/17/2004 | EP1398464A2 Supporting variable bypass valve in a gas turbine |
| 03/17/2004 | EP1398394A1 Cold spraying method for MCrAIX coating |
| 03/17/2004 | EP1398393A1 Property recovering method |
| 03/17/2004 | EP1398098A1 Method for fabrication of turbine blades with cooling channels |
| 03/17/2004 | EP1397810A1 A brayton cycle nuclear power plant and a method of starting the brayton cycle |
| 03/17/2004 | EP1397588A2 Method for operating an internal combustion engine |
| 03/17/2004 | EP1397584A1 Gas turbine arrangement |
| 03/17/2004 | CN1483122A Device and method for supersound-reinforced continuous stream fuel-injection |
| 03/17/2004 | CN1482345A Stator vane actuator in gas turbine engine |
| 03/16/2004 | US6706241 Nickel-base superalloy |
| 03/16/2004 | US6705831 Linked, manufacturable, non-plugging microcircuits |
| 03/16/2004 | US6705569 Axi-symmetric mixed compression inlet with variable geometry centerbody |
| 03/16/2004 | US6705074 Gas turbine with water injection |
| 03/16/2004 | US6705073 Gas turbine plant and process for limiting a critical process value |
| 03/16/2004 | US6705011 Turbine element manufacture |
| 03/16/2004 | CA2349509C Steam cooled gas turbine system |
| 03/11/2004 | WO2004020805A1 Nested channel ducts for nozzle construction and the like |
| 03/11/2004 | WO2003098020A3 Gas turbine with stator shroud in the cavity beneath the chamber |
| 03/11/2004 | US20040047731 Method and apparatus for varying the critical speed of a shaft |
| 03/11/2004 | US20040047725 Ring segment of gas turbine |
| 03/11/2004 | US20040046326 Gas turbine |
| 03/11/2004 | US20040045936 Chemical milling of gas turbine engine blisks |
| 03/11/2004 | US20040045767 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes |
| 03/11/2004 | US20040045766 Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer |
| 03/11/2004 | US20040045765 Tubular acoustic attenuation piece for an aircraft jet engine air intake |
| 03/11/2004 | US20040045302 Integrated gas turbine compressor-rotary fuel injector |
| 03/11/2004 | US20040045301 Fabricated cowl for double annular combustor of a gas turbine engine and method of making same |
| 03/11/2004 | US20040045294 Gas turbine plant |
| 03/11/2004 | US20040045274 Combined cycle gas turbine system |
| 03/11/2004 | US20040045271 Methods and apparatus for exhausting gases from gas turbine engines |
| 03/10/2004 | EP1396611A2 Method and apparatus for varying the critical speed of a shaft |
| 03/10/2004 | EP1396609A2 Gas turbine with a spacer member and a turbine rotor disk defining an air cooling passage |
| 03/10/2004 | EP1396608A2 Integrally bladed rotor |
| 03/10/2004 | EP1395783A1 Method and installation for feeding an air separation plant with a gas turbine |
| 03/10/2004 | CN1481293A Method for smoothing surface of gas turbine blade |
| 03/09/2004 | US6704625 Aircraft architecture with a reduced bleed aircraft secondary power system |
| 03/09/2004 | US6702873 High particle separation efficiency system |
| 03/09/2004 | US6702547 Gas turbine |
| 03/09/2004 | US6701616 Method of repairing shroud tip overlap on turbine buckets |
| 03/04/2004 | WO2004018856A1 Integrated flywheel |
| 03/04/2004 | WO2004018844A1 Recirculation structure for a turbocompressor |
| 03/04/2004 | WO2003102494A3 Flame detection method and apparatus for gas turbine exhaust path |
| 03/04/2004 | WO2003098006A3 Turbine no-load speed limiter |
| 03/04/2004 | WO2002080189B1 A nuclear power plant and a method of conditioning its power generation circuit |
| 03/04/2004 | US20040042927 Gas turbine blades; chemical and heat resistance |
| 03/04/2004 | US20040042909 Compression feed for high humidity fuel gas |
| 03/04/2004 | US20040042902 Organic matrix composite integrally bladed rotor |
| 03/04/2004 | US20040042900 Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots |
| 03/04/2004 | US20040042896 Gas turbine shaft and heat shield cooling arrangement |
| 03/04/2004 | US20040042692 Foil bearing |
| 03/04/2004 | US20040042691 Foil bearing |
| 03/04/2004 | US20040042579 Nuclear power plant and method of operating the same |
| 03/04/2004 | US20040041348 Floating brush seal assembly |
| 03/04/2004 | US20040040360 Method of manufacturing blade retainer and manufacturing devices therefor |
| 03/04/2004 | US20040040314 Gas turbine and spacer member for the use therein |
| 03/04/2004 | US20040040313 Gas turbine power generation system |
| 03/04/2004 | US20040040309 Gas turbine and method for operating a gas turbine |
| 03/04/2004 | US20040040306 Nested channel ducts for nozzle construction and the like |
| 03/04/2004 | US20040040280 Heat exchanger for power generation equipment |
| 03/04/2004 | US20040040279 System for control and regulation of the flame temperature for single-shaft gas turbines |
| 03/04/2004 | DE20319241U1 Rotor injector valve for thermal turbo-engines in a fuel supply system in a rotor air mass measuring device comprises a rotor impeller fixed or rotatably arranged upstream |
| 03/04/2004 | DE10325311A1 Kraftstoffkreiselpumpe Fuel centrifugal pump |
| 03/03/2004 | EP1394711A1 Filter control method, and filter controlled by the method |
| 03/03/2004 | EP1394505A2 Methods and apparatus for securing components for inspection |
| 03/03/2004 | EP1394390A1 Gas turbine plant |
| 03/03/2004 | EP1394389A1 Improved heat exchanger for power generation equipment |
| 03/03/2004 | EP1394388A2 System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine |
| 03/03/2004 | EP1394362A2 Floating brush seal assembly |
| 03/03/2004 | EP1394361A1 Gas turbine |
| 03/03/2004 | EP1394358A2 Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots |
| 03/03/2004 | EP1394278A1 Reduced-tantalum superalloy composition and article made therefrom, and method for selecting a reduced-tantalum superalloy |
| 03/03/2004 | EP1392958A1 Rapid shutdown and ecology system for engine fuel control systems |
| 03/03/2004 | EP1392957A1 Abradeable seal system |
| 03/03/2004 | CN1478999A Control method of gas fuel engine fuel flow quantity and its flow quantity control valve |
| 03/03/2004 | CN1478993A Improved heat exchanger of generating equipment |
| 03/02/2004 | US6699604 Protective coating including porous silicon nitride matrix and noble metal |
| 03/02/2004 | US6698920 Temperature measuring system and optical switch used therein |
| 03/02/2004 | US6698645 Method of producing fiber-reinforced metallic building components |
| 03/02/2004 | US6698182 Gas turbine combined plant |
| 03/02/2004 | US6698180 Efficient dual air flow |
| 02/26/2004 | WO2004017301A1 Device and method for active soundproofing, and power unit for aeroplanes |
| 02/26/2004 | WO2004016921A1 System for cooling cooling air in a gas turbine, and method for cooling cooling air |
| 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 | US20040038086 Thermal barrier coatings with low thermal conductivity |
| 02/26/2004 | US20040038085 Heat resistant layer is made of a mixed oxide containing 15 mol % of at least one lanthanide sesquioxide, selected from LA, Pr, Nd, Sm, Eu, Tb and mixtures, and balance oxide selected from zirconia, ceria, and hafnia |
| 02/26/2004 | US20040037699 Connecting system for a transition duct in a gas turbine |
| 02/26/2004 | US20040037696 Drainage system for gas turbine supporting bearings |
| 02/26/2004 | US20040036230 Sealing structure for combustor liner |
| 02/26/2004 | US20040035163 Apparatus and method of correcting deformation of gas turbine blade |
| 02/26/2004 | US20040035118 Blade cooling in a gas turbine engine |
| 02/26/2004 | US20040035117 Method and system power production and assemblies for retroactive mounting in a system for power production |
| 02/26/2004 | DE20215521U1 Lufteinlassgehäuse, insbesondere für den Lufteinlass von Gasturbinen Air inlet housing, in particular for the intake air of gas turbines |
| 02/25/2004 | EP1392087A1 Method for plasma-catalytic conversion of fuels that can be used in an internal combustion engine or a gas turbine into a synthetic gas and the plasma-catalytic converter used for same |
| 02/25/2004 | EP1391597A2 Noise reduction conduit for static components in aircraft engines |
| 02/25/2004 | EP1391596A1 Gas turbine plant |
| 02/25/2004 | EP1391582A2 Sealing structure for combustor liner |
| 02/25/2004 | EP1391531A2 Thermal barrier coating with nitride particles |
| 02/25/2004 | EP1391527A1 Nickel-base alloy |
| 02/25/2004 | EP1390670A1 Heat shield arrangement for a hot-gas conducting component, in particular for structural pieces of gas turbines and method for production of said arrangement |