| 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) |
|---|
| 02/04/1992 | US5085037 Minimizing the effects of icing in the intakes of aerospace propulsors |
| 02/02/1992 | CA2046797A1 Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air |
| 01/31/1992 | CA2042220A1 Aft entry cooling system and method for an aircraft engine |
| 01/31/1992 | CA2042216A1 Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
| 01/31/1992 | CA2042197A1 Seal assembly for segmented turbine engine structures |
| 01/29/1992 | EP0468782A2 Gas turbine rotor and operation thereof |
| 01/29/1992 | EP0468253A2 Diagnostic device for gas turbine ignition system |
| 01/28/1992 | US5083429 Method of and compression tube for increasing pressure of a flowing gaseous medium, and power machine applying the compression tube |
| 01/28/1992 | US5083423 Apparatus and method for optimizing the air inlet temperature of gas turbines |
| 01/23/1992 | WO1992001149A1 Radial inflow particle separation method and apparatus |
| 01/21/1992 | US5082245 Spill proof check valve apparatus |
| 01/21/1992 | US5082206 Hypersonic flight vehicle |
| 01/21/1992 | US5082050 Thermal restraint system for a circular heat exchanger |
| 01/15/1992 | EP0466501A2 Curved film cooling holes for gas turbine engine vanes |
| 01/15/1992 | EP0465554A1 High performance turbine engine |
| 01/15/1992 | EP0465531A1 Dual range air turbine starter |
| 01/15/1992 | EP0198077B1 Gas turbine engine |
| 01/14/1992 | US5080556 Thermal seal for a gas turbine spacer disc |
| 01/14/1992 | US5080303 Gearbox breather outlet |
| 01/14/1992 | US5079915 Heat protective lining for a passage in a turbojet engine |
| 01/14/1992 | US5079911 Gas-turbine power plant |
| 01/14/1992 | US5079910 Device for sealing inspection apertures |
| 01/14/1992 | CA2042266A1 Curved film cooling holes for gas turbine engine vanes |
| 01/09/1992 | WO1991019153A3 Thermal restraint system for a circular heat exchanger |
| 01/07/1992 | US5078359 Mounting means for a fuel control |
| 01/07/1992 | US5078342 Failure tolerant engine mounting |
| 01/07/1992 | US5078341 Inlet ramp for supersonic or hypersonic aircraft |
| 01/07/1992 | US5078324 Pressurized stem air blast fuel nozzle |
| 01/07/1992 | US5078173 Droop compensated bypass valve |
| 01/07/1992 | US5077967 Profile matched diffuser |
| 01/07/1992 | CA1293865C Wall having cooling passage |
| 01/01/1992 | CN1057508A Transportable electrical power generating system fueled by organic waste |
| 01/01/1992 | CN1057507A Projectile shield |
| 12/31/1991 | US5076591 Gas leakage seal |
| 12/31/1991 | US5076062 Gas-cooled flameholder assembly |
| 12/31/1991 | US5076052 Blocking device for fan ramjet engines |
| 12/31/1991 | US5076049 Pretensioned frame |
| 12/29/1991 | WO1992000183A1 A composite structural component |
| 12/26/1991 | WO1991019929A1 Mounting means for a fuel control |
| 12/26/1991 | WO1991019893A1 A transportable electrical power generating system fueled by organic waste |
| 12/25/1991 | CN1057315A Method and equipment for generating mechanical energy |
| 12/24/1991 | US5074748 Seal assembly for segmented turbine engine structures |
| 12/24/1991 | US5074111 Seal plate with concentrate annular segments for a gas turbine engine |
| 12/24/1991 | US5074109 Low pressure turbine rotor suspension in a twin hub turbo-engine |
| 12/19/1991 | DE4118061A1 Gas-turbine power plant - has heat-exchanger between water and air in supply system to burner |
| 12/19/1991 | CA2042198A1 Projectile shield |
| 12/18/1991 | EP0461447A1 Pressurised atomising nozzle |
| 12/17/1991 | US5073084 For a gas turbine engine of the type having an airstream flow |
| 12/17/1991 | US5073083 Turbine vane with internal cooling circuit |
| 12/17/1991 | CA1293198C Turbine engine noise suppression apparatus and methods |
| 12/11/1991 | EP0461026A1 Fuel injection assembly for turbomachine, including preevaporation chamber |
| 12/11/1991 | EP0460105A1 Bypass valve and visual indicator for a fuel system. |
| 12/10/1991 | US5070689 Power unit with stored energy |
| 12/10/1991 | CA1292951C Gas-turbine with link attachment of a sealing ring in a guide vane ring |
| 12/04/1991 | EP0459816A1 Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
| 12/04/1991 | EP0459815A1 Gas turbine engine fan duct base pressure drag reduction |
| 12/04/1991 | EP0459327A1 Gasturbinearrangement |
| 12/03/1991 | US5069034 Heat protective lining for an afterburner or transition duct of a turbojet engine |
| 12/03/1991 | US5069032 Gas turbine ignition system |
| 12/03/1991 | US5069031 Gas turbine engine stored energy combustion system |
| 12/02/1991 | CA2042201A1 Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
| 12/01/1991 | CA2042755A1 Gas turbine arrangement |
| 12/01/1991 | CA2039821A1 Turbine shroud clearance control assembly |
| 12/01/1991 | CA2039820A1 Nozzle band overhang cooling |
| 12/01/1991 | CA2039756A1 Stator having selectively applied thermal conductivity coating |
| 11/30/1991 | WO1991019153A2 Thermal restraint system for a circular heat exchanger |
| 11/30/1991 | CA2081099A1 Thermal restraint system for a circular heat exchanger |
| 11/27/1991 | EP0458453A2 Gas turbine engine thrust measurement |
| 11/27/1991 | CN1056563A Transpiration cooled throat section for low nox combustor and related process |
| 11/21/1991 | EP0457208A2 Starting device for the starter motor of a turbine engine |
| 11/21/1991 | EP0436685A4 An acoustic liner |
| 11/12/1991 | US5065073 Apparatus and method for providing ignition to a turbine engine |
| 11/12/1991 | US5064357 Fuel supply apparatus |
| 11/12/1991 | US5063733 Engine cooling system protection device |
| 11/12/1991 | CA2034465A1 Method and apparatus for automatic bypass operation |
| 11/12/1991 | CA2034391A1 Passive bypass valve assembly |
| 11/08/1991 | CA2039740A1 Exhaust assembly for a high speed civil transport aircraft engine |
| 11/06/1991 | EP0455487A1 Gas turbine combustors |
| 11/06/1991 | CN1014625B Temp. resistant fastener arrangement |
| 11/04/1991 | CA2040780A1 Transpiration cooled throat section for low nox combustor and related process |
| 10/29/1991 | US5060469 Integrated power unit control apparatus and method |
| 10/23/1991 | EP0453360A1 Aviation engine with high bypass ratio and of the type with front contra-rotating fan |
| 10/23/1991 | EP0453179A2 Electromagnetic damping of shaft motion |
| 10/22/1991 | US5058853 Vibration isolation mount system |
| 10/22/1991 | US5058617 Nacelle inlet for an aircraft gas turbine engine |
| 10/22/1991 | US5058378 Integrated turboramjet engine |
| 10/22/1991 | US5058377 Turboramjet engine |
| 10/19/1991 | CA2034328A1 Electromagnetic damping of shaft |
| 10/17/1991 | WO1991015667A1 Process and assembly for increasing the power of a gas turbine |
| 10/16/1991 | EP0452005A1 Gas turbine aircraft engine fuel delivery system |
| 10/16/1991 | EP0451945A1 An apparatus for and method of filtering a fluid |
| 10/16/1991 | CN1055429A Gas turbine flame detection system with refrected flame radiation attenuator |
| 10/16/1991 | CN1014350B Segmented rigid sliding seal |
| 10/15/1991 | US5056738 Damper assembly for a strut in a jet propulsion engine |
| 10/15/1991 | US5056335 Auxiliary refrigerated air system employing input air from turbine engine compressor after bypassing and conditioning within auxiliary system |
| 10/15/1991 | US5056307 Exhaust nozzle cooling utilizing total engine flow |
| 10/08/1991 | US5055014 Fluid supply conduit |
| 10/08/1991 | US5054996 Thermal linear actuator for rotor air flow control in a gas turbine |
| 10/08/1991 | US5054284 Combustion heated air turbine starter system |
| 10/08/1991 | US5054283 Turbine engine impingement assembly |