Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
10/2003
10/16/2003WO2002029224A8 Air intake guard for engine
10/16/2003US20030195113 Reproducing a used high temperature denitration catalyst into an intermediate temperature denitration catalyst and reusing the product
10/16/2003US20030192737 Outlet silencer and heat recovery structures for gas turbine
10/16/2003US20030192317 Method of combustor cycle airflow adjustment
10/15/2003EP1353054A1 Turboprop engine
10/15/2003EP1353042A2 A gas turbine single plant modifying method, a catalyst re-using method and a re-produced catalyst
10/15/2003EP1352989A1 Object having a masking layer
10/15/2003EP1352985A1 Thermal barrier coating system
10/15/2003EP1352196A2 Control strategy for flexible catalytic combustion system
10/15/2003EP1352161A2 Main propulsion engine system integrated with secondary power unit
10/15/2003EP0919701B1 Sealing structure for joint surfaces of flanges of gas turbine
10/15/2003CN1449471A Combined cycle power generation plant and method of operating such a plant
10/14/2003US6632257 Fuel composition and method for extending the time between turbine washes when burning ash bearing fuel in a turbine
10/14/2003US6631753 Clean melt nucleated casting systems and methods with cooling of the casting
10/14/2003US6631561 Turbine blade and method for producing a turbine blade
10/14/2003CA2075778C Trenched brush seal
10/09/2003WO2003083268A1 Refrigeration power plant
10/09/2003US20030189339 Electrical system for turbine/alternator on common shaft
10/08/2003EP1350927A2 Shroud segment, manufacturing method for a shroud segment, as well as shroud assembly for a turbine engine
10/08/2003EP1350860A1 Process of masking cooling holes of a gas turbine component
10/08/2003EP1350019A2 Fluid and fuel delivery systems reducing pressure fluctuations and engines including such systems
10/08/2003EP1350018A1 Combustor turbine successive dual cooling
10/08/2003EP1349695A1 Laser machining cooling holes in gas turbine components
10/08/2003EP0943069B1 An electricity generating system having an annular combustor
10/08/2003CN1447878A Device and method for preheating combustibles in combined gas and turbine installations
10/08/2003CN1123683C Gas/steam generating equipment
10/08/2003CN1123682C Combined circulation generating unit
10/08/2003CN1123680C Process and appts. for achieving power augementation in gas turbines via wet compression
10/07/2003US6630244 Fuel injectors having siloxane-acrylate graft copolymer protective layer; durability
10/07/2003US6630198 Injecting a first liquid into the engine to remove particulate matter, and then injecting a second liquid to reduce particulate formation, such as an antistatic liquid
10/07/2003US6629817 System and method for airfoil film cooling
10/07/2003US6629413 Thermodynamic apparatus
10/07/2003US6629368 Method for isothermal brazing of single crystal components
10/07/2003CA2065722C Boltless turbine nozzle/stationary seal mounting
10/02/2003WO2003080432A1 Apparatus and method for variation of a wall skin
10/02/2003US20030187530 Rotation planning apparatus and rotation planning system
10/02/2003US20030186076 Layered heat-resistant alloy plate and method of producing the same
10/02/2003US20030185675 Rotor insert assembly and method of retrofitting
10/02/2003US20030185674 Shroud segment and assembly for a turbine engine
10/02/2003US20030185669 Aspirating face seal with axially extending seal teeth
10/02/2003US20030184022 Aspirating face seal with axially biasing one piece annular spring
10/02/2003US20030183272 Air intake for an auxiliary power unit in an aircraft
10/02/2003US20030183188 Modification of lubricant properties in a recirculating lubricant system
10/02/2003US20030182945 Nozzle with fluted tube
10/02/2003US20030182941 Combustion turbine inlet for air cooling via refrigerated liquid hydrocarbon fuel vaporization
10/01/2003EP1348898A1 Aspirating face seal with axially extending seal teeth
10/01/2003EP1348835A2 Valve assembly for gas turbine engine
10/01/2003EP1348834A2 Aspirating face seal with axially biasing one-piece annular spring
10/01/2003EP1348098A2 Turbine recuperator
10/01/2003EP1348071A2 Installation for the generation of energy
10/01/2003EP1348067A2 Metallic honeycomb cellular seal-structure for a turbomachine
10/01/2003CN1445437A Synthetic high-temp assembly and manufacturing method therefor
10/01/2003CN1122781C Low noise combustion method
09/2003
09/30/2003US6627019 Process for making ceramic matrix composite parts with cooling channels
09/30/2003US6626637 Cooling method for turbines
09/30/2003US6626230 Multi-wall core and process
09/30/2003US6625989 Method and apparatus for the cooling of jet-engine turbine casings
09/25/2003WO2003078813A1 Gas turbine apparatus
09/25/2003WO2003078812A1 Compressed air energy storage system with a heat maintenance system
09/25/2003US20030181140 Shaping tool and method for shaping curved surfaces on workpieces
09/25/2003US20030180147 Turbrine vane system
09/25/2003US20030177767 Compressed air energy storage system
09/25/2003US20030177755 Gas turbine intake air filter unit
09/24/2003EP1347151A2 Hybrid high temperature airfoil and method of making the same
09/24/2003EP1346790A2 Shaping tool and method for shaping curved surfaces on workpieces
09/24/2003EP1346179A1 Ultrasonically enhanced continuous flow fuel injection apparatus and method
09/24/2003EP1345732A1 Method for smoothing the surface of a gas turbine blade
09/24/2003EP1117588B1 Aircraft engine air intake system
09/24/2003EP1084371B1 Impingement and film cooling for gas turbine combustor walls
09/24/2003CN1443927A Equipment for fixing supporting blades of disributor component arround circumferential curved line
09/24/2003CN1122148C Electricity generating system having annular combustion chamber
09/23/2003US6623254 High pressure water pump
09/23/2003US6623238 Air turbine starter with seal assembly
09/23/2003US6622490 Turbine power plant having an axially loaded floating brush seal
09/23/2003US6622487 Fluid flow control valve
09/23/2003US6622475 Bleed system driven in simplified manner for a turbojet or turboprop engine
09/23/2003US6622473 Speed-reducing gear unit to absorb the axial loads generated by a turbojet fan
09/18/2003WO2003076787A1 Multi-spool by-pass turbofan engine
09/18/2003WO2003076782A1 Method for igniting the combustion chamber of a gas turbine installation and an ignition device for carrying out said method
09/18/2003WO2003076780A1 Method for operating a turbine
09/18/2003US20030176223 Gas turbine power generation facility
09/18/2003US20030175122 Hybrid high temperature articles and method of making
09/18/2003US20030173213 Supplying solution of alkali metal carbonate or bicarbonate to both anode and cathode chambers of electrolysis cell, which are separated by diaphragm, electrolyzing solution, mixing resulting cathode and anode water to obtain detergent
09/18/2003US20030172856 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine
09/18/2003US20030172641 Fuel injection system for a combustion engine
09/18/2003CA2477447A1 Multi-spool by-pass turbofan engine
09/17/2003EP1344916A2 Fuel system
09/17/2003EP1344915A2 A variable position intake for an aircraft mounted gas turbine engine
09/17/2003EP1343956A1 Bypass duct fan noise reduction assembly
09/17/2003EP1343951A2 Turbine bucket cover and brush seal
09/17/2003EP1343950A2 System to feed cooling air into a gas turbine rotor
09/17/2003EP1257373B1 Device and method for casting a workpiece and workpiece
09/17/2003CN1443274A Heat engines and associated methods of producing mechanical energy and their application to vehicle
09/17/2003CN1443270A Method for operating gas and steam turbine installation and corresponding installation
09/16/2003US6619939 Rotary pump
09/16/2003US6619916 Methods and apparatus for varying gas turbine engine inlet air flow
09/16/2003US6619915 Thermally free aft frame for a transition duct
09/16/2003US6619913 Fan casing acoustic treatment
09/16/2003US6619912 Turbine blade or vane
09/16/2003US6619908 Axial and radial seal arrangement
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