| 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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| 03/06/2002 | EP0868372B1 Jet aircraft engine transport apparatus |
| 03/06/2002 | CN1080142C Two stream tangential entry nozzle |
| 03/05/2002 | US6352577 Microchannel laminated mass exchanger and method of making |
| 03/05/2002 | US6351940 Inverter ducting for dual fan concept |
| 03/05/2002 | US6351937 Gas turbine plant |
| 03/05/2002 | CA2270672C Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system, and fuel nozzle wash system |
| 02/28/2002 | WO2002016743A1 Integrated thermal management and coolant system for an aircraft |
| 02/28/2002 | WO2001087528A3 Welding superalloy articles |
| 02/28/2002 | US20020025250 Connector tube for a turbine rotor cooling circuit |
| 02/28/2002 | US20020025248 Method for enhancing heat transfer inside a turbulated cooling passage |
| 02/28/2002 | US20020023696 Formation of an aluminide coating, incorporating a reactive element, on a metal substrate |
| 02/28/2002 | US20020023425 Method and apparatus for the rapid startup and rapid increase in output of a gas turbine plant |
| 02/28/2002 | US20020023424 Gas turbine generator plant |
| 02/28/2002 | DE10039246A1 Verfahren zur Umwandlung von thermischer Energie in mechanische Arbeit A method for converting thermal energy into mechanical work |
| 02/27/2002 | EP1182401A1 Method and apparatus for decreasing combustor emissions |
| 02/27/2002 | EP1182398A1 Process for increasing the fluidic stability of a premix-burner as well as premix-burner for carrying out said process |
| 02/27/2002 | EP1182339A2 Clocked turbine airfoil cooling |
| 02/27/2002 | EP1181520A1 Inspection device for an annular combustion chamber of a gas turbine and method of inspecting an annular combustion chamber of a gas turbine |
| 02/27/2002 | CN1079895C Wet purification method and device of spray nozzle ring of exhaust steam turbocharger-pulley machine |
| 02/26/2002 | US6351090 Device for starting a gas turbine in an aircraft |
| 02/26/2002 | US6350103 Jet engine booster structure |
| 02/26/2002 | US6349537 Vehicle main and auxiliary power units |
| 02/26/2002 | US6349536 Multifunctional water injection manifold device and operation method thereof |
| 02/26/2002 | CA2170875C Interactive laser welding at elevated temperatures of superalloy articles |
| 02/21/2002 | WO2002014695A1 Method and system of pulsed or unsteady ejector |
| 02/21/2002 | WO2002014664A1 Gas turbine engine having improved efficiency |
| 02/21/2002 | WO2002014663A1 Method for converting thermal energy into mechanical work |
| 02/21/2002 | WO2002014654A1 Turbine vane system |
| 02/21/2002 | US20020020295 Centrifugally ejecting heavier-than-air particles within air precleaner; pollution control |
| 02/21/2002 | US20020020168 Turbojet power plant with heat exchanger |
| 02/20/2002 | EP1180578A1 Statoric blades for a turbomachine |
| 02/20/2002 | EP1180577A2 Cooling method for a turbine rotor |
| 02/20/2002 | EP1180208A1 A thermodynamic apparatus |
| 02/20/2002 | EP1180197A1 Sealing system for a rotor of a turbo engine |
| 02/20/2002 | EP1180196A1 Turbo-machine comprising a sealing system for a rotor |
| 02/20/2002 | EP0981681B1 Gas and steam turbine system, and refrigeration of the coolant intended for the gas turbine in such a system |
| 02/20/2002 | CN1336265A Metal object having under-pressure and single-end belt, and its mfg. method |
| 02/19/2002 | US6348085 Filter arrangement and methods |
| 02/19/2002 | US6347660 Multipiece core assembly for cast airfoil |
| 02/19/2002 | US6347508 Combustor liner support and seal assembly |
| 02/19/2002 | CA2254922C Process and apparatus for achieving power augmentation in gas turbines via wet compression |
| 02/14/2002 | WO2002012692A1 Compressor starting torque converter |
| 02/14/2002 | WO2002012691A1 Gas turbine engine and method of operation at idle speed |
| 02/14/2002 | WO2002012690A1 Air intake duct |
| 02/14/2002 | US20020018710 Coolant recovery type gas turbine |
| 02/14/2002 | US20020017095 System for chilling inlet air for gas turbines |
| 02/13/2002 | EP1179664A2 Steam cooled gas turbine system |
| 02/12/2002 | US6345955 Bowed nozzle vane with selective TBC |
| 02/12/2002 | US6345495 Gas turbine system for flameless combustion of fuel gases |
| 02/12/2002 | US6345494 Side seal for combustor transitions |
| 02/12/2002 | US6345441 Method of repairing combustion chamber liners |
| 02/12/2002 | CA2246856C Seal device between fastening bolt and bolthole in gas turbine disc |
| 02/12/2002 | CA2229883C Gas turbine shroud and platform seal system |
| 02/12/2002 | CA2077842C Gas turbine engine case counterflow thermal control |
| 02/07/2002 | WO2002010569A1 Proportional bypass valve for a fuel control system |
| 02/07/2002 | WO2001055273A3 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 02/07/2002 | US20020014078 Fuel discharge member, a burner, a premixing nozzle of a combustor, a combustor, a gas turbine, and a jet engine |
| 02/07/2002 | US20020014069 Quasi-Isothermal brayton cycle engine |
| 02/07/2002 | DE10119111A1 Gas turbine engine has exhaust gas drive to separate shaft gives all torque output |
| 02/07/2002 | DE10035676A1 Gasturbine und Verfahren zum Betrieb einer Gasturbine Gas turbine and method of operating a gas turbine |
| 02/06/2002 | EP1178195A2 Gas turbine system |
| 02/06/2002 | EP1177367A1 Seal for sealing a gap, in particular in a turbine, and a turbine |
| 02/06/2002 | EP1177330A2 Thermal barrier coating |
| 02/06/2002 | CN1334760A Repair of turbine exhaust case |
| 02/05/2002 | US6343911 Side wall cooling for nozzle segments for a gas turbine |
| 02/05/2002 | US6343465 Aircraft fuel tank explosion reduction safety method |
| 02/05/2002 | CA2268685C Gas turbine combustion system and combustor ignition method therefor |
| 02/05/2002 | CA2254230C Gas turbine rotor blade |
| 02/05/2002 | CA2253741C Gas turbine cooled blade turbulators |
| 01/31/2002 | WO2002008592A1 Gas turbine and method for operating a gas turbine |
| 01/31/2002 | WO2002008577A1 Method for operating a gas and steam turbine installation and corresponding installation |
| 01/31/2002 | US20020012588 Gas turbine engine |
| 01/31/2002 | US20020011065 Gas turbine exhaust passage and damper system for same |
| 01/31/2002 | US20020011064 Fuel injector with bifurcated recirculation zone |
| 01/31/2002 | DE10035710A1 Fossil-fuel-operated power station, has regenerator having at least three regenerator containers, and which serves as preheater that regains part of heat contained in flue gas |
| 01/30/2002 | EP1176297A1 Internal combustion rotary turbomotor |
| 01/30/2002 | EP1176127A2 Fiber reinforced composite article, fiber containing member, and method for making |
| 01/30/2002 | EP1175956A1 Metallic article with integral end band under compression and method for making |
| 01/30/2002 | EP0902860B1 Process and device for preheating suction air by waste heat in power engines |
| 01/30/2002 | CN1078663C Flow control apparatus for gas turbine engine installation pressure relief doors |
| 01/29/2002 | US6341938 Methods and apparatus for minimizing thermal gradients within turbine shrouds |
| 01/29/2002 | US6341485 Gas turbine combustion chamber with impact cooling |
| 01/29/2002 | CA2245505C Gas turbine generator plant |
| 01/24/2002 | WO2001065086A8 Internal combustion rotary turbomotor |
| 01/24/2002 | US20020009361 Shaft bearing for a turbomachine, turbomachine, and method of operating a turbomachine |
| 01/24/2002 | US20020007820 Apparatus and method for determining the status of a valve arrangement forming part of a fuelling system |
| 01/24/2002 | US20020007624 Method and system for generating power |
| 01/24/2002 | DE10033736A1 Miniature gas turbine for generator drive in hybrid drive vehicle has secondary energy converter for recovery of exhaust gas thermal energy |
| 01/24/2002 | DE10033052A1 Verfahen zum Betreiben einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens Procedure for operating a gas turbine plant and gas turbine system for implementing the method |
| 01/24/2002 | DE10029060A1 Turboluftstrahltriebwerk mit Wärmetauscher Turbojet engine with heat exchanger |
| 01/23/2002 | EP1174587A2 Method of adjusting component airflow |
| 01/23/2002 | EP1174209A1 Method of repairing combustion chamber liners |
| 01/23/2002 | EP1173664A1 Cooling air system |
| 01/23/2002 | EP1173656A1 High pressure turbine cooling of gas turbine engine |
| 01/22/2002 | US6340286 Rotary machine having a seal assembly |
| 01/22/2002 | US6340285 End rail cooling for combined high and low pressure turbine shroud |
| 01/22/2002 | US6339926 Steam-cooled gas turbine combined power plant |
| 01/22/2002 | US6339924 Method and apparatus for encapsulating gas turbine engine fuel connections |
| 01/22/2002 | US6339923 Fuel air mixer for a radial dome in a gas turbine engine combustor |
| 01/17/2002 | WO2002005046A2 Extended range proportional flow valve method |