| Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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| 03/30/1995 | WO1995008473A1 A duct cover for directing a fluid therethrough and a method for making the same |
| 03/30/1995 | CA2172151A1 A duct cover for directing a fluid therethrough and a method for making the same |
| 03/28/1995 | US5400984 Thermal anti-icing of aircraft structures |
| 03/14/1995 | US5397077 For a supersonic aircraft engine |
| 03/14/1995 | CA1334723C Ducted fan turbine engine |
| 02/21/1995 | US5390879 Jet pipe for supporting a thrust reverser for aircraft jet engines |
| 12/06/1994 | US5369954 Turbofan engine bypass and exhaust system |
| 11/30/1994 | EP0626039A1 Exhaust eductor cooling system. |
| 10/25/1994 | US5357742 Turbojet cooling system |
| 10/06/1994 | DE4400621A1 Pusher-type propeller drive for aircraft, land vehicles or water craft |
| 10/05/1994 | CN1026146C Area controlled, thrust vectoring vane cascade |
| 10/04/1994 | US5351888 Multi-axis vectorable exhaust nozzle |
| 10/04/1994 | US5351476 Nacelle cooling and ventilation system |
| 09/29/1994 | DE4310017A1 Transport aircraft having a blunt tail |
| 08/16/1994 | US5337975 Breathing system for hypersonic aircraft |
| 08/11/1994 | DE4303548A1 Insulation driver |
| 06/16/1994 | DE4242332A1 Noise reflectors for aircraft of all types and sizes - are of dish shape and attached inclined upwards on side underneath engine to send sounds into sky and may have holes for water run=off |
| 06/07/1994 | US5317867 Changeover valve |
| 04/27/1994 | EP0593987A1 Variable square air intake duct |
| 04/12/1994 | US5301901 Telescoping centerbody wedge for a supersonic inlet |
| 04/05/1994 | US5299760 S-duct for a turbo-jet aircraft engine |
| 03/09/1994 | EP0586000A1 Non-metallic thermally conductive honeycomb thrust reverser inner wall |
| 02/09/1994 | EP0582522A1 Mounting device of a turbine engine on an aircraft structure |
| 02/08/1994 | US5284012 Nacelle cooling and ventilation system |
| 02/02/1994 | CN1081493A S-duct for a turbo-jet aircraft engine |
| 01/25/1994 | US5280704 Lock for a thrust reverser mechanism, a thrust reverser mechanism, and a thrust reverser |
| 01/20/1994 | WO1994001735A1 S-duct for a turbo-jet aircraft engine |
| 01/20/1994 | DE4223413A1 Intake system for super- and hypersonic aircraft - has articulated members, associated with swivel elements, actuated by toggle lever joints |
| 12/07/1993 | CA1324999C Bodies with reduced surface drag |
| 11/30/1993 | US5265408 Exhaust eductor cooling system |
| 09/15/1993 | CN1022124C Axisymmetric vectoring exhaust nozzle |
| 09/08/1993 | EP0558726A1 Thermal anti-icing of aircraft structures. |
| 09/01/1993 | CN1021987C Infrared suppressor for gas turbine engine |
| 08/19/1993 | WO1993016280A1 Exhaust eductor cooling system |
| 08/17/1993 | US5236152 Heat exchanging to cool vehicle surfaces and produce fuel from hydrocarbons concurrently |
| 07/27/1993 | US5230603 Control of flow instabilities in turbomachines |
| 07/13/1993 | US5226455 Variable geometry duct seal |
| 06/23/1993 | EP0547266A1 Fighter configuration, with inlets on the upper back sides of the fuselage, and canards acting as airflow straighteners for the inlets |
| 06/02/1993 | EP0544482A1 Changeover valve |
| 04/27/1993 | USRE34235 Sealing plug |
| 04/14/1993 | EP0536954A1 A lock for a thrust reverser mechanism, a thrust reverser mechanism, and a thrust reverser |
| 03/31/1993 | CN1020207C Two-dimensional exhaust nozzles with divergent flap actuation system |
| 03/30/1993 | US5197855 Engine exhaust/blade interaction noise suppression |
| 03/30/1993 | US5197694 Overwing thrust reverser |
| 03/21/1993 | WO1993006005A1 Thermal anti-icing of aircraft structures |
| 03/21/1993 | CA2095530A1 Thermal anti-icing of aircraft structures |
| 03/01/1993 | CA2072417A1 Aircraft engine nacelle having circular arc profile |
| 01/12/1993 | US5177957 Propfan turbine engine |
| 12/29/1992 | US5174524 Cooling system for high speed aircraft |
| 12/02/1992 | EP0516468A2 Jet engine fan nacelle |
| 12/01/1992 | US5167119 For use on an aircraft |
| 12/01/1992 | US5167117 Method and apparatus for cooling an airplane engine |
| 12/01/1992 | CA2065637A1 Jet engine fan nacelle |
| 11/19/1992 | EP0514119A1 Nacelle cooling and ventilation system |
| 11/17/1992 | CA2065678A1 Nacelle cooling and ventilation system |
| 10/20/1992 | US5156362 Jet engine fan nacelle |
| 10/20/1992 | CA1308925C Gas turbine engine |
| 09/22/1992 | CA1307672C Turbo-engine guard |
| 09/08/1992 | US5145126 Engine nacelle |
| 08/11/1992 | US5136839 Ducted fan turbine engine |
| 07/22/1992 | CN1017539B Flap support arrangement |
| 07/14/1992 | US5129446 Air/liquid heat exchanger |
| 06/16/1992 | CA1303368C Separator having multiple particle extraction passageways |
| 06/09/1992 | US5120005 Jet engine |
| 06/09/1992 | CA1302841C Diffuser |
| 06/02/1992 | US5117630 Pivoting door thrust reverser |
| 05/27/1992 | EP0487241A1 Heat exchange system |
| 05/26/1992 | US5116251 Inlet system for supersonic or hypersonic aircraft |
| 05/26/1992 | US5116001 Variable air intake |
| 05/20/1992 | CA2048807A1 Self-powered heat exchange system |
| 05/19/1992 | US5114097 Aircraft |
| 05/19/1992 | US5113669 Self-powered heat exchange system |
| 05/13/1992 | CN1061119A Liquid cooled electric generating apparatus and method for filling liquid cirulation system therein |
| 05/06/1992 | EP0484041A1 Liquid cooled electric generating apparatus and method for filling a liquid circulation system therein |
| 05/05/1992 | US5110069 Single pivot overwing thrust reverser |
| 05/01/1992 | CA2053450A1 Liquid cooled electric generating apparatus and method for filling a liquid circulation system therein |
| 03/24/1992 | US5097892 Air/liquid heat exchanger with ram pressure evaporative cooling |
| 02/18/1992 | US5088660 Bleed stability door |
| 02/18/1992 | US5088277 Aircraft engine inlet cowl anti-icing system |
| 01/21/1992 | US5082206 Hypersonic flight vehicle |
| 01/15/1992 | EP0466316A2 Gas turbine engine thrust reverser control |
| 01/14/1992 | US5080303 Gearbox breather outlet |
| 01/14/1992 | US5079915 Heat protective lining for a passage in a turbojet engine |
| 01/07/1992 | US5078341 Inlet ramp for supersonic or hypersonic aircraft |
| 10/29/1991 | US5060472 Insulated cooling liner |
| 10/22/1991 | US5058828 Overwing thrust reverser |
| 10/22/1991 | US5058617 Nacelle inlet for an aircraft gas turbine engine |
| 10/15/1991 | US5056307 Exhaust nozzle cooling utilizing total engine flow |
| 10/08/1991 | US5054998 Thrust reversing system for counter rotating propellers |
| 10/08/1991 | US5054281 Gas turbine engine compartment vent system |
| 09/18/1991 | CN1013982B Exhaust gas nozzle including cooling air diverter valve |
| 08/27/1991 | US5042746 Nozzle assembly for aircraft |
| 08/27/1991 | US5042745 Vectoring exhaust gases |
| 08/24/1991 | CA2034439A1 Variable contour annular air inlet for an aircraft engine nacelle |
| 08/07/1991 | EP0439923A1 Gearbox breather outlet |
| 07/23/1991 | US5033693 Single-piece, flexible inlet ramp |
| 06/25/1991 | US5026004 Variable air intake ramps for aerospace vehicles |
| 05/14/1991 | US5014933 Translating lip aircraft cowling structure adapted for noise reduction |
| 04/09/1991 | US5005782 Two dimensional and asymmetric supersonic air intake for the combustion air of an aircraft engine |
| 04/02/1991 | US5004187 Symmetrical, two dimensional, supersonic and hypersonic air intake for the combustion air of an aircraft engine |