Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction

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United States of America Patent

PATENT NO 8864066
APP PUB NO 20110309189A1
SERIAL NO

13131999

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Abstract

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An engine assembly for an aircraft, including a rigid structure including a box rib extension protruding from a box of the structure, in a line of separation, towards a fuselage of the aircraft. The extension supports a first attachment in a position separating it from a second attachment in the line of separation. The first and second attachments enable the moment being exerted in a lengthways direction of the turbine engine to be transmitted jointly.

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Patent Owner(s)

  • AIRBUS OPERATIONS LIMITED;AIRBUS OPERATIONS SAS

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Marche, Jacques Hervé Toulouse, FR 8 36

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