| 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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| 05/20/1992 | EP0486226A1 Combustor liner with circumferentially angled film cooling holes |
| 05/20/1992 | CA2048807A1 Self-powered heat exchange system |
| 05/19/1992 | US5114103 Aircraft engine electrically powered boundary layer bleed system |
| 05/19/1992 | US5113669 Self-powered heat exchange system |
| 05/19/1992 | US5113649 Passive bypass valve assembly |
| 05/16/1992 | CA2048726A1 Combustor liner with circumferentially angled film cooling holes |
| 05/13/1992 | EP0485175A1 Diffuser with splitter for gas turbine compressor |
| 05/12/1992 | US5111663 Turbine start-up particulate separator |
| 05/12/1992 | US5111653 Fuel delivery system with capacity monitor |
| 05/12/1992 | US5111570 Metal alloy substrate |
| 05/10/1992 | CA2048808A1 Profile matched diffuser |
| 05/05/1992 | US5110269 Gas turbine fuel pumping apparatus |
| 05/05/1992 | US5110033 Segmented brush seal |
| 05/05/1992 | US5109664 Method of operating a combustion chamber for a gas turbine engine |
| 04/30/1992 | WO1992007179A1 Fuel supply system |
| 04/30/1992 | DE4033711A1 Thermal insulation on housing side - consists of cladding with filler and elastic covering, expansion gap with metal sheet and cavity in between |
| 04/29/1992 | EP0482791A1 Windage shield |
| 04/29/1992 | EP0482758A1 Thermal seal for a gas turbine spacer disc |
| 04/28/1992 | US5108259 Flexible connector for use in aircraft |
| 04/28/1992 | US5108258 System for supporting the rotor in an axial exhaust turbine with an exhaust end bearing having isotropic stiffness and directly connected to a foundation |
| 04/28/1992 | US5107674 Control for a gas turbine engine |
| 04/22/1992 | EP0481620A1 Fuel control system for a gas turbine engine |
| 04/22/1992 | EP0481593A2 Fuel circulation control system |
| 04/22/1992 | EP0481592A1 Continuous flow fuel circulation system |
| 04/22/1992 | EP0481134A1 Recuperative heat exchanger |
| 04/22/1992 | CN1016374B Coolable thin metal sheet |
| 04/21/1992 | US5106264 System for supporting the rotor of an axial exhaust turbine with the exhaust end bearing being integrated in the foundation |
| 04/21/1992 | US5105625 Mounting for a ceramic scroll in a gas turbine machine |
| 04/21/1992 | US5105617 Cogeneration system with recuperated gas turbine engine |
| 04/21/1992 | US5105615 Turbojet engine with at least one axially movable arranged sliding valve |
| 04/18/1992 | CA2048837A1 Continuous flow fuel circulation system |
| 04/15/1992 | EP0479861A1 A device for the indirect heating of air |
| 04/15/1992 | CN1016265B Apparatus for combustion |
| 04/14/1992 | US5104286 Recirculation seal for a gas turbine exhaust diffuser |
| 04/14/1992 | US5103632 Seal for a stored energy combustor |
| 04/14/1992 | US5103631 Differential gear assembly |
| 04/14/1992 | US5103629 Gas turbine control system having optimized ignition air flow control |
| 04/08/1992 | EP0478703A1 Ecs with advanced air cycle machine |
| 04/08/1992 | CN1060137A Thermal seal for gas turbine space disc |
| 04/07/1992 | US5102697 Structural component made of a titanium alloy and covered by a protective coating and method for producing the coating |
| 04/07/1992 | US5102295 Thrust force-compensating apparatus with improved hydraulic pressure-responsive balance mechanism |
| 04/07/1992 | US5102221 Apparatus for retouching, in situ, components such as the rotor blades of a turbomachine, and a retouching method using the apparatus |
| 04/07/1992 | US5101619 Method for correcting a hot start condition |
| 04/07/1992 | US5101533 Vibration damping hinge joints for variable area jet engine exhaust nozzles |
| 04/07/1992 | CA1298615C Gas turbine unit for combined production of electricity and heat and method for operating such unit |
| 04/02/1992 | WO1992005351A1 Multifunction integrated power unit and power transfer apparatus therefor |
| 04/02/1992 | WO1992005343A1 Exhaust system for thermal electric stations, in particular gas turbine stations |
| 04/01/1992 | EP0478494A1 Apparatus and method for a stator assembly of a rotary machine |
| 04/01/1992 | EP0478234A1 Stress-relieved rotor blade attachment slot |
| 04/01/1992 | CN2100491U Channel-cooling structure of gas turbine moving blades |
| 04/01/1992 | CN1016083B Wall having cooling passage |
| 03/31/1992 | US5099869 Discharge arrangement for a pressure relief valve in a pressurized hot fluid circuit of an aircraft |
| 03/28/1992 | CA2048757A1 Stress-relieved rotor blade attachment slot |
| 03/26/1992 | DE4030174A1 Abgassystem fuer eine waermekraftanlage, insbesondere eine gasturbinenanlage Exhaust system for a waermekraftanlage, especially a gas turbine plant |
| 03/25/1992 | EP0475973A1 Apparatus for use in a fuel delivery system for a gas turbine engine |
| 03/24/1992 | US5098257 Apparatus and method for minimizing differential thermal expansion of gas turbine vane structures |
| 03/24/1992 | US5097666 Combustor fuel injection system |
| 03/24/1992 | US5097659 Airframe power unit using stored air and jet fuel |
| 03/24/1992 | US5097658 Integrated power unit control apparatus and method |
| 03/18/1992 | EP0475316A1 Gas turbine engine blade platform trimmer |
| 03/18/1992 | EP0475102A2 Apparatus and method for minimizing differential thermal expansion of gas turbine vane structures |
| 03/17/1992 | US5096157 Planetary roller type flow control valve |
| 03/17/1992 | US5095707 Extraterrestrial planetary power supply and method |
| 03/17/1992 | US5095694 Fuel purging system for a turbine engine |
| 03/17/1992 | US5095693 High-efficiency gas turbine engine |
| 03/17/1992 | US5095617 Method for forming a drain assembly |
| 03/17/1992 | CA1297305C Fuel nozzle guide structure and retainer for a gas turbine engine |
| 03/11/1992 | EP0474585A1 A dual pump improved fuel delivery system |
| 03/11/1992 | EP0473991A2 Gas turbine with cooled rotor blades |
| 03/11/1992 | CA2050961A1 Apparatus and method for minimizing differential thermal expansion of gas turbine vane structures |
| 03/10/1992 | US5095221 Gas turbine control system having partial hood control |
| 03/10/1992 | US5094071 Turboramjet engine |
| 03/05/1992 | WO1992003644A1 Secondary ignition system |
| 03/05/1992 | WO1991004395A3 Integrated power unit |
| 03/05/1992 | CA2050546A1 Apparatus and method for cooling rotating blades in a gas turbine |
| 03/04/1992 | EP0473494A1 Fuel supply system for a turbo-engine |
| 02/28/1992 | CA2046765A1 Aircraft engine electrically powered boundary layer bleed system |
| 02/25/1992 | US5090865 Windage shield |
| 02/25/1992 | US5090194 Fluidic multiplexer for fluid servomotors in a gas turbine engine |
| 02/19/1992 | EP0471438A1 Gas turbine engine combustor |
| 02/19/1992 | EP0471437A1 Gas turbine engine combustor |
| 02/18/1992 | US5088775 Seal ring with flanged end portions |
| 02/18/1992 | US5088742 Hydraulic seal and method of assembly |
| 02/18/1992 | US5088660 Bleed stability door |
| 02/18/1992 | US5088280 Prevention of icing in the intakes of aerospace propulsors |
| 02/18/1992 | US5088279 Duct support assembly |
| 02/18/1992 | US5088277 Aircraft engine inlet cowl anti-icing system |
| 02/12/1992 | EP0470868A1 Forge joining repair technique |
| 02/11/1992 | US5086968 Weld repairable combustor |
| 02/11/1992 | US5086617 Gas turbine engine fuel control system, and metering valve |
| 02/06/1992 | WO1992001891A1 Flame tube with a cooled supporting frame for a heat-resistant lining |
| 02/05/1992 | EP0469827A1 Heat exchange arrangement in a fan duct |
| 02/05/1992 | EP0469826A2 Seal assembly for segmented turbine engine structures |
| 02/05/1992 | EP0469825A2 Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
| 02/05/1992 | EP0469784A2 Aft entry cooling system and method for an aircraft engine |
| 02/05/1992 | CN1058449A Thermal linear actuator for rotor air flow control in gas turbine |
| 02/04/1992 | US5085559 Composite vane |
| 02/04/1992 | US5085040 Torch igniters |
| 02/04/1992 | US5085039 Coanda phenomena combustor for a turbine engine |
| 02/04/1992 | US5085038 Gas turbine engine |