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