| 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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| 03/27/2001 | US6206378 Gas turbine spindle bolt seal device |
| 03/27/2001 | US6206348 Evaporative cooler for a gas turbine engine |
| 03/27/2001 | US6206136 Acoustic liner and method of making an acoustic liner |
| 03/27/2001 | US6206090 Concentric fuel/oil filters and heat exchanger package |
| 03/27/2001 | US6205789 Multi-hole film cooled combuster liner |
| 03/27/2001 | US6205768 Catalytic arrangement for gas turbine combustor |
| 03/27/2001 | US6205766 Fluid flow valve and fluid flow system |
| 03/27/2001 | US6205765 Apparatus and method for active control of oscillations in gas turbine combustors |
| 03/27/2001 | US6205762 Combined cycle power generating plant and method of supplying cooling steam for gas turbine in same |
| 03/22/2001 | WO2001020149A1 Methods of igniting a catalytic converter |
| 03/22/2001 | WO2001020148A2 Variable speed fuel pumping system for a gas turbine and method of operation |
| 03/22/2001 | WO2001019675A2 Supersonic external-compression diffuser and method for designing same |
| 03/22/2001 | US20010000049 Exhaust gas recirculation type combined plant |
| 03/22/2001 | DE19944428A1 Voltage pulse generator for ignition device for gas turbine group e.g. for power generation plant, has mechanical pulses supplied to piezoelement for providing corresponding voltage pulses |
| 03/22/2001 | DE19943782A1 Gas and steam turbine system for generating electricity can be used at normal cost for low/medium power, achieves partic. high efficiency with only average maintenance staff demands |
| 03/21/2001 | EP1085196A1 Hybrid mode-scattering/sound-absorbing segmented liner system and method |
| 03/21/2001 | EP1084372A1 Film cooling strip for gas turbine engine combustion chamber |
| 03/21/2001 | EP1084371A1 Impingement and film cooling for gas turbine combustor walls |
| 03/21/2001 | EP1084337A1 Oil supply system for a gas turbine |
| 03/21/2001 | EP0832396B1 Fuel control system for a staged combustor |
| 03/20/2001 | US6203927 Substrate with ceramic coating on surface and sintering |
| 03/20/2001 | US6203847 Coating of a discrete selective surface of an article |
| 03/20/2001 | US6203274 Steam turbine |
| 03/20/2001 | US6203021 Abradable seal having a cut pattern |
| 03/20/2001 | US6202405 Wall construction for a combustion chamber or a nozzle of a high performance propulsion plant |
| 03/20/2001 | US6202404 Method and apparatus for reducing the temperature of air entering a compressor of a turbojet engine by variably injecting fluid into the incoming air |
| 03/20/2001 | US6202403 Core compartment valve cooling valve scheduling |
| 03/20/2001 | US6202402 Gas-turbine construction |
| 03/20/2001 | US6202400 Gas turbine exhaust recirculation method and apparatus |
| 03/15/2001 | WO2001018372A1 Gas turbine operative at high ambient temperatures |
| 03/15/2001 | DE10041413A1 Operating method for power generating station with gas turbine group with part of generated steam fed into cooling air guide system before or after superheating |
| 03/14/2001 | EP1083301A2 High-efficiency power generating method |
| 03/14/2001 | EP1082530A1 A rotor machine device |
| 03/14/2001 | EP1082529A1 Integral inertial particle separator for radial inlet gas turbine engine |
| 03/14/2001 | EP1082524A1 Fluid deflecting and straining system |
| 03/14/2001 | CN1287596A Retaining arrangement for a bearing, in particular for a high pressure compressor shaft |
| 03/14/2001 | CN1287148A Efficient electric power generation method |
| 03/13/2001 | US6200689 Laser shock peened gas turbine engine seal teeth |
| 03/13/2001 | US6199746 Method for preparing superalloy castings using a metallurgically bonded tapered plug |
| 03/13/2001 | US6199371 Thermally compliant liner |
| 03/13/2001 | US6199368 Coal gasification combined cycle power generation plant and an operating method thereof |
| 03/13/2001 | US6199365 Piezoelectric chemical ignition device |
| 03/13/2001 | US6199363 Method for operating a gas turbogenerator set |
| 03/08/2001 | WO2001016472A1 Manifold drain system for gas turbine |
| 03/08/2001 | WO2001016471A1 Method and device for increasing the pressure of a gas |
| 03/08/2001 | WO2001015866A1 Method and device for treating the surface of a part |
| 03/08/2001 | CA2383082A1 Method and device for the surface threatment of a component |
| 03/07/2001 | EP1081335A2 Stator assembly for a rotary machine and method for making the stator assembly |
| 03/07/2001 | EP1081239A1 Method for setting up and controlling confinement media flow in laser shock peening |
| 03/07/2001 | EP1080300A1 Recuperator for gas turbine engine |
| 03/06/2001 | US6198174 Microturbine power generating system |
| 03/06/2001 | US6197424 Dimensionally stable ceramic insulation composition of hollow oxide-based spheres; a phosphate binder; an oxide filler powder, where the binder fills gaps between spheres and the powder, each sphere in contact with other spheres |
| 03/06/2001 | US6196798 Gas turbine cooling blade |
| 03/06/2001 | US6196795 Turbine pack and method for adapting a turbine pack |
| 03/06/2001 | US6196791 Gas turbine cooling moving blades |
| 03/06/2001 | US6196790 Seal assembly for an intershaft seal in a gas turbine engine |
| 03/06/2001 | US6195979 Cooling apparatus for gas turbine moving blade and gas turbine equipped with same |
| 03/06/2001 | US6195978 Ecology system for a gas turbine engine |
| 03/06/2001 | US6195891 Method for identification and repair of indications in hardware |
| 03/01/2001 | WO2000031394A3 An engine |
| 03/01/2001 | DE19940575A1 Gas turbine arrangement for energy generation has heat exchanger to receive expanded hot gases and transfer waste heat to isothermally compressed air |
| 02/28/2001 | EP1079076A2 Shroud assembly having c-clip retainer |
| 02/28/2001 | EP1079069A2 Steam cooling system for a gas turbine |
| 02/28/2001 | EP1079068A2 Connector tube for a turbine rotor cooling circuit |
| 02/28/2001 | EP1079067A2 A cooling air supply system for a rotor |
| 02/28/2001 | EP1078204A1 A device for the supply of a liquid fuel to a burner member |
| 02/28/2001 | CN1285894A Device for producing energy by means of a turbo-machine |
| 02/27/2001 | US6195607 Method and apparatus for optimizing NOx emissions in a gas turbine |
| 02/27/2001 | US6195247 Exciter controlled by FADEC system |
| 02/27/2001 | US6194086 Nickel and cobalt superalloy substrate; low pressure plasma spraying of abrasives |
| 02/27/2001 | US6193465 Trapped insert turbine airfoil |
| 02/27/2001 | US6193192 Deicing device for a jet engine air inlet cowl |
| 02/27/2001 | US6192668 Method and apparatus for compressing gaseous fuel in a turbine engine |
| 02/22/2001 | WO2001013184A1 Fuzzy logic based fuel flow selection system |
| 02/22/2001 | WO2001012968A1 Fuel control valve |
| 02/22/2001 | WO2001012506A1 Protection device for the air inlet of aircraft turbines |
| 02/22/2001 | WO2001012381A1 Laser cladding a turbine engine vane platform |
| 02/22/2001 | WO2000055036A3 Tangentially directed acoustic jet controlling boundary layers |
| 02/22/2001 | WO2000038985A3 Low drag ducted ram air turbine generator and cooling system |
| 02/21/2001 | EP1077361A2 Methods and apparatus for measuring airfoil coordinates |
| 02/21/2001 | EP1077349A1 Fuel staging apparatus and methods for gas turbine nozzles |
| 02/21/2001 | EP1077338A2 Turbine brush seal protection device and method |
| 02/21/2001 | EP1077126A1 Injection formed hydrid airfoil |
| 02/21/2001 | EP1076761A1 Gas and steam turbine installation |
| 02/20/2001 | US6190128 Cooled moving blade for gas turbine |
| 02/20/2001 | US6190127 Tuning thermal mismatch between turbine rotor parts with a thermal medium |
| 02/20/2001 | US6190124 Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
| 02/20/2001 | US6190120 Partially turbulated trailing edge cooling passages for gas turbine nozzles |
| 02/20/2001 | US6189891 Gas turbine seal apparatus |
| 02/20/2001 | US6189814 Gas turbine engine combustion chamber |
| 02/20/2001 | US6189321 Distributor |
| 02/20/2001 | US6189313 Aircraft engine fuel system mounting assembly |
| 02/20/2001 | US6189311 Gas turbine engine |
| 02/20/2001 | CA2207033C Gas turbine engine feather seal arrangement |
| 02/15/2001 | WO2001011108A1 Electron beam physical vapor deposition apparatus and method |
| 02/15/2001 | WO2001011103A2 Electron beam physical vapor deposition apparatus and control panel therefor |
| 02/15/2001 | WO2001010536A1 Powered low restriction air precleaner device and method for providing a clean air flow to an apparatus such as a combustion engine air intake, engine cooling system, ventilation system and cab air intake system |
| 02/15/2001 | DE19936655A1 Gas turbine unit for combination power plant; has turbine and combustion chamber using first fuel, and preheating devices including condensing boil supplied with second fuel |
| 02/14/2001 | EP1076159A2 Stator vane blank and method of forming the vane blank |
| 02/14/2001 | CN1062054C Process for cleaning gas turbine inlet air, its appts and gas turbine |