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