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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08/23/1992 | CA2098741A1 Turbine cooling system |
08/19/1992 | EP0309485B1 Wide range gaseous fuel combustion system for gas turbine engines |
08/18/1992 | US5139545 Air intakes for gas turbine engines |
08/12/1992 | CA2060914A1 Combustor degradation detection system |
08/11/1992 | US5137425 Propfan engine having two oppositely rotating fan rotors |
08/11/1992 | US5137421 Shroud rings |
08/11/1992 | US5136838 Stored energy, wide energy range turbine starting system |
08/11/1992 | US5136837 Aircraft engine starter integrated boundary bleed system |
08/09/1992 | CA2060876A1 Recirculation seal for a gas turbine exhaust diffuser |
08/06/1992 | WO1992009821A3 An improved pawl and ratchet clutch and method |
08/06/1992 | DE4102833A1 Gas turbine engine - has multiple compressors between pre-compressor and combustion chamber and mounted circumferentially |
08/05/1992 | EP0497574A1 Fan case treatment |
08/04/1992 | US5134855 Air flow diffuser with path splitter to control fluid flow |
08/04/1992 | US5134844 Aft entry cooling system and method for an aircraft engine |
08/04/1992 | US5134841 Combined gas/steam turbine process |
07/28/1992 | US5133180 Chemically recuperated gas turbine |
07/23/1992 | WO1992013339A1 Noise attenuation panel |
07/23/1992 | WO1992012855A1 Noise attenuation panel |
07/23/1992 | WO1992012854A1 Structural cellular component |
07/23/1992 | CA2098099A1 Noise attenuation panel |
07/23/1992 | CA2092411A1 Noise attenuation panel |
07/23/1992 | CA2092410A1 Structural cellular component |
07/22/1992 | EP0495587A1 Gas turbine engine fuel manifold |
07/21/1992 | US5131840 Combustion device for combustion of two fluid components |
07/21/1992 | US5131223 Integrated booster and sustainer engine for a missile |
07/15/1992 | EP0494389A1 Corrosion resistant magnesium titanate coatings for gas turbines |
07/15/1992 | EP0494167A1 Vertical gas turbine. |
07/15/1992 | CN1062779A Pressurized fluidized-bed boiler power plant |
07/14/1992 | US5129599 Hybrid liquid-vapor propellant feed system for aerospace vehicles |
07/14/1992 | US5129226 Flameholder for gas turbine engine afterburner |
07/14/1992 | US5129224 Cooling of turbine nozzle containment ring |
07/14/1992 | US5129222 Constant air/fuel ratio control system for EPU/IPU combustor |
07/14/1992 | US5129221 Gas turbine engine fuel control system with enhanced relight capability |
07/09/1992 | WO1992011451A1 Heat exchange apparatus for gas turbine fluids |
07/08/1992 | CA2058781A1 Corrosion resistant magnesium titanate coatings for gas turbines |
07/07/1992 | US5127793 Turbine shroud clearance control assembly |
07/07/1992 | US5127229 Gas turbine combustor |
07/07/1992 | US5127222 Buffer region for the nacelle of a gas turbine engine |
07/07/1992 | US5127221 Transpiration cooled throat section for low nox combustor and related process |
07/07/1992 | US5127220 Method for accelerating a gas turbine engine |
07/01/1992 | EP0493111A1 Gas turbine with modulation of cooling air |
07/01/1992 | EP0493004A1 Gas generator for a gas turbine |
07/01/1992 | EP0492865A1 Clearance control system |
07/01/1992 | EP0491966A1 Support device of a thermal turbomachine |
07/01/1992 | CN1017276B Fluidic multiplexer |
06/30/1992 | US5126612 Active radial magnetic bearing combined with a back-up bearing |
06/30/1992 | US5125793 Turbine blade cooling with endothermic fuel |
06/30/1992 | US5125597 Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system |
06/30/1992 | US5125228 Diaphragm seal plate |
06/30/1992 | US5125226 Coupling ducts or the like |
06/25/1992 | WO1992010657A1 Process for starting a gas turbine and gas turbine |
06/25/1992 | WO1992010656A1 Diaphragm seal plate |
06/25/1992 | WO1992010655A1 Device in a power plant |
06/24/1992 | EP0491589A1 Ignition generator of high energy e.g. for gas turbine |
06/23/1992 | US5124052 Bypass; prevention blockage of filter |
06/23/1992 | US5123810 Power transmission |
06/23/1992 | US5123242 Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
06/23/1992 | US5123241 System for deforming a turbine stator housing |
06/23/1992 | US5123240 Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine |
06/23/1992 | US5123239 Method of starting a gas turbine engine |
06/22/1992 | CA2056591A1 Clearance control system |
06/17/1992 | EP0490522A1 Turbine rotor seal body |
06/17/1992 | EP0490470A1 Integrated propulsion system |
06/17/1992 | EP0489894A1 A composite structural component. |
06/17/1992 | DE4036176C1 Fuel nozzle for atomising gas stream - has auxiliary scavenging water line to act on fuel line |
06/16/1992 | US5121600 Transportable electrical power generating system fueled by organic waste |
06/16/1992 | US5121599 Oil filtration system and method |
06/16/1992 | US5121598 Management system for heat generated by aircraft gas turbine installations |
06/16/1992 | US5121597 Gas turbine combustor and methodd of operating the same |
06/16/1992 | US5121596 Method of starting gas turbine |
06/16/1992 | CA1303371C High pressure seal |
06/16/1992 | CA1303369C Fuel spraybar |
06/16/1992 | CA1303368C Separator having multiple particle extraction passageways |
06/11/1992 | WO1992009850A1 Ceramic heat shield on a bearing structure |
06/11/1992 | WO1992009821A2 An improved pawl and ratchet clutch and method |
06/11/1992 | WO1992009790A1 Method and apparatus for enhancing gas turbo machinery flow |
06/11/1992 | CA2048805A1 Turbine rotor seal body |
06/10/1992 | EP0489653A1 Seal joint between fuselage and segments of jet engine exhaust nozzle |
06/10/1992 | EP0489193A1 Combustion chamber for gas turbine |
06/10/1992 | EP0350503B1 Fuel injectors for turbine engines |
06/09/1992 | US5120975 Gas turbine flame detection system with reflected flame radiation attenuator |
06/09/1992 | US5120192 Cooled turbine blade and combined cycle power plant having gas turbine with this cooled turbine blade |
06/09/1992 | US5119636 Fuel injector for a turbine engine |
06/09/1992 | US5119624 Gas turbine engine power unit |
06/03/1992 | EP0488579A1 Pressurized fluidized-bed boiler power plant |
06/03/1992 | CN1016892B Gas-cooled flameholder assembly |
06/02/1992 | US5118258 Dual pump fuel delivery system |
06/02/1992 | US5117908 Method and equipment for obtaining energy from oil wells |
06/02/1992 | US5117626 Apparatus for cooling rotating blades in a gas turbine |
05/27/1992 | EP0487242A1 Compressor bleed structure |
05/27/1992 | EP0487241A1 Heat exchange system |
05/27/1992 | EP0487193A1 Attenuating turbine shroud support |
05/27/1992 | EP0487125A1 Mounting for a ceramic scroll in a gas turbine engine |
05/26/1992 | US5116362 Fuel metering and actuation system |
05/26/1992 | US5116251 Inlet system for supersonic or hypersonic aircraft |
05/26/1992 | US5116001 Variable air intake |
05/26/1992 | US5115638 Propulsion turbine fuel control system |
05/26/1992 | US5115637 External cartridge gas combustor ignitor |
05/26/1992 | US5115633 Compact high-energy auxiliary power method and means |
05/24/1992 | CA2048779A1 Attenuating shroud support |