| 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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| 05/23/1996 | CA2205044A1 Dual fuel gas turbine combustor |
| 05/22/1996 | EP0712466A1 Centrifugal fuel pump with starting stage |
| 05/21/1996 | US5517865 Vortex suppression for an eductor |
| 05/17/1996 | WO1996014370A2 Improvements in the combustion and utilisation of fuel gases |
| 05/17/1996 | CA2202767A1 Improvements in the combustion and utilisation of fuel gases |
| 05/15/1996 | EP0712114A2 Active acoustic liner |
| 05/15/1996 | EP0711956A1 Device for actively controlling the combustion instabilities and the decoking of a fuel injector |
| 05/15/1996 | EP0711497A1 Heat treatment apparatus for turbine blades |
| 05/15/1996 | EP0628090B1 A coated article |
| 05/15/1996 | CN1122447A High temperature detecting head |
| 05/15/1996 | CN1122409A Method for adjusting rotation speed of gas turbine when load is cut off |
| 05/14/1996 | US5516257 Aircraft fan containment structure restraint |
| 05/08/1996 | EP0710728A1 Fibre reinforced metal disc preform and manufacturing method thereof |
| 05/08/1996 | EP0672220B1 Fuel splitter valve assembly for gas turbine |
| 05/08/1996 | EP0607265B1 Closed loop fuel control system and method |
| 05/07/1996 | US5515444 Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors |
| 05/07/1996 | US5513488 Power process utilizing humidified combusted air to gas turbine |
| 05/02/1996 | WO1996012873A1 A system for repairing damaged gas turbine engine airfoils |
| 05/02/1996 | DE19535411A1 Gas turbine engine for model aircraft |
| 05/01/1996 | EP0709561A1 Power plant |
| 05/01/1996 | EP0709547A1 Cooling of the rim of a gas turbine rotor disk |
| 05/01/1996 | EP0708878A1 Apparatus for repairing a combustion chamber assembly |
| 05/01/1996 | EP0708877A1 Method for repairing a combustion chamber assembly |
| 04/30/1996 | US5511945 Turbine motor and blade interface cooling system |
| 04/30/1996 | US5511374 High pressure air source for aircraft and engine requirements |
| 04/30/1996 | US5511309 Method of manufacturing a turbine airfoil with enhanced cooling |
| 04/25/1996 | WO1996012141A1 Tangential air entry fuel nozzle |
| 04/25/1996 | WO1996012049A1 Protective layer for protecting parts against corrosion, oxidation and excessive thermal stresses, as well as process for producing the same |
| 04/25/1996 | DE4437662A1 Aviation gas-turbine with gear system for auxiliary unit drive |
| 04/23/1996 | US5509782 Bearing case support |
| 04/18/1996 | WO1996011465A1 Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors |
| 04/18/1996 | DE4436686A1 Heat resistant material for heat shield used in gas turbines |
| 04/18/1996 | CA2200296A1 Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors |
| 04/17/1996 | EP0706728A1 Engine starting systems and methods |
| 04/16/1996 | US5507620 Gas turbine with cooled rotor |
| 04/11/1996 | DE19536604A1 Zündvorrichtung und Zündverfahren unter Verwendung elektrostatischer Düse und katalytischen Zünders Igniter and ignition method using electrostatic nozzle and catalytic igniter |
| 04/10/1996 | EP0705912A2 A coated article |
| 04/10/1996 | EP0705384A1 Starting fuel pressure schedule for a gas turbine |
| 04/10/1996 | CN1120319A Pulse combusted acoustic agglomeration apparatus and process |
| 04/09/1996 | CA2065158C Integrated power unit combustion apparatus and method |
| 04/05/1996 | CA2159684A1 Ignition apparatus using electrostatic nozzle and catalytic igniter |
| 04/04/1996 | DE4435267A1 Gas turbine operation method |
| 04/03/1996 | EP0704603A2 Sealing and cooking method for the hot side of a gas turbine shaft |
| 04/03/1996 | EP0704601A1 Combined heat shield and retainer for turbine assembly bolt |
| 03/21/1996 | WO1996008643A1 Method for supplying vaporized fuel oil to a gas turbine combustor and system for same |
| 03/20/1996 | EP0702135A1 A fuel injector and igniter assembly |
| 03/20/1996 | EP0702129A2 Cooling the rotor of an axial gasturbine |
| 03/20/1996 | EP0701669A1 Geared drive system for a bladed propulsor |
| 03/19/1996 | US5499651 Deicing system for a butterfly valve |
| 03/19/1996 | US5499497 Temperature detector and control for an igniter |
| 03/14/1996 | DE4432073A1 Vorrichtung zur Befestigung von Turboladern Device for fastening of turbochargers |
| 03/12/1996 | US5498127 Active acoustic liner |
| 03/12/1996 | US5497615 Gas turbine generator set |
| 03/12/1996 | US5497613 Hot gas manifold system for a dual topping combustor gas turbine system |
| 03/12/1996 | US5497612 Laser initiated non-linear fuel droplet ignition method |
| 03/12/1996 | US5497611 Process for the cooling of an auto-ignition combustion chamber |
| 03/07/1996 | DE4431291A1 Hochtemperatursonde High temperature probe |
| 03/06/1996 | CN1118038A Oil seal for gas turbine |
| 03/05/1996 | US5495715 Engine fuel metering system |
| 02/29/1996 | WO1995029331A3 Stator vane arrangement for successive turbine stages |
| 02/28/1996 | EP0698730A2 Lubricants cooling in gas turbine |
| 02/28/1996 | EP0698725A2 Impingement cooling of wall portion |
| 02/28/1996 | EP0698724A2 Cooling circuit for turbine stator vane trailing edge |
| 02/28/1996 | EP0698723A2 Turbine stator vane segment having closed cooling circuit |
| 02/28/1996 | EP0519026B1 Process for starting a gas turbine and gas turbine |
| 02/28/1996 | CN1117753A New power process |
| 02/27/1996 | US5493854 Method for operating a gas turbine in a simple cycle and in a cycle combined with a steam turbine |
| 02/27/1996 | CA2079046C High energy ignition generator in particular for gas turbines |
| 02/24/1996 | CA2155376A1 Turbine stator vane segment having closed cooling circuit |
| 02/24/1996 | CA2155375A1 Cooling circuit for turbine stator vane trailing edge |
| 02/22/1996 | WO1996005625A2 Ultra-high efficiency turbine and fuel cell combination |
| 02/22/1996 | WO1996005412A1 Pressurized ball bearing assemblies |
| 02/21/1996 | EP0697507A2 Gasturbine speed control method for sudden load loss |
| 02/21/1996 | EP0696985A1 Nacelle arrangement |
| 02/20/1996 | US5492195 Muffler traversed by a fluid |
| 02/20/1996 | US5491972 Combination igniter and fuel atomizer nozzle assembly for a gas turbine engine |
| 02/15/1996 | WO1996004516A1 Microcomponent sheet architecture |
| 02/15/1996 | DE4427987A1 Air storage turbine using waste heat steam raising equipment |
| 02/13/1996 | US5491308 Modular sound attenuation assembly for an auxiliary power unit |
| 02/13/1996 | US5490387 Flame-out resistant fuel pumping system |
| 02/13/1996 | US5490377 Performance enhanced gas turbine powerplants |
| 02/08/1996 | WO1996003536A1 Protective coating |
| 02/08/1996 | WO1996003535A1 Protective coating |
| 02/07/1996 | EP0604436B1 Ducted fan gas turbine engine accessory drive system |
| 02/07/1996 | CN1116274A Method for controlling gas turbine group |
| 02/06/1996 | US5490195 Method for measuring and extending the service life of fatigue-limited metal components |
| 02/06/1996 | US5488829 Method and apparatus for reducing noise generated by combustion |
| 02/01/1996 | WO1996002567A1 Proteins from mammalian liver and their use in oncology |
| 02/01/1996 | CA2194861A1 Proteins from mammalian liver and their use in oncology |
| 01/31/1996 | EP0694120A1 Integrated engine control system for a gas turbine engine |
| 01/30/1996 | US5487265 Gas turbine coordinated fuel-air control method and apparatus therefor |
| 01/25/1996 | DE4445794C1 Gas-duct inner tube externally joined to heavy metal formers |
| 01/24/1996 | EP0558726B1 Thermal anti-icing of aircraft structures |
| 01/23/1996 | US5486093 Leading edge cooling of turbine airfoils |
| 01/23/1996 | US5486091 Gas turbine airfoil clocking |
| 01/23/1996 | US5486090 Turbine shroud segment with serpentine cooling channels |
| 01/23/1996 | US5485959 Axisymmetric vectoring exhaust nozzle thermal shield |
| 01/23/1996 | US5485723 Variable thickness isogrid case |
| 01/23/1996 | US5485720 Laser initiated non-linear fuel droplet ignition |
| 01/23/1996 | US5485719 Integration of combustor-turbine units and integral-gear pressure processors |