| Patents for F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699) |
|---|
| 06/28/1990 | DE3841174A1 Propeller fan |
| 06/19/1990 | US4934600 Exhaust nozzle thermal distortion control device |
| 06/19/1990 | US4934481 Arrangement for suppressing jet engine noise |
| 06/05/1990 | US4930308 Double-flow turboshaft engine with variable confluent nozzle |
| 06/05/1990 | US4930307 Ducted fan gas turbine engine with surge controller |
| 05/29/1990 | US4928482 Control of high compressor vanes and fuel for a gas turbine engine |
| 05/22/1990 | US4926633 Coolant pressure regulating apparatus |
| 05/22/1990 | CA1269334A1 Compact muffler apparatus and associated methods |
| 05/16/1990 | EP0368725A1 Thrust reverser for a jet-engine provided with deviator flaps with mini-nozzles |
| 05/09/1990 | EP0366829A1 Jet-engine thrust-reversers |
| 05/08/1990 | US4923371 Wall having cooling passage |
| 05/08/1990 | US4922713 Turbojet engine thrust reverser with variable exhaust cross-section |
| 05/08/1990 | US4922712 Thrust reverser for high bypass turbofan engine |
| 05/08/1990 | US4922711 Thrust reversing system for high bypass fan engines |
| 05/03/1990 | WO1990004714A1 Sustainer propulsion system |
| 05/01/1990 | US4920742 Heat shield for gas turbine engine frame |
| 04/25/1990 | EP0365425A1 Thrust reverser with balanced pivotable doors |
| 04/24/1990 | US4919364 Propulsion system for hypersonic flight |
| 04/18/1990 | EP0364360A1 Method for producing composite parts composed of a fleece and a reinforcement |
| 04/17/1990 | US4917302 High temperature flexible seal |
| 04/17/1990 | US4916895 Thrust reverse for a turbofan engine |
| 04/11/1990 | EP0363301A1 Control system for gas turbine engines |
| 04/10/1990 | US4914905 Air deflector for a turbofan engine thrust reverser |
| 04/04/1990 | EP0362054A1 Gas injection device for a combined turbo-stato-rocket thruster |
| 04/04/1990 | EP0362052A1 Nozzle structure for a combined turbo-static rocket |
| 04/04/1990 | EP0362051A1 Bidimensional ejection nozzle for a turbine and its control system |
| 04/03/1990 | US4913354 Jet pipe for jet propulsion in aircraft |
| 03/20/1990 | US4909442 Actuation system for a blocker door in a jet engine nacelle |
| 03/20/1990 | US4909346 Jet engine noise suppression system |
| 03/20/1990 | US4909031 Combined multi-speed jet engine for the drive of airplanes and space vehicles |
| 03/13/1990 | US4907743 Assembly of two bodies having distinctly different coefficients of expansion |
| 03/07/1990 | EP0357494A1 Thrust reverser with auxiliary flaps for a jet engine |
| 02/13/1990 | US4899539 Flow mixer and flame stabilizer for a turbofan engine |
| 01/30/1990 | US4896846 Superagile tactical fighter aircraft and method of flying it in supernormal flight |
| 01/30/1990 | CA1264951A1 Exhaust system including protective arrangements |
| 01/24/1990 | EP0352171A1 Thrust reverser for a bypass jet engine with moving deviation flaps |
| 01/23/1990 | US4895378 For preventing leakage of hot gases |
| 01/23/1990 | US4894985 Thrust reverser with movable deflector |
| 01/16/1990 | US4893847 Bearing seal for universal ball joint |
| 01/09/1990 | US4892254 Aircraft engine interface fairing support |
| 01/04/1990 | DE3822065A1 Flow guiding device for jet engine nozzles |
| 12/28/1989 | WO1989012741A1 Vane-type thrust vectoring nozzle |
| 12/19/1989 | US4887663 Hot gas duct liner |
| 12/13/1989 | EP0345834A1 Thrust reversing system for high bypass fan engines |
| 12/06/1989 | EP0345200A1 Cooling means for augmentor liner |
| 12/06/1989 | EP0344877A1 Heat shield for gas turbine engine frame |
| 12/05/1989 | US4884748 Fairing flap arrangement |
| 11/28/1989 | CA1263242A1 Gas turbine outlet arrangement |
| 11/07/1989 | US4878618 Wear resistant, self-damping clamp assembly |
| 11/07/1989 | US4878617 Triple axis thrust vectoring exhaust nozzle |
| 10/31/1989 | US4876851 Infrared radiation screening device |
| 10/25/1989 | EP0338869A1 Turbine thrust reverser |
| 10/11/1989 | CN1036245A Wall having cooling passage |
| 10/04/1989 | EP0335481A1 Wall having cooling passage |
| 09/27/1989 | EP0333919A1 Joint connection for annular flanges |
| 09/27/1989 | CN1035878A Joint connection for annular flanges |
| 09/19/1989 | US4866942 Augmentor curtain liner for equalizing pressure therein |
| 09/12/1989 | US4865256 Turbojet engine having a thrust reverser door and variable exhaust cross-section |
| 09/12/1989 | US4864820 Exhaust nozzle |
| 09/12/1989 | US4864819 Exhaust system including protective arrangements |
| 09/12/1989 | US4864818 Augmentor liner construction |
| 08/29/1989 | US4860956 Thrust reverser for aircraft jet engine and aircraft engine equipped with said thrust reverser |
| 08/22/1989 | US4858721 Acoustic panel for sound insulating linings of gas ducts |
| 08/22/1989 | US4858430 Thrust reverser for a turbofan engine |
| 08/08/1989 | US4854122 Augmentor curtain liner assembly for sharing tensile loading |
| 08/02/1989 | EP0326448A1 Mixing device with a variable section for the different jets of a jet engine |
| 08/01/1989 | US4852805 Hybrid thrust reverser cascade basket and method |
| 07/25/1989 | US4850535 Variably convergent exhaust nozzle for a model ducted fan unit |
| 07/18/1989 | US4848664 Yaw thrust vectoring exhaust nozzle |
| 07/18/1989 | US4848081 Cooling means for augmentor liner |
| 07/04/1989 | US4843814 Assembly for producing a propulsive force |
| 06/28/1989 | EP0321993A2 Thrust reverser for high bypass jet engines |
| 06/20/1989 | US4840329 Aircraft with stowable vectorable nozzle and ejector thrust augmentation |
| 06/13/1989 | US4838584 Quick disconnect duct coupler |
| 06/06/1989 | US4836469 System for reducing aircraft noise and hush kit |
| 06/06/1989 | US4836451 Yaw and pitch convergent-divergent thrust vectoring nozzle |
| 06/06/1989 | US4835961 Fluid dynamic pump |
| 05/17/1989 | EP0316233A1 Assembly method for two parts having different thermal expansion coefficients |
| 05/10/1989 | EP0315524A1 Cascade-type thrust reverser for a jet engine, combined with a variable outlet area nozzle |
| 05/10/1989 | EP0315522A1 Jet engine nozzle with thrust reversing ports and an adjustable outlet area |
| 05/10/1989 | EP0315486A2 Aircraft engine frame construction |
| 05/09/1989 | US4828173 Area controlled, thrust vectoring vane cascade |
| 05/03/1989 | EP0164337B1 Translating jet engine nozzle plug |
| 05/03/1989 | DE3734624A1 Propeller fan |
| 05/02/1989 | US4827248 Proximity sensor with automatic gap control |
| 05/02/1989 | US4826106 Advanced composite aircraft cowl |
| 05/02/1989 | US4825644 Ventilation system for a nacelle |
| 04/26/1989 | EP0313464A1 Transition channel for a jet engine |
| 04/26/1989 | EP0313194A1 Interturbine duct |
| 04/26/1989 | EP0165988B1 Power drive unit |
| 04/25/1989 | US4823547 Gas turbine engine |
| 04/18/1989 | US4821979 Variable area exhaust nozzle for a gas turbine engine |
| 04/11/1989 | US4820097 Fastener with airflow opening |
| 04/11/1989 | US4819876 For a gas turbine engine powered aircraft |
| 04/11/1989 | US4819425 Primary-secondary ventilated flow mixer nozzle for high bypass turbo fan jet propulsion system |
| 04/05/1989 | EP0310497A1 Gas turbine thrust-reversing doors having a flush interior surface |
| 04/05/1989 | CN1032218A Linkage for area controlled, thrust vectoring vane cascade |
| 04/05/1989 | CN1032217A Area controlled, thrust vectoring vane cascade with nutating control vane |
| 04/04/1989 | US4817871 Control system for turbojet engine nozzle flaps |
| 04/04/1989 | US4817378 Gas turbine engine with augmentor and variable area bypass injector |