AIRCRAFT NACELLE PROVIDED WITH AT LEAST ONE THRUST REVERSAL DEVICE COMPRISING AT LEAST ONE LONGITUDINAL DEFLECTOR, AIRCRAFT COMPRISING AT LEAST ONE PROPULSION ASSEMBLY COMPOSED OF SUCH A NACELLE

Number of patents in Portfolio can not be more than 2000

United States of America

APP PUB NO 20250092847A1
SERIAL NO

18887483

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Abstract

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An aircraft nacelle provided with a thrust reversal device which comprises at least one diversion system which is configured to divert, in the activated state, an airflow channeled in the nacelle toward a lateral opening of the nacelle, at least one orientation system comprising at least one transverse deflector which is configured to orientate the airflow diverted by the diversion system in the radial directions and toward the upstream end of the nacelle, and at least one longitudinal deflector which is secant to the transverse deflector(s) and which is oriented in a direction which forms an angle of less than 25° with the longitudinal direction.

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Patent Owner(s)

Patent OwnerAddress
AIRBUS OPERATIONS SASTOULOUSE FRANCE

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
BOURDEAU, Christophe TOULOUSE, FR 12 35
CHELIN, Frédéric TOULOUSE, FR 22 117
SCHOLZ, Olivier TOULOUSE, FR 4 0

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