| 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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| 04/03/2002 | EP1193235A2 A heat-resisting fiber-reinforced composite material and manufacturing method thereof |
| 04/03/2002 | EP1192334A1 Fuel and oil system for a gas turbine |
| 04/03/2002 | EP1154876A4 Repair of turbine exhaust case |
| 04/03/2002 | EP0852659B1 Sealing element for sealing a gap and gas turbine facility |
| 04/03/2002 | CN1082004C Three link engine mount with fault automatic protecting device |
| 04/02/2002 | US6365236 Alternating the temperature during electron beam vapor deposition, layers are applied at different temperature conditions for different porosities |
| 04/02/2002 | US6364805 Planetary gear |
| 04/02/2002 | US6364603 Fan case for turbofan engine having a fan decoupler |
| 04/02/2002 | US6364602 Method of air-flow measurement and active operating limit line management for compressor surge avoidance |
| 04/02/2002 | US6364249 Engine integrated with rotary wing aircraft transmission |
| 04/02/2002 | US6363724 Gas only nozzle fuel tip |
| 04/02/2002 | US6363710 Gas and steam-turbine plant |
| 04/02/2002 | US6363709 Exhaust gas recirculation type combined plant |
| 04/02/2002 | US6363707 Method for supplying lift and hydraulic fluid for a gas turbine |
| 04/02/2002 | US6363706 Apparatus and method to increase turbine power |
| 04/02/2002 | CA2247491C Steam cooled gas turbine rotor |
| 03/28/2002 | WO2002026004A1 Device for producing a plasma, ionisation method, use of said method and production processes using said device |
| 03/28/2002 | WO2002025084A1 Method for reducing rotor/stator interaction noise in a turbo-machine and device therefor |
| 03/28/2002 | WO2002025083A1 Two stage expansion and single stage combustion compressed air storage power plant |
| 03/28/2002 | WO2002025066A1 Steam-type gas turbine subassembly and method for enhancing turbine performance |
| 03/28/2002 | US20020037692 Clogging-free drain system installed in a cutting apparatus |
| 03/28/2002 | US20020037220 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby |
| 03/28/2002 | US20020037217 Cooling circuit for steam and air-cooled turbine nozzle stage |
| 03/28/2002 | US20020036115 Noise attenuation panel |
| 03/27/2002 | EP1191674A2 A microturbine based power generation system and method |
| 03/27/2002 | EP1191214A2 Exhaust nozzle with stub airfoils |
| 03/27/2002 | EP1191207A2 A starting system and method for a microturbine power generation unit |
| 03/27/2002 | EP1191206A2 Interstage cooling system of a multi-compressor turbocharger, engine and turbocharger comprising such a cooling system, and method of operating the turbocharger |
| 03/27/2002 | EP1191205A1 Procedure for noise reduction for a turbo machine using a Phase shift/Phase superposition and method for execution of this procedure |
| 03/27/2002 | EP1191204A2 A co-generation system and a dehumidification air-conditioner |
| 03/27/2002 | EP1191125A1 Method for making a thermal barrier coating |
| 03/27/2002 | EP1190200A1 Fuel injector heat shield |
| 03/26/2002 | US6361273 Heat shield for a gas turbine |
| 03/26/2002 | US6360844 Aircraft engine acoustic liner and method of making the same |
| 03/26/2002 | US6360524 Oxygen separator designed to be integrated with a gas turbine and method of separating oxygen |
| 03/21/2002 | WO2002023027A1 Water supply system for steam injection and inlet fogging in a gas turbine powerplant and operating method for this system |
| 03/21/2002 | WO2002022291A1 Device and method for producing a blade for a turbine and blade produced according to this method |
| 03/21/2002 | WO2001083297A3 Aircraft gas turbine engine having a centrifuge |
| 03/21/2002 | WO2001069064B1 Cast heat exchanger system |
| 03/21/2002 | DE10052893A1 Arrangement for improving efficiency of flow machines, preferably in motor vehicles, has flow control body whose inlet and outlet sections have protruding, increased flow cross-sections |
| 03/20/2002 | EP1188901A2 Bypass holes for rotor cooling |
| 03/20/2002 | EP1188900A2 Balancing method for a blisk |
| 03/20/2002 | EP1188500A1 Apparatus and method for producing a turbine blade and turbine blade |
| 03/20/2002 | EP0984839B1 Metal-ceramic graded-index material, product produced from said material, and method for producing the material |
| 03/20/2002 | CN1341192A Internal combustion rotary turbomotor |
| 03/20/2002 | CN1340576A Anti-oxidation coat, its correlated product and method |
| 03/20/2002 | CN1340401A Self-cleaning soldering material |
| 03/20/2002 | CN1081289C Stationary blade for gas turbine |
| 03/19/2002 | US6358590 Noise attenuation panel |
| 03/19/2002 | US6358014 Composite spinner and method of making the same |
| 03/19/2002 | US6357236 Gas turbine, combined cycle plant and compressor |
| 03/19/2002 | US6357222 Method and apparatus for reducing thermal stresses within turbine engines |
| 03/19/2002 | US6357220 Gearbox accessory mount |
| 03/19/2002 | US6357219 Turbine engine fuel control system |
| 03/19/2002 | US6357217 Endothermic cooling of guide vanes and/or moving blades in a gas turbine |
| 03/14/2002 | WO2002021027A1 Heat-resistance magnetic silicone rubber body for brush seals in turbomachinery and methods of application |
| 03/14/2002 | WO2002020949A1 Turbo-machine and turbine blade |
| 03/14/2002 | WO2002020349A1 Two piece spinner |
| 03/14/2002 | WO2002020134A2 Methods for filtering air for a gas turbine system |
| 03/14/2002 | WO2001071176A3 Method and system for generating power |
| 03/14/2002 | US20020031427 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor |
| 03/14/2002 | US20020029559 Gas turbine system |
| 03/14/2002 | DE10042933A1 Vorrichtung zum Kühlen des Gehäuses einer Fluggasturbine Device for the cooling of the housing of an aircraft gas turbine |
| 03/13/2002 | EP1186832A2 Fuel nozzle assembly for reduced exhaust emissions |
| 03/13/2002 | EP1186761A2 Energy recovery from compressor discharge bleed air in gas turbine plants |
| 03/13/2002 | EP1186749A1 Turbomachine and turbine blade |
| 03/13/2002 | EP1185766A1 Concentricity ring |
| 03/13/2002 | EP1185765A1 Apparatus for reducing combustor exit duct cooling |
| 03/13/2002 | EP1185764A1 Device for controlling air flow in a turbine blade |
| 03/13/2002 | EP1135540B1 Method and device for cleaning a product |
| 03/12/2002 | US6355356 Coating system for providing environmental protection to a metal substrate, and related processes |
| 03/12/2002 | US6355116 Method for renewing diffusion coatings on superalloy substrates |
| 03/12/2002 | US6354799 Superalloy weld composition and repaired turbine engine component |
| 03/12/2002 | US6354780 Eccentric balanced blisk |
| 03/12/2002 | US6354073 Combined cycle electric power plant |
| 03/07/2002 | WO2002018674A2 Thermal barrier coating system for turbine components |
| 03/07/2002 | WO2002003024A8 Play measuring sensor by multiple depth abrasion |
| 03/07/2002 | WO2001054981A3 Propulsion module |
| 03/07/2002 | US20020028141 Apparatus and methods for balancing turbine rotors |
| 03/07/2002 | US20020028140 Cooling circuit for and method of cooling a gas turbine bucket |
| 03/07/2002 | US20020028135 Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment |
| 03/07/2002 | US20020028134 Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment |
| 03/07/2002 | US20020027213 Extended range proportional valve method |
| 03/07/2002 | US20020026796 Method for increasing the fluid-mechanical stability of a premix burner as well as a premix burner for performing the method |
| 03/07/2002 | US20020026786 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 03/07/2002 | US20020026785 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 03/07/2002 | US20020026784 Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system and fuel nozzle wash system |
| 03/07/2002 | US20020026783 Gas turbine, combined cycle plant and compressor |
| 03/07/2002 | DE10040869A1 Verfahren und Vorrichtung zur Unterdrückung von Strömungswirbeln innerhalb einer Strömungskraftmaschine Method and apparatus for suppressing flow vortices within a turbomachine |
| 03/07/2002 | DE10033653A1 Drive system for e.g. aircraft, is formed multistage with drives units such that the drive system is combined with at least one negative pressure system |
| 03/06/2002 | EP1184623A2 Liquid fuel and water injection purge system and method for a gas turbine |
| 03/06/2002 | EP1184621A1 Gas only nozzle fuel tip and method for cooling the same |
| 03/06/2002 | EP1184552A2 Cooling device for a gas turbine casing |
| 03/06/2002 | EP1184541A1 Combined cycle power plant |
| 03/06/2002 | EP1184479A1 Method of forming a reactive-element containing aluminide on a metallic substrate |
| 03/06/2002 | EP1184475A2 Oxidation-resistant coatings, and related articles and processes |
| 03/06/2002 | EP1184129A2 Self cleaning braze material |
| 03/06/2002 | EP1183444A1 Turbomachine and sealing element for a rotor thereof |
| 03/06/2002 | EP1183442A1 Cast on-board injection nozzle with adjustable flow area |
| 03/06/2002 | EP1183088A1 Concentric fuel/oil filters and heat exchanger package |