| 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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| 09/06/2001 | US20010019696 Gas turbine bucket with impingement cooled platform |
| 09/06/2001 | US20010018960 Directional solidification method and apparatus |
| 09/06/2001 | US20010018824 Method for pressure modulation of turbine sidewall cavities |
| 09/05/2001 | EP1130322A1 Multi-stage multi-plane combustion system for a gas turbine engine |
| 09/05/2001 | EP1130321A1 Combustor liner cooling thimbles and related method |
| 09/05/2001 | EP1130294A2 Surface following brush seal |
| 09/05/2001 | EP1130237A2 Closed circuit cooled turbine blading |
| 09/05/2001 | EP1130219A1 Turbine engine with sealing means between panels |
| 09/05/2001 | EP1129273A2 Gas turbine power generating system including a battery source for supplying startup power |
| 09/05/2001 | EP1129224A1 Device and process for cooling metal components which were subjected to high temperatures |
| 09/05/2001 | EP0820535B1 Erosion/corrosion protective coating for high-temperature components |
| 09/05/2001 | CN1311390A Closed circulation cooling blade turbomachine |
| 09/04/2001 | US6285089 Induction static start for a turbine generator with a brushless exciter and associated methods |
| 09/04/2001 | US6284392 High temperature resistant, creep resistant; for turbines vanes and other turbine components |
| 09/04/2001 | US6284390 Thermal barrier coating system utilizing localized bond coat and article having the same |
| 09/04/2001 | US6283356 Repair of a recess in an article surface |
| 09/04/2001 | US6282885 Gas turbine engine |
| 09/04/2001 | US6282882 Turbine engine control system providing electronic power turbine governor and temperature/torque limiting |
| 09/04/2001 | US6282881 Cooling system for a turbomachine speed reducer |
| 09/04/2001 | US6282786 Method of making injection formed hybrid airfoil |
| 09/03/2001 | WO2001065086A1 Internal combustion rotary turbomotor |
| 08/30/2001 | WO2001062419A1 Clean melt nucleated casting systems and methods with cooling of the casting |
| 08/30/2001 | WO2001062414A1 Device and method for casting a workpiece and workpiece |
| 08/30/2001 | WO2001062372A1 A heat exchanger for cooling and for a pre-cooler for turbine intake air conditioning |
| 08/30/2001 | WO2001045877A8 Multi-wall core and process |
| 08/30/2001 | WO2001023724A3 Integrated bleed air and engine starting system (ibaness) |
| 08/30/2001 | US20010018319 Process for treating the interior of a hollow component |
| 08/30/2001 | US20010018024 Internal cooling circuit for gas turbine bucket |
| 08/30/2001 | US20010017232 Aircraft engine acoustic liner and method of making the same |
| 08/30/2001 | US20010017029 Method and apparatus for compressing gaseous fuel in a turbine engine |
| 08/29/2001 | EP1128158A2 Rotor component displacement measurement system |
| 08/29/2001 | EP1128039A2 Gas turbine |
| 08/29/2001 | EP1128024A2 Gas turbine moving blade |
| 08/29/2001 | EP1128022A2 Rotor windage nut |
| 08/29/2001 | EP1127635A1 Apparatus and method for casting a workpiece and workpiece |
| 08/29/2001 | CN1310785A Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
| 08/29/2001 | CN1310292A Gas turbine |
| 08/28/2001 | US6281596 Automatic turbogenerator restarting method and system |
| 08/28/2001 | US6281595 Microturbine based power generation system and method |
| 08/28/2001 | US6279311 Combined cycle power plant |
| 08/28/2001 | US6279310 Gas turbine starting method using gas and liquid fuels |
| 08/28/2001 | CA2257292C Combined cycle power plant and cooling steam supply method for gas turbine therein |
| 08/23/2001 | WO2001061168A1 Modular gas turbine power plant |
| 08/23/2001 | US20010016163 Gas turbine moving blade |
| 08/23/2001 | US20010016161 Turbocharger |
| 08/23/2001 | US20010015060 Externally fired combined cycle gas turbine system |
| 08/23/2001 | US20010015059 Cooling-air cooler for a gas-turbine plant and use of such a cooling-air cooler |
| 08/23/2001 | DE10029212A1 Mehrstufige Gasturbinenanlage Multi-stage gas turbine plant |
| 08/22/2001 | EP1126137A2 Turbine engine windmilling brake |
| 08/22/2001 | EP1125087A1 Burner assembly |
| 08/22/2001 | EP1125038A1 Isolated oil feed pipe |
| 08/21/2001 | US6276632 Axi-symmetric mixed compression inlet with variable geometry centerbody |
| 08/21/2001 | US6276432 Directional solidification method and apparatus |
| 08/21/2001 | US6276142 Cooled heat shield for gas turbine combustor |
| 08/21/2001 | US6276140 Device to generate energy through a turbo engine |
| 08/21/2001 | US6276123 Two stage expansion and single stage combustion power plant |
| 08/21/2001 | CA2231668C Blade cooling air supplying system of gas turbine |
| 08/21/2001 | CA2070511C Turbine nozzle support |
| 08/16/2001 | WO2001059278A1 Gas turbine intake cooling system and cooling method |
| 08/16/2001 | WO2001059168A1 Iron base high temperature alloy |
| 08/16/2001 | WO2001058622A1 Method and arrangement for producing casting moulds from metal |
| 08/16/2001 | WO2001011103A3 Electron beam physical vapor deposition apparatus and control panel therefor |
| 08/16/2001 | US20010014283 Debris trap in a turbine cooling system |
| 08/16/2001 | EP1144710A3 Electron beam physical vapor deposition apparatus and control panel therefor |
| 08/16/2001 | EP1124047A1 Dual-orifice bypass system for duel-fuel gas turbine |
| 08/16/2001 | EP1123987A1 Repairable diffusion aluminide coatings |
| 08/16/2001 | EP1123726A1 Process and apparatus for the compression of atmospheric air, plant for distilling air and turbine for corresponding gases |
| 08/16/2001 | EP1123457A2 Gas turbine engine |
| 08/16/2001 | EP1123422A1 Electron beam physical vapor deposition apparatus and method |
| 08/16/2001 | DE19962316A1 Bürstendichtung Brush seal |
| 08/15/2001 | CN1308708A Operaitng a gas turbine with supplemental compressed air |
| 08/15/2001 | CN1308100A Composite wear-resisting material |
| 08/15/2001 | CN1069737C Combined-cycle power generation plant |
| 08/14/2001 | US6274945 Combustion control method and system |
| 08/14/2001 | US6274193 Repair of a discrete selective surface of an article |
| 08/14/2001 | US6273676 Method and assembly for masking a flow directing assembly |
| 08/14/2001 | US6273135 Fuel flow control apparatus |
| 08/14/2001 | US6272847 Centrifugal direct injection engine |
| 08/14/2001 | US6272840 Piloted airblast lean direct fuel injector |
| 08/14/2001 | US6272838 Method and apparatus for controlling the inlet duct leading to an auxiliary power unit |
| 08/14/2001 | CA2232128C Cooled platform for a gas turbine moving blade |
| 08/14/2001 | CA2231690C Cooled stationary blade for a gas turbine |
| 08/14/2001 | CA2231495C Gas turbine rotating blade |
| 08/14/2001 | CA2231035C Gas turbine blade |
| 08/09/2001 | WO2001058004A2 Combustion control method and system |
| 08/09/2001 | WO2001057364A1 Frangible cover for turbofan engine blade removal and access |
| 08/09/2001 | WO2001057283A1 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting |
| 08/09/2001 | US20010012568 Thermal barrier coating system utilizing localized bond coat and article having the same |
| 08/09/2001 | US20010011452 Cooling air ducting system in the high pressure turbine section of a gas turbine engine |
| 08/09/2001 | DE10026816A1 Verfahren und Anordnung zum Herstellen vonGußkörpern aus Metall Method and apparatus for producing metal vonGußkörpern |
| 08/09/2001 | DE10003728A1 Hitzeschildanordnung für eine Heißgas führende Komponente, insbesondere für Strukturteile von Gasturbinen A heat shield arrangement for a hot gas-carrying component, in particular for structural parts of gas turbines |
| 08/09/2001 | DE10000418A1 Verdichter eines Abgasturboladers Compressor of an exhaust turbocharger |
| 08/09/2001 | CA2394307A1 Combustion control method and system |
| 08/08/2001 | EP1122879A2 Method and apparatus for controlling rotary machine coupled to a turbo engine |
| 08/08/2001 | EP1122405A2 Gas turbine bucket cooling circuit |
| 08/08/2001 | EP1122329A1 A method of providing a protective coating on a metal substrate, and related articles |
| 08/08/2001 | EP0856095B1 Variable area compensation valve |
| 08/07/2001 | US6270852 Providing superalloy substrate, superalloy material being capable of forming adherent alumina layer; applying bond coat; forming alumina layer; applying ceramic layer on alumina layer |
| 08/07/2001 | US6270311 Gas turbine split ring |
| 08/07/2001 | US6270309 Low drag ducted Ram air turbine generator and cooling system |