| 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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| 02/27/2007 | US7181916 Method for operating a reduced center burner in multi-burner combustor |
| 02/27/2007 | US7181915 High temperature centerbody for temperature reduction by optical reflection and process for manufacturing |
| 02/27/2007 | CA2399551C Rotor coupling having insulated structure |
| 02/26/2007 | CA2557104A1 Process for assembling a turbine engine |
| 02/26/2007 | CA2557073A1 Device for heating a cylindrical part, to be used in the assembly of an inter-shaft bearing in a turbine engine |
| 02/22/2007 | WO2007019713A1 Compressor compressor wheel cleaning attachment and exhaust turbocharger |
| 02/22/2007 | WO2006120168A3 Fuel supply for a gas turbine, comprising a deviation zone |
| 02/22/2007 | US20070039331 Modular gas turbine |
| 02/22/2007 | US20070039330 Air thrust bearing for a gas turbine engine |
| 02/22/2007 | US20070039329 System and method for attenuating combustion oscillations in a gas turbine engine |
| 02/22/2007 | US20070039327 Monobloc flameholder arm for an afterburner device of a bypass turbojet |
| 02/22/2007 | US20070039326 Fuel injection method and apparatus for a combustor |
| 02/22/2007 | US20070039309 Stiffener for low pressure compressor for an aircraft engine |
| 02/22/2007 | US20070039307 Gas turbine installation |
| 02/22/2007 | US20070039305 Lubricating Oil Heat Recovery System for Turbine Engines |
| 02/21/2007 | EP1754863A2 Lubricating oil heat recovery system for turbine engines |
| 02/21/2007 | EP1754862A1 Compressor, compressor wheel, washing attachment and exhaust turbocharger |
| 02/21/2007 | EP1753938A1 A support structure in a turbine or compressor device and a method for assembling the structure |
| 02/21/2007 | EP1337741B1 A turbine arrangement and a method of operating a turbine arrangement |
| 02/21/2007 | CN1918375A Gas turbine plant |
| 02/21/2007 | CN1918373A Radial turbine and method of cooling nozzle of the same |
| 02/21/2007 | CN1916386A Multi-spool by-pass turbofan engine |
| 02/21/2007 | CN1916384A Lubricating oil heat recovery system for turbine engines |
| 02/20/2007 | US7179507 Thermally spraying formulation comprising solid lubricant and a ceramic and a matrix-forming metal or metal alloy, wherein solid lubricant is hexagonal boron nitride, wherein matrix-forming metal or metal alloy is Cu, Al or an alloy of Cu, Al, CuAl or AlSi, ceramic is selected from albite, illite, quartz |
| 02/20/2007 | US7179320 Air recharge system dryer and methods therefor |
| 02/20/2007 | US7178348 Refrigeration power plant |
| 02/20/2007 | US7178341 Multi-zone tubing assembly for a transition piece of a gas turbine |
| 02/20/2007 | US7178340 Transition duct honeycomb seal |
| 02/20/2007 | US7178335 Pressure regulator |
| 02/20/2007 | US7178325 Divergent flap for a gas turbine engine |
| 02/20/2007 | CA2417370C Stationary blade in gas turbine and gas turbine comprising the same |
| 02/20/2007 | CA2363302C Shot-peening of cooled blade tops |
| 02/15/2007 | WO2007017498A1 Method for the aerodynamic design of a compressor of a turbine engine |
| 02/15/2007 | WO2007017486A1 Method for operating a gas turbine, and gas turbine for carrying out the method |
| 02/15/2007 | WO2007017317A1 Sound absorber for gas turbine installations |
| 02/15/2007 | WO2006014614A3 Control treatment for gas turbine in material treatment unit |
| 02/15/2007 | US20070036703 Configuration and process for carbonyl removal |
| 02/15/2007 | US20070033945 Gas turbine system and method of operation |
| 02/15/2007 | US20070033919 Gas turbine combustor |
| 02/15/2007 | DE19847150B4 Trägerkonstruktion für wärmeisolierendes und/oder schallabsorbierendes Material und Schalldämpferkulissenelement unter Verwendung derselben Support structure for heat insulating and / or sound-absorbing material and sound-damping element using the same |
| 02/15/2007 | CA2618007A1 A method for operating a gas turbine and a gas turbine for implementing the method |
| 02/14/2007 | EP1752637A2 Architecture for an acoustic liner |
| 02/14/2007 | EP1752619A2 Turbo group with starting device |
| 02/14/2007 | EP1752618A2 Steam cooled system in combined cycle power plant |
| 02/14/2007 | EP1751401A2 Heat shield for gas turbine engine |
| 02/14/2007 | EP1537248B1 Producing metallic articles by reduction of nonmetallic precursor compounds and melting |
| 02/14/2007 | CN1912368A Fuel pre-evaporation and premix perforated pipe |
| 02/14/2007 | CN1912351A Rotation jet engine |
| 02/13/2007 | US7175693 Method for preventing fuel infiltration into microporous polymer membranes |
| 02/13/2007 | US7175385 Mounting of the rotor of a gas turbine |
| 02/13/2007 | US7175342 Shaft-misalignment-measuring device, a shaft-misalignment-measuring method, a single-shaft combined plant using the shaft-misalignment-measuring device and a start-up method of the single-shaft combined plant |
| 02/13/2007 | US7174997 Failure tolerant passive lubrication system |
| 02/13/2007 | US7174945 Refractory metal core wall thickness control |
| 02/13/2007 | US7174719 Gas turbine engine with seal assembly |
| 02/13/2007 | CA2274526C Abradable seal |
| 02/09/2007 | CA2525643A1 Transition piece for gas turbine |
| 02/08/2007 | WO2007016086A1 Engine intake sealing system |
| 02/08/2007 | WO2007016085A1 Control of engine intake door |
| 02/08/2007 | WO2007015847A2 Turbine engine with interstage heat transfer |
| 02/08/2007 | US20070028622 One-piece baffle infrared suppressor apparatus and method |
| 02/08/2007 | US20070028619 Fuel injector |
| 02/08/2007 | US20070028590 Sealing system for the rear lubricating chamber of a jet engine |
| 02/08/2007 | US20070028589 Thermal management system for a gas turbine engine |
| 02/08/2007 | US20070028588 Heat transfer apparatus and systems including the apparatus |
| 02/08/2007 | DE102005047739B3 Substrate with matrix layer for turbine systems and production process has multilayer of and or encapsulated nanoparticles that release a colored material above a threshold temperature |
| 02/07/2007 | EP1749995A2 Multi spool gas turbine system |
| 02/07/2007 | EP1749994A2 Method and apparatus for adding a secondary fluid flow to a gas turbine engine fuel line |
| 02/07/2007 | EP1749993A2 Auxiliary power unit intake duct with aero-acoustic guide vanes |
| 02/07/2007 | EP1749979A2 Movement system for the inspection of a gas turbine and gas turbine equipped with such a system |
| 02/07/2007 | CN2866857Y Gas-turbogenerator controlling device |
| 02/07/2007 | CN2866856Y Gas turbine gas nozzle device |
| 02/07/2007 | CN1910307A Alloy coating for diffusion barrier, method for forming same, and high-temperature device member |
| 02/07/2007 | CN1908405A Inlet guide vane control device of gas turbine |
| 02/07/2007 | CN1298978C Cooling system for gas turbine |
| 02/06/2007 | US7172787 Multilayer element of Nickel alloy, spraying and removing layer by peeling |
| 02/06/2007 | US7171870 Geared fluid drive with parallel start-up capability |
| 02/06/2007 | CA2327817C Inter-stage seal retainer and assembly |
| 02/06/2007 | CA2288557C Gas turbine combustor cooling structure |
| 02/02/2007 | CA2554933A1 Sealing system for the rear lubrication chamber of a turbojet |
| 02/01/2007 | WO2008041964A2 Infrared suppression system |
| 02/01/2007 | WO2007012722A1 Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit |
| 02/01/2007 | US20070025847 Gas turbine |
| 02/01/2007 | US20070023157 Apparatus and method for reducing operating stress in a turbine blade and the like |
| 02/01/2007 | US20070022758 Reverse-flow gas turbine combustion system |
| 02/01/2007 | US20070022757 Infrared suppression system |
| 02/01/2007 | US20070022739 Methods and apparatus for operating gas turbine engines |
| 02/01/2007 | US20070022736 Igniter for internal combustion engines operating over a wide range of air fuel ratios |
| 02/01/2007 | US20070022735 Pto assembly for a gas turbine engine |
| 02/01/2007 | US20070022734 Gas turbine, combined cycle plant and compressor |
| 02/01/2007 | US20070022733 Electric power supply equipment |
| 02/01/2007 | US20070022732 Methods and apparatus for operating gas turbine engines |
| 02/01/2007 | US20070022731 Compact, light weight eductor oil cooler plenum and surge flow plenum design |
| 02/01/2007 | DE19617916B4 Verdampfer zum Verdampfen eines tiefkalten flüssigen Mediums Evaporator for evaporating a cryogenic liquid medium |
| 02/01/2007 | CA2615273A1 Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit |
| 01/31/2007 | EP1748170A2 PTO assembly for a gas turbine engine, gas turbine engine and method of operation of a gas turbine engine |
| 01/31/2007 | EP1748169A1 Fixation of a seal arrangement on a rotor of a turbomachine |
| 01/31/2007 | EP1747054A1 A fluid separation device |
| 01/31/2007 | CN1904327A Gas turbine controller |
| 01/31/2007 | CN1904326A Gas turbine controller |
| 01/31/2007 | CN1904325A PTO device for a gas turbine engine |