Front landing-gear well

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United States of America Patent

PATENT NO 9505483
APP PUB NO 20140246542A1
SERIAL NO

14348093

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A forward part of an aircraft comprising a fuselage and a landing gear well housing a forward landing gear comprising a breaker strut designed to adopt an extended configuration when the landing gear is extended, configuration in which said breaker strut lies in a strut plane parallel to the transverse direction of the forward part. The forward part comprises a transverse beam resisting strut reactions located above the landing gear well and mounted on the fuselage at its two ends, the beam having a globally rectangular cross-section, in which the median plane parallel to the length of the rectangle is coincident with said strut plane.

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Patent Owner(s)

  • AIRBUS OPERATIONS SAS

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Durand, Yves Aussonne, FR 37 305
Guering, Bernard Montrabe, FR 130 837

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