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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10/19/2004 | US6805535 Device and method for producing a blade for a turbine and blade produced according to this method |
10/19/2004 | US6805483 System for determining gas turbine firing and combustion reference temperature having correction for water content in combustion air |
10/19/2004 | US6805140 Probe with longitudinal axis and perpendicular offset nozzles connected to common manifold; aircraft engines |
10/19/2004 | US6804946 Combustion system with shutdown fuel purge |
10/19/2004 | CA2284487C Combined cycle power plant |
10/19/2004 | CA2263834C Hot gas-carrying gas collection pipe of gas turbine |
10/14/2004 | WO2004087839A1 Fluidized bed gasifier, gas fuel producing method, and gas power generation system |
10/14/2004 | US20040202569 Precipitation-strengthened nickel-iron-chromium alloy and process therefor |
10/14/2004 | US20040202544 Methods and apparatus for assembling rotatable machines |
10/14/2004 | US20040202542 Turbine element |
10/14/2004 | US20040200887 Method of fabricating a hollow mechanical part by diffusion welding and superplastic forming |
10/14/2004 | US20040200288 Combustion chamber dynamic pressure transducer tee probe holder and related method |
10/14/2004 | US20040200224 Method and installation for feeding an air separation plant with a gas turbine |
10/14/2004 | US20040200215 Bearing system for high-speed rotating machinery |
10/14/2004 | US20040200207 Gas turbine apparatus |
10/14/2004 | US20040200206 Gas turbine apparatus |
10/14/2004 | DE10313490A1 Axial durchströmte thermische Turbomaschine Axial-flow thermal turbomachinery |
10/14/2004 | DE10313489A1 Axial durchströmte thermische Turbomaschine Axial-flow thermal turbomachinery |
10/13/2004 | EP1467065A2 Turbine blade |
10/13/2004 | EP1467063A1 Methods and apparatus for assembling rotatable machines |
10/13/2004 | EP1466993A1 Heat resisting steel, gas turbine using the steel, and components thereof |
10/13/2004 | EP1466692A1 Method of manufacturing a hollow workpiece by diffusion welding and superplastic forming |
10/13/2004 | EP1466084A1 Gas turbine group |
10/13/2004 | EP1466037A1 High-temperature protective coating |
10/13/2004 | EP1244870B1 Silencer for the compressor of an exhaust gas turbocharger |
10/13/2004 | CN1537212A Combustion chamber device |
10/13/2004 | CN1536214A Improved high temp. splashboard |
10/13/2004 | CN1536210A Improved high-temperature central body utilizing light reflection to reduce temperature and its manufacturing method |
10/13/2004 | CN1536200A Turbo-element |
10/13/2004 | CN1536199A Method and equipment for assembling rotary machine |
10/13/2004 | CN1171036C Combustion chamber unit of gas turbine |
10/12/2004 | US6802690 Outlet silencer structures for turbine |
10/12/2004 | US6802479 Flammable fluid line shroud |
10/12/2004 | US6802178 Fluid injection and injection method |
10/12/2004 | CA2290552C Brush-hair seal |
10/08/2004 | CA2463390A1 Turbine element |
10/07/2004 | WO2004085816A1 Temperature measuring device and regulation of the temperature of hot gas of a gas turbine |
10/07/2004 | WO2004085338A1 Material for thermal barrier coating |
10/07/2004 | WO2004085031A1 Suction filter, turbo compressor, and method of packaging the compressor |
10/07/2004 | US20040197486 Method of applying environmental and bond coatings to turbine flowpath parts |
10/07/2004 | US20040196951 Nuclear power plant and a method of conditioning its power generation circuit |
10/07/2004 | US20040195437 Protection device for a jet engine air intake structure |
10/07/2004 | US20040195397 Ejector device for direct injection fuel jet |
10/07/2004 | US20040194941 Active cooling panel of thermostructural composite material and method for its manufacture |
10/07/2004 | US20040194627 System and method for thermal management |
10/06/2004 | EP1464791A1 Process and apparatus for manufacturing a turbine component |
10/06/2004 | EP1464722A2 Method of applying environmental and bond coating to turbine flowpath parts |
10/06/2004 | EP1464721A2 Thermal barrier coating system |
10/06/2004 | EP1464376A1 Planar membrane deoxygenator |
10/06/2004 | EP1463879A1 A gas turbine apparatus and a starting method thereof |
10/06/2004 | EP1131537B1 method for operating a turbo-machine |
10/06/2004 | EP0955455B1 Power generation method and power generating apparatus |
10/06/2004 | CN1535350A Blade for turbine engine and method for production of said blade |
10/06/2004 | CN1533821A 过滤装置 Filtration device |
10/05/2004 | US6799425 Method for converting thermal energy into mechanical work |
09/30/2004 | WO2004083730A1 Gas turbine |
09/30/2004 | US20040192500 Control apparatus and control method for automatic transmission |
09/30/2004 | US20040191544 Thermal barrier coating system |
09/30/2004 | US20040187472 Method and system for reducing turbine exhaust turbulence |
09/29/2004 | EP1463195A1 Turbine generator start method and turbine generation system |
09/29/2004 | EP1462664A2 Methods and apparatus for joining gas turbine parts together |
09/29/2004 | EP1462633A1 Measuring and controlling of the hot gas temperature of a gas turbine |
09/29/2004 | EP1462617A2 Blading for an axial-flow turbomachine |
09/29/2004 | EP1462614A2 Axial-flow thermal turbomachine |
09/29/2004 | EP1462609A1 Turbomachine blade with reduced weight and it's production method |
09/29/2004 | EP1462606A1 Multi-component hybrid turbine blade |
09/29/2004 | EP1461544A1 Reduced twist carrier |
09/29/2004 | EP1461521A2 Fuel vaporization systems for vaporizing liquid fuel |
09/29/2004 | EP1071831B1 Method for producing fibre reinforced metallic components |
09/29/2004 | CN1532376A First stage protective cover structure of turbomachine and reinforced maintenance method |
09/29/2004 | CN1168945C System for supplying thermoelectricity |
09/28/2004 | US6799112 Methods and apparatus for operating gas turbine engines |
09/28/2004 | US6798079 Turbine power generator including supplemental parallel cooling and related methods |
09/28/2004 | US6796765 Methods and apparatus for assembling gas turbine engine struts |
09/28/2004 | US6796764 Turbine fuel pump |
09/28/2004 | CA2353374C Self cleaning braze material |
09/23/2004 | WO2004081482A1 A bypass valve for a gas turbine engine recuperator system |
09/23/2004 | US20040184912 Gas turbine stator housing |
09/23/2004 | US20040182330 Method for operating an internal combustion engine |
09/23/2004 | US20040182085 Combustion chamber |
09/23/2004 | US20040182083 Integrated cycle power system and method |
09/23/2004 | DE10310815A1 Wirbelgleichrichter in Röhrenbauweise mit Haltering Vortex reducer tube construction with retaining ring |
09/23/2004 | DE102004012626A1 Turbinendüse mit Leckströmungs-Dichtungsstegen und zugeordnetes Schweissverfahren Turbine nozzle with leak flow sealing lands and associated welding processes |
09/22/2004 | EP1460340A1 Gasturbine |
09/22/2004 | EP1458981A1 Compressor for gas turbines |
09/22/2004 | EP1458967A1 Gas turbine engine with offset drive |
09/22/2004 | EP1458563A1 Foam wall combustor construction |
09/22/2004 | EP1198664B1 Draining device for the fuel supply system of a gas turbine engine |
09/22/2004 | CN1530528A Improved high-temperature turbine nozzle with light decreasement by light reflection and manufactuirng process |
09/22/2004 | CN1530520A Turbonazzle with sealed zone of parasitic wings anjd welding method thereof |
09/22/2004 | CN1530517A Internal core outline for vortex blade |
09/21/2004 | US6793457 Fabricated repair of cast nozzle |
09/21/2004 | US6793175 Supersonic external-compression diffuser and method for designing same |
09/21/2004 | US6792763 Coated seal article with multiple coatings |
09/21/2004 | US6792762 Gas turbine equipment and gas turbine cooling method |
09/21/2004 | US6792760 Method for operating a turbine |
09/21/2004 | US6792756 Gas supply control device for a gas storage power plant |
09/21/2004 | US6792746 Separated core engine type turbofan engine |
09/21/2004 | US6792655 Apparatus for correcting airfoil twist |
09/21/2004 | CA2209881C Apparatus and method for reducing noise emissions from a gas turbine engine inlet |