| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 03/28/1991 | DE3930846A1 Aircraft air-intake system - has teeth on leading edge of hinging shutter |
| 03/26/1991 | US5001901 Hydraulic fluid circuit for full case hydraulic unit |
| 03/19/1991 | US5000399 Variable contour annular air inlet for an aircraft engine nacelle |
| 03/19/1991 | US5000386 Exhaust flaps |
| 02/19/1991 | US4994660 Axisymmetric vectoring exhaust nozzle |
| 02/19/1991 | US4993663 Engine of an aircraft |
| 02/12/1991 | US4991795 Two-stage supersonic inlet |
| 02/05/1991 | US4989807 S-shaped jet engine inlet diffuser |
| 01/30/1991 | EP0409911A1 Vtol aircraft |
| 01/09/1991 | EP0407221A1 Variable air intake |
| 01/09/1991 | CN1048429A Infrared suppressor for gas turbine engine |
| 01/02/1991 | EP0406155A1 Infrared suppressor for a gas turbine engine |
| 12/25/1990 | US4979699 Flight control augmentation inlet device |
| 12/18/1990 | US4978071 For directing exhaust flow of the nozzle |
| 12/01/1990 | CA2012248A1 Hybrid laminar flow nacelle |
| 11/13/1990 | US4969535 Acoustic liner |
| 10/24/1990 | CN1046370A Axisymmetric vectoring exhaust nozzle |
| 10/11/1990 | DE3619652C1 Jet aircraft manoeuvring aid - has three movable flaps each suspended from four point linkage |
| 10/11/1990 | CA2013931A1 Nozzle with thrust vectoring in the yaw direction |
| 10/10/1990 | CN1046019A Nozzle with thrust vectoring in yaw direction |
| 09/12/1990 | EP0387123A1 Thermic protection liner for hot pipe of turbo-jet engine |
| 09/05/1990 | EP0385294A1 Turbojet |
| 08/23/1990 | WO1990009313A1 Vtol aircraft |
| 06/19/1990 | US4934600 Exhaust nozzle thermal distortion control device |
| 06/19/1990 | US4934412 Layers of reinforced cured polyimide resin with an inner layer of foil |
| 06/14/1990 | WO1990006440A1 Integrated starting system |
| 05/29/1990 | US4928480 For a gas turbine engine |
| 05/08/1990 | US4922712 Thrust reverser for high bypass turbofan engine |
| 05/08/1990 | US4922711 Thrust reversing system for high bypass fan engines |
| 05/01/1990 | US4922119 Integrated starting system |
| 04/26/1990 | DE3835669A1 Air inlet for high-performance aircraft |
| 04/26/1990 | DE3835668A1 Controllable air inlet on high-performance aircraft |
| 04/26/1990 | DE3835667A1 Air-inlet controller for high-performance aircraft |
| 04/26/1990 | DE3835665A1 Controller for an air inlet for high-performance aircraft |
| 04/26/1990 | DE3835664A1 Variable air inlet for high-performance aircraft |
| 04/26/1990 | DE3835663A1 Device for controlling an air inlet on high-performance aircraft |
| 04/24/1990 | US4919364 Propulsion system for hypersonic flight |
| 04/17/1990 | US4917302 High temperature flexible seal |
| 04/05/1990 | WO1990003309A1 Ducted fan turbine engine |
| 04/04/1990 | EP0361901A1 Ducted fan turbine engine |
| 03/14/1990 | EP0358348A2 Aft spill ramjet |
| 03/14/1990 | EP0358347A2 Variable air intake ramps for aerospace vehicles |
| 03/06/1990 | CA1266382A1 Air inlet filter for gas turbine engine |
| 02/28/1990 | EP0356280A1 Bidimensional and symmetrical supersonic and hypersonic air intake for the combustion air of an aircraft engine |
| 02/13/1990 | US4899958 Air intake system of an aircraft |
| 02/07/1990 | EP0354103A1 Bidimensional and asymmetrical supersonic air intake for the combustion air of an aircraft engine |
| 02/07/1990 | EP0353288A1 Process and apparatus for filling a constant speed drive |
| 01/23/1990 | US4895219 Fill valve for liquid containing device |
| 01/23/1990 | US4895192 Process and apparatus for filling a constant speed drive |
| 01/03/1990 | CN1006320B Gas-turbine engine |
| 12/19/1989 | US4887424 Propfan turbine engine |
| 12/13/1989 | EP0345834A1 Thrust reversing system for high bypass fan engines |
| 11/28/1989 | US4883148 Fill valve for liquid containing device |
| 11/21/1989 | US4881367 Gas turbine engine |
| 09/12/1989 | US4865268 Jet engine nacelle |
| 09/12/1989 | US4864820 Exhaust nozzle |
| 09/06/1989 | EP0330782A1 Particle separator for use with turbines |
| 08/01/1989 | US4852805 Hybrid thrust reverser cascade basket and method |
| 08/01/1989 | CA1257971A1 Gas turbine engine nacelle |
| 07/25/1989 | US4850535 Variably convergent exhaust nozzle for a model ducted fan unit |
| 07/04/1989 | US4844382 Dual turning vane air inlet assembly |
| 06/29/1989 | WO1989005757A1 Process and apparatus for filling a constant speed drive |
| 06/20/1989 | US4840329 Aircraft with stowable vectorable nozzle and ejector thrust augmentation |
| 06/06/1989 | US4836469 System for reducing aircraft noise and hush kit |
| 05/30/1989 | US4833879 Turbo-engine guard |
| 05/16/1989 | US4830312 Airplane, preferably a helicopter |
| 05/09/1989 | US4828173 Area controlled, thrust vectoring vane cascade |
| 05/02/1989 | US4826106 Advanced composite aircraft cowl |
| 05/02/1989 | US4825644 Ventilation system for a nacelle |
| 04/11/1989 | US4819876 For a gas turbine engine powered aircraft |
| 04/04/1989 | US4817756 Quiet nacelle system and hush kit |
| 03/07/1989 | CA1250750A1 Aircraft engine inlet |
| 02/21/1989 | US4805840 Thrust deflectors for propulsion nozzles of turbomachines |
| 02/14/1989 | US4804155 VTOL aircraft |
| 02/14/1989 | US4803756 Hinge pin retaining assembly having an integral slotted plate and hinge pin |
| 01/31/1989 | US4801087 Exhaust nozzle for a gas turbine engine |
| 01/24/1989 | US4799633 For use on an aircraft |
| 01/04/1989 | EP0298010A2 Divergent flap actuation system for a two-dimensional exhaust nozzle |
| 01/04/1989 | CN1030122A Divergent flap actuation system for two-dimensional exhaust nozzles |
| 12/07/1988 | CN88103093A Area controlled thrust vectoring vane cascade |
| 11/29/1988 | US4787421 Flow path defining means and method of making |
| 11/23/1988 | EP0292419A2 Area controlled, thrust vectoring vane cascade |
| 11/23/1988 | EP0291523A1 Process and device for camouflaging power unit inlets |
| 11/22/1988 | US4786016 Annular nacelle adapted to surround a gas turbine engine |
| 11/16/1988 | CN88102721A Exhaust gas nozzle including cooling air diverter valve |
| 11/09/1988 | EP0290371A1 Exhaust gas nozzle including a cooling air diverter |
| 11/02/1988 | CN88101774A Gas-turbine engine |
| 10/26/1988 | CN88101862A Flap support arrangement |
| 10/18/1988 | US4778109 Adjustable two dimensional nozzle for aircraft jet engines |
| 10/12/1988 | EP0286567A1 Flap support arrangement |
| 09/28/1988 | EP0283578A2 Aircraft, in particular helicopter |
| 08/16/1988 | US4763858 Deflectable jet engine inlet |
| 08/02/1988 | US4760978 Ice-free screen for protecting engines from damage caused by foreign bodies in the intake airstream |
| 07/27/1988 | EP0275757A1 Bidimensional, controllable jet nozzle |
| 07/26/1988 | US4759513 Noise reduction nacelle |
| 07/07/1988 | DE3713875C1 Air inlet on aircraft |
| 07/05/1988 | US4754924 Variable geometry nozzle |
| 06/16/1988 | WO1988004479A1 Process and device for camouflaging power unit inlets |
| 06/16/1988 | DE3641289A1 Verfahren und vorrichtung zur radartarnung von triebwerkseinlaeufen Method and device for radar camouflage of triebwerkseinlaeufen |
| 06/07/1988 | US4749151 For use in an aircraft |