Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
08/2002
08/29/2002WO2002042150B1 Aircraft deicer
08/28/2002EP1234764A2 Aircraft infrared suppressor
08/28/2002EP0888497B1 System and method for diverting boundary layer air
08/27/2002US6440521 Method for transferring heat in an aircraft engine thrust reverser
08/27/2002US6439504 System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system
08/27/2002CA2296833C Turbo fan engine nacelle exhaust system with concave primary nozzle plug
08/22/2002US20020112535 Test bed for a thrust reverser
08/21/2002EP1232944A1 Deicing method with forced circulaion for jet engine intake fairing and device for the implementation of said method
08/06/2002US6427801 Apparatus for reducing noise in the jet engine
08/06/2002US6427434 Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit
08/01/2002US20020100837 Aircraft propulsive power unit
08/01/2002DE10102252A1 Vorrichtung zum zumindestens teilweisen Abdecken der Lufteinströmöffnung eines Stahltriebwerkes eines Flugzeuges Means for at least partially covering the air inflow of a steel engine of an airplane
07/2002
07/18/2002US20020092948 Apparatus and method for reducing jet engine noise
07/04/2002US20020084382 Aircraft deicer
07/03/2002EP0865570B1 Noise suppression system for a jet engine
06/2002
06/20/2002DE10060548A1 Exhaust gas diffuser for gas-turbine-powered aircraft
06/19/2002EP1215118A1 Test bench for thrust reverser
06/18/2002US6405977 Modular air intake duct for aircraft
06/06/2002WO2002044105A1 Porous sound absorbing material and method of manufacturing the material
06/05/2002EP0998628B1 Turning vane arrangement for ir suppressors
06/04/2002US6398129 Throat configuration for axisymmetric nozzle
05/2002
05/30/2002WO2002042150A1 Aircraft deicer
05/23/2002US20020061110 Actively-controlled sound absorption panel system using movement-controlled reflective plate
05/22/2002EP1206384A2 Supersonic external-compression diffuser and method for designing same
05/22/2002EP1206383A1 Air intake protection device for aircraft engines
05/21/2002US6390414 Self-adjusting air intake
05/07/2002US6381950 Engine nozzle arrangement for an aircraft
04/2002
04/25/2002US20020047070 Method and apparatus for aircraft inlet ice protection
04/24/2002EP0923488B1 Detachable integral aircraft tailcone and power assembly
04/16/2002US6371411 Method and apparatus for aircraft inlet ice protection
04/11/2002WO2002029224A1 Air intake guard for engine
04/10/2002EP1195512A2 Flow blocking exhaust nozzle
04/09/2002US6367739 Compound exhaust system
04/09/2002US6367738 Aerobatic aircraft
04/03/2002EP1193682A1 Acoustic sandwich panel with no septum and apparatus and method for suppressing noise in a turbojet nozzle
04/03/2002EP1192348A1 Engine nozzle arrangement for an aircraft
03/2002
03/28/2002WO2001062592A3 Inlet vortex bustor and ice protector for auxiliary power units
03/28/2002US20020036241 Throat configuration for axisymmetric nozzle
03/27/2002CN1341808A Power device
03/26/2002US6360989 Nacelle assembly for a gas turbine engine
03/26/2002US6360528 Chevron exhaust nozzle for a gas turbine engine
03/26/2002US6360527 Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ring
03/19/2002US6357672 Sealing means for a multi-axis nozzle
03/07/2002WO2001054981A3 Propulsion module
03/06/2002CN1080228C Turbojet pod
03/05/2002US6352211 Flow blocking exhaust nozzle
02/2002
02/26/2002US6349899 Aircraft auxiliary air intake with ram and flush opening door
02/21/2002WO2002014149A1 Air intake for large-size nacelle with enhanced transportability
02/13/2002EP1179473A1 Air intake with improved transportability for an aircraft engine nacelle of large dimensions
01/2002
01/23/2002EP1174341A1 Aircraft jet engine nacelle with an enhanced rear ejection block with common nozzle
01/17/2002US20020006333 Aeroengine nacelle afterbodies
01/17/2002US20020005038 Method and apparatus for the cooling of jet-engine turbine casings
01/02/2002EP1117588A4 Aircraft engine air intake system
12/2001
12/20/2001DE10019437A1 Verfahren und Vorrichtung zum Kühlen der Gehäuse von Turbinen von Strahltriebwerken Method and apparatus for cooling the housing of turbines of jet engines
12/19/2001EP1163151A1 Modular air intake duct for aircraft
12/11/2001US6327846 Universal-joint vectoring system for a turbojet-engine exhaust nozzle
11/2001
11/06/2001US6311928 Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
10/2001
10/30/2001US6308915 Detachable integral aircraft tailcone and power assembly
10/24/2001EP1148221A2 Method and device to cool the casings of turbojet engines
10/18/2001WO2001019675A3 Supersonic external-compression diffuser and method for designing same
10/17/2001EP0991860B1 Multi-stage mixer/ejector for suppressing infrared radiation
09/2001
09/25/2001US6293494 Aircraft air inlet with airflow guide to prevent flow separation
09/18/2001US6290173 Aircraft cracked stack prevention apparatus and method
09/18/2001US6289665 Aircraft air conditioner energy recovery method
09/04/2001US6282881 Cooling system for a turbomachine speed reducer
08/2001
08/30/2001WO2001062592A2 Inlet vortex bustor and ice protector for auxiliary power units
08/21/2001US6276632 Axi-symmetric mixed compression inlet with variable geometry centerbody
08/02/2001WO2001054981A2 Propulsion module
08/02/2001WO2001054978A1 Improved aerobatic aircraft
07/2001
07/31/2001US6267327 Coupling system for connecting a gas turbine engine to an aircraft mounted exhaust system
07/25/2001EP1117588A1 Aircraft engine air intake system
07/24/2001US6264137 Inlet vortex bustor and ice protector for auxiliary power units
07/17/2001US6260794 Dolphin cascade vane
07/17/2001US6260567 Mission adaptive inlet
06/2001
06/27/2001EP1111226A1 Hot air exhaust device for a jet engine air intake fairing with de-icing circuit
06/21/2001US20010003897 Device for discharging hot air for a jet engine air inlet cowl, with a deicing circuit
06/13/2001CN2434223Y Device for preventing flying birds into jet engine
06/12/2001US6244539 Detachable integral aircraft tailcone and power assembly
05/2001
05/30/2001EP1103462A1 Method and apparatus for aircraft inlet ice protection
05/29/2001US6237325 Bypass turbojet-engine cowling comprising an electrically grounded displaceable component
05/15/2001US6231006 Mission adaptive inlet
04/2001
04/25/2001EP0739291B1 Engine exhaust gas deflection system
04/17/2001US6216980 System for closing a pivoting thrust reverser door
04/10/2001US6212877 Vectoring ring support and actuation mechanism for axisymmetric vectoring nozzle with a universal joint
04/03/2001US6210773 Non-metallic thermally conductive honeycomb thrust reverser inner wall
04/03/2001US6209821 Apparatus and method for measuring air temperature ahead of an aircraft for controlling a variable inlet/engine assembly
03/2001
03/22/2001WO2001019675A2 Supersonic external-compression diffuser and method for designing same
03/21/2001EP1084951A2 A nacelle assembly for a gas turbine engine
03/20/2001US6202403 Core compartment valve cooling valve scheduling
03/13/2001US6199795 Twin engine aircraft
02/2001
02/28/2001EP1077871A1 Ir suppressor
02/22/2001WO2001012506A1 Protection device for the air inlet of aircraft turbines
02/13/2001US6185926 Turbojet engine thrust reverser and exhaust nozzle assembly
01/2001
01/31/2001EP1071609A1 Jet engine exhaust nozzle
01/31/2001EP1071608A2 Biplanar scarfed nacelle inlet
01/30/2001US6179251 Thin inlet lip design for low drag and reduced nacelle size
01/30/2001US6179249 Turbojet pod with laminar flow
01/30/2001US6178740 Turbo fan engine nacelle exhaust system with concave primary nozzle plug
01/18/2001WO2001004485A1 Engine nozzle arrangement for an aircraft
01/09/2001US6170780 Twin engine aircraft
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