| 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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| 02/28/2005 | CA2476470A1 Turbine airfoil cooling flow particle separator |
| 02/24/2005 | WO2005017333A2 Wide-angle concentric diffuser |
| 02/24/2005 | WO2005016754A1 Device for stabilizing the engine inlet flow in static tests of engines |
| 02/24/2005 | WO2005016748A2 Dual action inlet door and method for use thereof |
| 02/24/2005 | WO2005016490A1 Separator systems |
| 02/24/2005 | US20050043905 Device for estimating the mass flow of fuel |
| 02/24/2005 | US20050043870 Method and apparatus for recording and retrieving maintenance, operating and repair data for turbine engine components |
| 02/24/2005 | US20050042474 High-temperature protection layer |
| 02/24/2005 | US20050042090 Methods and apparatus for fabricating gas turbine engines |
| 02/24/2005 | US20050042081 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle |
| 02/24/2005 | US20050042080 Device for controlling clearance in a gas turbine |
| 02/24/2005 | US20050040579 Method and apparatus to decrease combustor emissions |
| 02/24/2005 | US20050039463 Rotary injector |
| 02/24/2005 | US20050039460 Gas turbine fuel pilot nozzle |
| 02/24/2005 | US20050039459 High temperature splash plate for temperature reduction by optical reflection and process for manufacturing |
| 02/24/2005 | US20050039457 Turbine fuel ring assembly |
| 02/24/2005 | US20050039456 Fuel/air premixer for gas turbine combustor |
| 02/24/2005 | US20050039437 Turbofan variable fan nozzle |
| 02/24/2005 | US20050039436 Gas turbine installation |
| 02/24/2005 | US20050039435 Ice protection system for an aircraft engine |
| 02/24/2005 | US20050039433 Gas turbine power plant |
| 02/24/2005 | CA2545931A1 Separator systems |
| 02/23/2005 | EP1508965A2 Electric motor or generator |
| 02/23/2005 | EP1508881A1 Method and apparatus for recording and retrieving maintenance, operating and repair data for turbine engine components |
| 02/23/2005 | EP1508673A2 Methods for fabricating gas turbine engines |
| 02/23/2005 | EP1508671A2 A brush seal for gas turbine engines |
| 02/23/2005 | EP1508670A2 Cooled vane of a gas turbine |
| 02/23/2005 | CN1584297A Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method |
| 02/23/2005 | CN1584118A Upgrading of aluminide coating on used turbine engine component |
| 02/23/2005 | CN1584104A Turbine element repair |
| 02/23/2005 | CN1584103A Turbine element repair |
| 02/23/2005 | CN1190295C Repair of single crystal nickel superalloy part |
| 02/22/2005 | US6857847 Simplified support device for nozzles of a gas turbine stage |
| 02/22/2005 | US6857669 Device for connecting two tubular pieces of an aircraft turbine engine |
| 02/22/2005 | US6857441 Fluid metering device |
| 02/22/2005 | US6857325 Moving blade support jig, moving blade support apparatus, and flow rate measuring apparatus |
| 02/22/2005 | US6857320 Combustion chamber dynamic pressure transducer tee probe holder and related method |
| 02/22/2005 | US6857274 Fluid injector and injection method |
| 02/22/2005 | US6857271 Secondary fuel nozzle with readily customizable pilot fuel flow rate |
| 02/22/2005 | US6857270 Gas turbine plant |
| 02/22/2005 | CA2207828C Process for manufacturing a hollow turbine blade including separation after welding |
| 02/22/2005 | CA2129950C Turbomachine radial impeller vibration constraining and damping mechanism |
| 02/18/2005 | CA2478788A1 Abradable device on fan case for gas turbine engine |
| 02/17/2005 | WO2005015063A1 Slide ring and slide-ring seal assembly for jet engines |
| 02/17/2005 | US20050038570 Warning before pump limit or in case of blade failure on a turbomachine |
| 02/17/2005 | US20050036891 Thermal barrier coating for reduced sintering and increased impact resistance, and process of making same |
| 02/17/2005 | US20050036886 Center-located cutter teeth on shrouded turbine blades |
| 02/17/2005 | US20050035086 Upgrading aluminide coating on used turbine engine component |
| 02/17/2005 | US20050034464 Jet aircraft electrical energy production system |
| 02/17/2005 | US20050034462 System for warming pressurized gas |
| 02/17/2005 | US20050034458 Gas turbine engine combustor can with trapped vortex cavity |
| 02/17/2005 | DE10332043A1 Drive system for motor vehicle IC engine turbo charger, features electrical rotary motor for active torque improvement of the turbo charger |
| 02/16/2005 | EP1507080A1 Convergent-divergent turboreactor nozzle |
| 02/16/2005 | EP1507066A2 Center-located cutter teeth on shrouded turbine blades |
| 02/16/2005 | EP1507022A1 Thermal barrier coating for reduced sintering and increased impact resistance, and process of making same |
| 02/16/2005 | EP1507019A1 Upgrading aluminide coating on used turbine engine component |
| 02/16/2005 | EP1507015A1 High-temperature member for use in gas turbine |
| 02/16/2005 | EP1242729B1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method |
| 02/16/2005 | EP1228293B1 Method for producing a turbine blade |
| 02/16/2005 | EP1180196B1 Turbo-machine comprising a sealing system for a rotor |
| 02/16/2005 | CN2679366Y Dual-layer bar grate densification device |
| 02/16/2005 | CN1582366A Gas turbine system comprising closed system of fuel and combustion gas using underground coal layer |
| 02/16/2005 | CN1582364A 燃气涡轮机组 Gas turbines |
| 02/16/2005 | CN1582363A Stator for a turbomachine |
| 02/16/2005 | CN1580642A Thermal isolation device for liquid fuel components |
| 02/16/2005 | CN1580640A Combustor |
| 02/16/2005 | CN1580519A Microcircuit cooling for a turbine blade |
| 02/16/2005 | CN1580518A Microcircuit airfoil mainbody |
| 02/16/2005 | CN1580498A Center-located cutter teeth on shrouded turbine blades |
| 02/16/2005 | CN1189519C Composite wear-resisting material |
| 02/15/2005 | US6855089 Reduced twist carrier |
| 02/15/2005 | US6854738 Sealing structure for combustor liner |
| 02/15/2005 | US6854274 System and method for efficient load following control logic for a turbogenerator operating in stand-alone mode |
| 02/15/2005 | US6854259 Gas turbine installation |
| 02/15/2005 | US6854257 System for injecting fuel into a turbomachine |
| 02/12/2005 | CA2478781A1 Convergent-divergent nozzle for jet turbine engine |
| 02/11/2005 | CA2476215A1 Upgrading aluminide coating on used turbine engine component |
| 02/10/2005 | WO2004110639A3 Water distribution and vaporization assembly |
| 02/10/2005 | WO2004077400A3 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 02/10/2005 | US20050032013 Burner unit and method for operation thereof |
| 02/10/2005 | US20050031781 Aluminizing slurry compositions free of hexavalent chromium, and related methods and articles |
| 02/10/2005 | US20050031482 Such as gas turbine engine components; alloy of at least 50% rhodium, 5% of platinum and/or palladium, and given percent ranges of ruthenium and chromium, less than about 50% by volume of an A3-structured phase; heat and oxidation resistance |
| 02/10/2005 | US20050031451 Microcircuit cooling for a turbine blade |
| 02/10/2005 | US20050031450 Microcircuit airfoil mainbody |
| 02/10/2005 | US20050028533 Method of engine starting in a gas turbine engine |
| 02/10/2005 | US20050028530 Method for operating a turbine group |
| 02/10/2005 | US20050028529 Method of generating energy in a power plant comprising a gas turbine, and power plant for carrying out the method |
| 02/10/2005 | US20050028528 Plug sealing device that is not welded to the chamber wall |
| 02/10/2005 | CA2776661A1 Turbofan case and method of making |
| 02/10/2005 | CA2776404A1 Turbofan case and method of making |
| 02/10/2005 | CA2776341A1 Turbofan case and method of making |
| 02/10/2005 | CA2776318A1 Turbofan case and method of making |
| 02/10/2005 | CA2776317A1 Turbofan case and method of making |
| 02/10/2005 | CA2776316A1 Turbofan case and method of making |
| 02/10/2005 | CA2776254A1 Turbofan case and method of making |
| 02/09/2005 | EP1505278A2 A fluid system |
| 02/09/2005 | EP1505264A1 Low pressure turbine of a turbomachine |
| 02/09/2005 | EP1505261A1 Device to control clearances in a gas turbine |
| 02/09/2005 | EP1505257A2 Gas turbine blade circuit cooling |
| 02/09/2005 | EP1505256A2 Microcircuit cooling for a turbine blade |