| 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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| 11/24/1992 | US5165236 For utilizing gases |
| 11/24/1992 | US5165232 Dual charge engine start accumulator |
| 11/24/1992 | US5165228 Turboramjet engine |
| 11/24/1992 | US5165226 Single vortex combustor arrangement |
| 11/24/1992 | US5165223 Process for starting a gas turbine and gas turbine |
| 11/24/1992 | CA2069274A1 Fluid production method and apparatus |
| 11/21/1992 | CA2065639A1 Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines |
| 11/19/1992 | EP0514260A1 Device for regulating the air supply of a gas turbine |
| 11/19/1992 | EP0514119A1 Nacelle cooling and ventilation system |
| 11/19/1992 | EP0513959A1 Shear wire flange joint |
| 11/19/1992 | EP0513957A1 Scavenge air removal and bypass system and method of operation |
| 11/19/1992 | EP0513956A1 Boltless turbine nozzle/stationary seal mounting |
| 11/17/1992 | US5163287 Stored energy combustor with fuel injector containing igniter means for accommodating thermal expansion |
| 11/17/1992 | US5163285 Cooling system for a gas turbine |
| 11/17/1992 | CA2065678A1 Nacelle cooling and ventilation system |
| 11/17/1992 | CA1310273C Axial flow gas turbine |
| 11/17/1992 | CA1310194C Auxiliary power source in an unducted fan gas turbine engine |
| 11/14/1992 | CA2065723A1 Lightweight engine turbine bearing support assembly for withstanding radial and axial loads |
| 11/14/1992 | CA2065680A1 Shear wire flange joint |
| 11/12/1992 | WO1992019854A1 Separable fan strut for a gas turbofan powerplant |
| 11/12/1992 | DE4114678A1 Gas turbine engine operating method - has atomiser nozzle to inject water, so that evaporation enthalpy corresponds to output of adiabatic compression |
| 11/11/1992 | EP0512941A1 Stator assembly for a rotary machine |
| 11/11/1992 | EP0512568A1 System and method for integration of combustor-turbine units and compressors |
| 11/11/1992 | CA2068272A1 System and method for integration of combustor-turbine units and compressors |
| 11/10/1992 | US5161947 Fan case strut for turbomachine |
| 11/10/1992 | US5161365 Endothermic fuel power generator and method |
| 11/10/1992 | US5161364 Control of aircraft bleed air stage mixing |
| 11/10/1992 | US5161363 Providing power to an aircraft |
| 11/10/1992 | CA1309873C Gas turbine combustor transition duct forced convection cooling |
| 11/10/1992 | CA1309872C Jet engine noise suppression system |
| 11/04/1992 | EP0511935A1 Bleed air control by mixing |
| 11/04/1992 | EP0511770A1 Heat exchanger system |
| 11/03/1992 | US5160251 Lightweight engine turbine bearing support assembly for withstanding radial and axial loads |
| 11/03/1992 | US5160248 Aluminum or alloy honeycomb |
| 11/03/1992 | US5160096 Gas turbine cycle |
| 11/03/1992 | US5160069 For a turbine engine |
| 11/03/1992 | US5160005 Pawl and ratchet clutch with torsion shaft |
| 11/03/1992 | US5159808 Gas turbine engine fuel and hydraulic fluid pumping system |
| 10/29/1992 | WO1992018760A1 A combustion chamber assembly |
| 10/29/1992 | DE4113247A1 Gas turbine plant for motor vehicle - has compressor rotor and turbine rotor formed by rotors of mass-produced exhaust gas turbochargers |
| 10/27/1992 | US5157915 Pod for a turbofan aero engine of the forward contrafan type having a very high bypass ratio |
| 10/27/1992 | US5157914 Modulated gas turbine cooling air |
| 10/23/1992 | CA2062887A1 Heat exchanger system |
| 10/21/1992 | EP0509802A1 Tip clearance control apparatus |
| 10/20/1992 | US5156001 Fuel supply circuit for a turbo-engine |
| 10/20/1992 | CA1308925C Gas turbine engine |
| 10/20/1992 | CA1308924C Jet engine fan and compressor bearing support |
| 10/20/1992 | CA1308923C Jet engine turbine support |
| 10/17/1992 | CA2062929A1 Tip clearance control apparatus and method |
| 10/15/1992 | WO1992017686A1 Turbine casing |
| 10/13/1992 | US5155437 Diagnostic device for gas turbine ignition system |
| 10/13/1992 | US5154052 Exhaust assembly for a high speed civil transport aircraft engine |
| 10/07/1992 | EP0378658B1 Surge protected gas turbine engine for providing variable bleed air flow |
| 10/06/1992 | US5152666 Stator assembly for a rotary machine |
| 10/06/1992 | US5152169 Gas turbine engine thrust measurement |
| 10/06/1992 | US5152146 Fuel control valve for an aircraft gas turbine engine fuel system |
| 10/06/1992 | US5152141 Management of electrically driven engine accessories |
| 09/29/1992 | US5150571 Device for exposing or shutting off a turbo-engine on the intake air side of the engine |
| 09/29/1992 | US5150570 Unitized fuel manifold and injector for a turbine engine |
| 09/29/1992 | US5150569 Integrated propulsion system |
| 09/29/1992 | US5150568 Control and protection system for turbine engines contained within a protective housing |
| 09/29/1992 | CA1307942C Optical radiation sensor apparatus |
| 09/23/1992 | EP0505263A1 Natural gas turbine with steam injection in semi open cycle |
| 09/23/1992 | CN1018384B Bimodal swirler injector for gas turbine combustor |
| 09/22/1992 | US5149250 Gas turbine vane assembly seal and support system |
| 09/22/1992 | US5148673 Integrated turboramjet engine |
| 09/22/1992 | US5148671 Fuel circulation control system |
| 09/22/1992 | US5148670 Gas turbine cogeneration apparatus for the production of domestic heat and power |
| 09/22/1992 | US5148669 Assembly for creating |
| 09/22/1992 | CA1307673C Center fastened stationary intake cowling for jet engine and jet engine equipped with said cowling |
| 09/22/1992 | CA1307672C Turbo-engine guard |
| 09/19/1992 | CA2062373A1 Natural gas steam turbine system operating with a semi-open cycle |
| 09/16/1992 | EP0504095A2 Gas turbine engine component repair |
| 09/16/1992 | EP0503752A1 Cooled shroud support |
| 09/08/1992 | US5145126 Engine nacelle |
| 09/08/1992 | US5144794 Gas turbine engine with cooling of turbine blades |
| 09/08/1992 | CA1307120C Wide range gaseous fuel combustion system for gas turbine engines |
| 09/08/1992 | CA1307119C Shut off valve for turbine engine |
| 09/02/1992 | EP0501813A1 Turbine airfoil with arrangement of multi-outlet film cooling holes |
| 09/02/1992 | EP0501700A1 Gas turbine vane assembly seal and support system |
| 09/02/1992 | EP0501152A2 Apparatus for ignition diagnosis in a combustion turbine |
| 09/02/1992 | EP0501066A1 Turbine rotor disk with integral blade cooling air slots and pumping vanes |
| 09/01/1992 | US5143512 Turbine rotor disk with integral blade cooling air slots and pumping vanes |
| 09/01/1992 | US5143329 Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
| 09/01/1992 | US5142859 Turbine cooling system |
| 09/01/1992 | US5142778 Gas turbine engine component repair |
| 09/01/1992 | CA1306873C Low coke fuel injector for a gas turbine engine |
| 09/01/1992 | CA1306872C Aircraft engine frame construction |
| 08/29/1992 | CA2059937A1 Gas turbine vane assembly seal and support system |
| 08/29/1992 | CA2059913A1 Turbine rotor disk with integral blade cooling air slots and pumping vanes |
| 08/28/1992 | CA2061881A1 Method and apparatus for ignition diagnosis in a combustion turbine |
| 08/26/1992 | EP0500487A1 Improved oil filtration system and method |
| 08/26/1992 | EP0500486A1 Segmented brush seal and method of manufacturing the seal |
| 08/26/1992 | EP0407408B1 Process and installation for recuperation of energy from oil wells |
| 08/25/1992 | US5141401 Stress-relieved rotor blade attachment slot |
| 08/25/1992 | US5141395 Flow activated flowpath liner seal |
| 08/25/1992 | US5141182 Gas turbine engine fan duct base pressure drag reduction |
| 08/25/1992 | US5140819 Turbine inlet silencer |
| 08/25/1992 | US5140807 Air blast tube impingement fuel injector for a gas turbine engine |
| 08/23/1992 | WO1992014918A1 An improved turbine cooling system |