| 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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| 05/17/1994 | US5311734 System and method for improved engine cooling in conjunction with an improved gas bearing face seal assembly |
| 05/14/1994 | CA2102637A1 Circulating fluidized bed reactor combined cycle power generation system |
| 05/11/1994 | WO1994010619A1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft |
| 05/11/1994 | EP0596062A1 Exhaust vent for de-icing system of aircraft nacelle. |
| 05/11/1994 | EP0349635B1 Turbine combustor with tangential fuel injection and bender jets |
| 05/11/1994 | CN1086581A Advanced regenerative parallel compound dual fluid heat engine-advanced cheng cycle (ACC) |
| 05/11/1994 | CA2143871A1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft |
| 05/10/1994 | US5309708 Multifunction integrated power unit |
| 05/10/1994 | CA1329352C Gas turbine plant system and gas pressure stabilizer thereof in emergency |
| 05/08/1994 | CA2102544A1 Method of operating a combined installation |
| 05/03/1994 | US5309029 Aircraft power unit with elective mechanical coupling |
| 05/03/1994 | US5308225 Rotor case treatment |
| 05/03/1994 | US5307633 Low carbon particle producing gas turbine combustor |
| 05/03/1994 | US5307632 Engine and method for turbo boosted operation of a mechanically assisted turbocharger in a two cycle engine |
| 05/03/1994 | US5307620 Fuel gas burning control method |
| 04/27/1994 | EP0593987A1 Variable square air intake duct |
| 04/27/1994 | EP0593816A1 Burner with electric ignition device |
| 04/26/1994 | US5305616 Gas turbine engine cooling system |
| 04/26/1994 | US5305609 Fuel injector arrangement |
| 04/26/1994 | US5305596 Method for preventing lean flaeout at ignition of a stored energy system for driving a turbine wheel |
| 04/26/1994 | CA2034412C Dry packing for rotating part and rotating machine including such packing |
| 04/21/1994 | DE4335598A1 Preventing fouling and increasing power in gas turbine installation - cooling intake air to below zero by turbo cooling unit consisting of compressor, cooler and expansion turbine preceding gas turbine proper |
| 04/20/1994 | EP0539359B1 Flame tube with a cooled supporting frame for a heat-resistant lining |
| 04/19/1994 | US5303541 Closed loop fuel control method |
| 04/14/1994 | WO1994008179A1 Multiple passage cooling circuit for gas turbine fuel injector nozzle |
| 04/14/1994 | WO1994008131A1 Laser initiated non-linear fuel droplet ignition |
| 04/13/1994 | EP0592223A1 Auto-ignition system and method for premixed gas turbine combustors |
| 04/13/1994 | EP0592161A1 Gas turbine engine combustor |
| 04/13/1994 | EP0591154A1 Turbofan engine fixed plug noise suppressor. |
| 04/13/1994 | CN1024212C Method and equipment for generating mechanical energy |
| 04/12/1994 | US5301901 Telescoping centerbody wedge for a supersonic inlet |
| 04/08/1994 | CA2107842A1 Auto-ignition system for premixed gas turbine combustors |
| 04/06/1994 | EP0590310A1 Gas turbine with flanged exhaust casing |
| 04/05/1994 | US5299920 Fixed geometry variable displacement pump system |
| 04/05/1994 | US5299914 Staggered fan blade assembly for a turbofan engine |
| 03/31/1994 | WO1994007005A1 Turbine vane assembly with integrally cast cooling fluid nozzle |
| 03/31/1994 | WO1994007004A1 Aluminide-silicide coatings, coating compositions, process for coating and improved coated products |
| 03/31/1994 | DE4232738A1 Supersonic missile flight control system - has air intakes in shell between tip and body connected to control nozzles in shell wall via reservoir and fluid elements |
| 03/30/1994 | EP0589745A1 Inlet control system of a turbomachine |
| 03/30/1994 | EP0589679A2 Method of preventing fuel thermal degradation deposits |
| 03/30/1994 | EP0589215A1 Gasturbine with exhaust casing and exhaust duct |
| 03/29/1994 | US5297390 Fuel injection nozzle having tip cooling |
| 03/29/1994 | US5297386 Cooling system for a gas turbine engine compressor |
| 03/23/1994 | EP0588629A1 Gas turbine fuel nozzle with replaceable cap |
| 03/23/1994 | CN1084247A Supporting case of waste gas turbosupercharger which can be assembled on internal-combustion engine |
| 03/23/1994 | CA2105188A1 Coated article for hot hydrocarbon fluid and method of preventing fuel thermal degradation deposits |
| 03/22/1994 | US5295787 Turbine engines |
| 03/22/1994 | US5295350 Process for the generation of power |
| 03/19/1994 | CA2106424A1 Gas turbine fuel nozzle with replaceable cap |
| 03/17/1994 | WO1993024754A3 A gas compressor |
| 03/16/1994 | EP0587153A2 Sealing device between spaces of different fluidic pressions for relatively movable housings of aircraft engines |
| 03/16/1994 | EP0586452A1 Noise attenuation panel |
| 03/16/1994 | EP0518868B1 Process and device for generating mechanical energy |
| 03/16/1994 | CN1083899A Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors |
| 03/16/1994 | CN1024032C Fully electromatic starter for aircraft engines |
| 03/15/1994 | US5294410 Gas purification and conditioning system |
| 03/15/1994 | US5293775 Gas turbine engine test cell |
| 03/09/1994 | EP0586287A1 High energy ignition generator especially for a gas turbine |
| 03/08/1994 | US5292227 Turbine frame |
| 03/08/1994 | CA1327522C Cleaning gas turbine inlet air |
| 03/08/1994 | CA1327455C Breach-cooled structure |
| 03/05/1994 | CA2105042A1 High-energy ignition generator in particular for a gas turbine |
| 03/03/1994 | WO1994004795A1 Energy generation process in a combined gas-steam power station |
| 03/02/1994 | EP0584958A1 Intercooled turbine blade cooling air feed system |
| 03/02/1994 | EP0584906A2 Film cooling starter geometry for combustor liners |
| 03/02/1994 | EP0448678B1 A fluid flow system |
| 03/01/1994 | US5289685 Fuel supply system for a gas turbine engine |
| 02/24/1994 | DE4227146A1 Verfahren zur Erzeugung von Energie in einer kombinierten Gas-Dampfkraftanlage Process for the production of energy in a combined gas-steam power plant |
| 02/23/1994 | EP0584037A1 Method and control system for preventing crash engagement of a ratchet and pawl clutch during restart of a turbine engine |
| 02/22/1994 | US5288204 Gas turbine engine support structure |
| 02/22/1994 | US5287697 Variable area bypass injector seal |
| 02/22/1994 | US5287694 Fluid channeling system |
| 02/22/1994 | CA2104523A1 Gas turbine fuel nozzle assembly |
| 02/17/1994 | WO1994003864A1 Process and device for monitoring vibrational excitation of an axial compressor |
| 02/17/1994 | WO1994003863A1 Process for detecting fouling of an axial compressor |
| 02/17/1994 | WO1994003862A1 Process and device for monitoring and for controlling of a compressor |
| 02/17/1994 | DE4226666A1 Heat exchanger with cruciform, counter-current matrix of profiled tubes - adds fraction of part-stream to gas flowing round profile tubes in coupling region to centre tube |
| 02/17/1994 | CA2141592A1 Process and device for monitoring vibrational excitation of an axial compressor |
| 02/17/1994 | CA2141544A1 Process and device for monitoring and for controlling of a compressor |
| 02/17/1994 | CA2141542A1 Process for detecting fouling of an axial compressor |
| 02/15/1994 | US5285636 Diagnostic drain mast for a gas turbine engine |
| 02/15/1994 | US5285626 Drive for main engine auxiliaries for an aircraft gas turbine engine |
| 02/10/1994 | DE4225858A1 Ash particle solidification and removal for a coal-dust fired gas-turbine installation - by partial cooling of combustion gases by injection of pass-out steam, water, or air |
| 02/10/1994 | DE4225625A1 Exhaust gas turbo-charger with compression and turbine on common shaft - has increased space round ribbed cross-section and jacketed intermediate wall between compressor and turbine |
| 02/09/1994 | EP0582522A1 Mounting device of a turbine engine on an aircraft structure |
| 02/09/1994 | EP0582427A1 Reducing thermal deposits in propulsion systems |
| 02/09/1994 | EP0581978A1 Multi-zone diffuser for turbomachine |
| 02/08/1994 | US5284020 Fuel supply system for gas turbine engines |
| 02/08/1994 | US5284012 Nacelle cooling and ventilation system |
| 02/03/1994 | WO1994002728A1 Process for operating a gas turbine |
| 02/03/1994 | WO1994002727A1 Method for conversion of thermal energy into mechanical energy in gas-turbine engine and gas-turbine engine |
| 02/03/1994 | DE4325346A1 Turbine housing with improved oxidn. resistance - coated in sensitive areas with diffusion alloy of nickel@ and chromium@ |
| 02/02/1994 | EP0580910A1 Combined power cycle with liquefied natural gas (LNG) and synthesis or fuel gas |
| 02/02/1994 | EP0580583A1 A combustion chamber assembly. |
| 02/01/1994 | US5283499 For use with an engine |
| 01/26/1994 | EP0580277A1 Ducted fan gas turbine engine |
| 01/25/1994 | US5281091 Electrical anti-icer for a turbomachine |
| 01/25/1994 | US5281089 Apparatus and method for a stator assembly of a rotary machine |
| 01/25/1994 | US5281085 Clearance control system for separately expanding or contracting individual portions of an annular shroud |
| 01/25/1994 | US5281084 Curved film cooling holes for gas turbine engine vanes |