| 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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| 12/08/2004 | EP1484102A2 Method and apparatus to generate power in a gas turbine powerplant |
| 12/08/2004 | EP1483492A1 Method for igniting the combustion chamber of a gas turbine installation and an ignition device for carrying out said method |
| 12/08/2004 | EP1483491A1 Apparatus and method for cooling combustion turbine inlet air using liquid hydrocarbon fuel vaporisation |
| 12/08/2004 | EP1407193B1 Coolable segment for a turbomachinery and combustion turbine |
| 12/08/2004 | EP1173664B1 Cooling air system |
| 12/08/2004 | EP0927814B1 Tip shroud for cooled blade of gas turbine |
| 12/08/2004 | CN1553989A Gas turbine state diagnostic method and system |
| 12/07/2004 | US6827548 Rotor assemblies for gas turbine engines |
| 12/07/2004 | US6827180 Noise attenuation panel |
| 12/07/2004 | CA2284490C Combined cycle power plant |
| 12/02/2004 | WO2004104392A2 Air turbine starter with angular contact thrust bearing |
| 12/02/2004 | US20040240988 Turbofan jet engine having a turbine case cooling valve |
| 12/02/2004 | US20040240985 Gas turbine engine |
| 12/02/2004 | US20040238687 Aeroengine nacelle |
| 12/02/2004 | US20040237948 Fuel vaporization systems for vaporizing liquid fuel |
| 12/02/2004 | US20040237540 Co-generation system and a dehumidification air-conditioner |
| 12/02/2004 | US20040237538 Gas turbine apparatus and a starting method thereof |
| 12/02/2004 | US20040237537 Gas turbine apparatus |
| 12/02/2004 | US20040237535 Method of operating a gas turbine |
| 12/02/2004 | US20040237534 Engine nozzle |
| 12/02/2004 | US20040237531 Combustor of gas turbine |
| 12/02/2004 | US20040237503 Rotor inlet temperature control for turbo machine |
| 12/02/2004 | US20040237502 Assembly and method for aircraft engine noise reduction |
| 12/02/2004 | US20040237500 Combustion chamber arrangement |
| 12/02/2004 | DE10321572A1 Supercharging air compressor for internal combustion engine separates sub-stream of compressed air downstream of compressor wheel and passes via temperature reduction unit to produce cooling air |
| 12/02/2004 | DE10312971A1 Gas turbine assembly especially for a power unit has cooling component between two combustion chambers in the gas turbine |
| 12/01/2004 | EP1482478A2 Assembly and method for aircraft engine noise reduction |
| 12/01/2004 | EP1482159A2 Engine nozzle and engine with such a nozzle |
| 12/01/2004 | EP1482158A1 Movable exhaust nozzle flap of a turbomachine with extended durability |
| 12/01/2004 | EP1482150A2 Method and system of synthesizing turbine inlet temperature of a turbo machine |
| 12/01/2004 | EP1482127A1 Sealing system for the bypass flow at the inlet of the afterburner nozzle of a turbomachine |
| 12/01/2004 | EP1481895A1 Rear suspension device for an aircraft engine |
| 12/01/2004 | EP1481756A1 Method of fabricating a hollow turbine blade |
| 12/01/2004 | EP1481755A1 Method for manufacturing a hollow blade for turbomachine |
| 12/01/2004 | EP1480770A2 Method and device for producing precision investment-cast ne metal alloy members and ne metal alloys for carrying out said method |
| 12/01/2004 | EP1409862B1 Gas turbine |
| 12/01/2004 | EP1105622B1 Mismatch proof variable stator vane |
| 12/01/2004 | EP1053434B1 Fuel air mixer for a radial dome in a gas turbine engine combustor |
| 12/01/2004 | CN1551946A Method for controlling temperature of combustion turbine inlet fuel in order to achieve maximum power output |
| 12/01/2004 | CN1550716A Outer and inner cowl-wire wrap to one piece cowl conversion |
| 12/01/2004 | CN1550714A Differential pressure induced purging fuel injector with asymmetric cyclone |
| 12/01/2004 | CN1550650A Microcircuit cooling for a turbine blade tip |
| 12/01/2004 | CN1550643A Method and apparatus to facilitate sealing within turbines |
| 12/01/2004 | CN1550561A Nickel-base alloy |
| 12/01/2004 | CN1550252A Planar membrane deoxygenator |
| 11/30/2004 | US6824575 Integrated coal gasification combined cycle power generator |
| 11/30/2004 | US6824359 Turbine blade |
| 11/30/2004 | US6824356 Foreign material exclusion device |
| 11/30/2004 | US6824351 Method and device for cooling the inflow area of the shaft of a steam turbine |
| 11/30/2004 | US6823674 Method for operating a gas and stream turbine installation and corresponding installation |
| 11/30/2004 | CA2468559A1 Rotor inlet temperature control for turbo machine |
| 11/27/2004 | CA2469853A1 Secondary flow sealing system at the entrance of a turbomachine nozzle with post-combustion chamber |
| 11/25/2004 | WO2004101975A1 Device for damping sound in a duct |
| 11/25/2004 | US20040234808 Mcraly-coating |
| 11/25/2004 | US20040234784 Bond coat for silicon based substrates |
| 11/25/2004 | US20040234782 Refractory oxide bonding layer comprise chromium, tantalum, niobium, silicon, platinum, hafnium, yttrium, aluminum, zirconium, titanium, rare earth metals, alkaline earth metals and mixtures; combustion chambers, gas turbine engines; heat and oxidation resistance, noncracking |
| 11/25/2004 | US20040234740 having a dispersion of fibers, at least some of which extend between the bond layer and the further layer; improved fracture toughness of each layer and improved overall strength and toughness of the system at the boundary between the layers. |
| 11/25/2004 | US20040234369 Air turbine starter with angular contact thrust bearing |
| 11/25/2004 | US20040231337 Gas turbine |
| 11/25/2004 | US20040231334 Gas turbine |
| 11/25/2004 | DE102004022162A1 Verfahren und Vorrichtung zur Vereinfachung von Abdichtungen innerhalb Turbinen Method and apparatus for simplification of seals within turbines |
| 11/24/2004 | EP1480311A2 Electric motor or generator |
| 11/24/2004 | EP1479975A1 Combustion chamber having a flexible joint between a chamber base and a chamber wall |
| 11/24/2004 | EP1479889A2 Gas turbine engine and intake for a gas turbine engine with a device to prevent ice forming |
| 11/24/2004 | EP1479873A2 Steam turbine |
| 11/24/2004 | EP1479660A2 Coating for silicon containing substrate |
| 11/24/2004 | EP1479658A2 Bond layer for silicon based substrates |
| 11/24/2004 | EP1479656A2 Bond coat for silicon based substrates |
| 11/24/2004 | EP1478836A1 Electric thrust reverser actuation system |
| 11/24/2004 | EP1478833A1 A rotary internal combustion engine |
| 11/24/2004 | EP1478827A1 Method and apparatus for increasing welding rates for high aspect ratio welds |
| 11/24/2004 | EP1381481A4 Multi-wall core and process |
| 11/24/2004 | CN1549887A Gas turbine stator housing |
| 11/24/2004 | CN1176781C Self-cleaning soldering material |
| 11/23/2004 | US6821086 Turbomachine seal assembly and method therefor |
| 11/23/2004 | US6821084 Torque tube bearing assembly |
| 11/23/2004 | US6820430 Method and apparatus for providing evaporative cooling and power augmentation in gas turbines |
| 11/23/2004 | US6820429 Adaptive acceleration schedules for gas turbine engine control systems |
| 11/23/2004 | US6820337 Process for making a panel with a protected acoustic damping layer and acoustic panel as made |
| 11/23/2004 | CA2312323C Planetary gear |
| 11/23/2004 | CA2211424C Combined bowl-deflector for combustion chamber of turbine engine |
| 11/20/2004 | CA2469849A1 Combustion chamber having a flexible liaison between the chamber floor and chamber wall |
| 11/18/2004 | US20040226443 Methods for filtering air for a gas turbine system |
| 11/18/2004 | US20040226333 Method of manufacturing elliptic deep-drawn products |
| 11/18/2004 | US20040226297 Burner for synthesis gas |
| 11/18/2004 | DE102004019837A1 Nickelbasis-Superlegierung und Einkristall-Gussstücke Nickel-base superalloy and single crystal castings |
| 11/17/2004 | EP1477741A1 Outer and inner cowl-wire wrap to one piece cowl conversion |
| 11/17/2004 | EP1476649A1 Ejector based engines |
| 11/17/2004 | EP1198665B1 Fuel divider and ecology system for a gas turbine engine |
| 11/17/2004 | CN1176321C Method and device for controlling fuel ratio in gas turbine burner |
| 11/16/2004 | US6818321 A substrate of nickel-based single crystal alloy or a nickel-based unidirectional solidified alloy and a coating of an alloy of boron sprayed or vapor deposited on the surface; gas turbine blades; jet engines; shields |
| 11/16/2004 | US6818252 Method of reducing corrosion in gas turbine engines |
| 11/16/2004 | US6818077 Comprised of at least chromium, cobalt, aluminum, niobium, carbon and boron with titanium, tantalum and/or molybdenum; high temperature creep rupture strength; oxidation and corrosion resistance |
| 11/16/2004 | US6817572 Air intake system of a propeller-turbine engine |
| 11/16/2004 | US6817190 Blade cooling in a gas turbine engine |
| 11/16/2004 | US6817189 Arrangement for the cooling of the casing of an aircraft gas turbine engine |
| 11/16/2004 | US6817187 Re-fired gas turbine engine |
| 11/16/2004 | US6817186 Operation control apparatus and operation control method for single-shaft combined plant |
| 11/16/2004 | US6817183 Liquid fuel injector for burners of gas turbines |
| 11/11/2004 | US20040223868 Nickel-base alloy |