Rigid framework for aircraft engine mounting structure and...

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Details

C060S796000, C060S797000, C248S554000, C248S557000

Reexamination Certificate

active

07931232

ABSTRACT:
A rigid structure of a suspension pylon for an aircraft engine, which is in a shape of a box closed by first and second box side panels. The structure includes inter-rib spaces, each space delimited by two directly consecutive box transverse ribs. For each inter-rib space forming part of a group including at least three arbitrary and directly consecutive inter-rib spaces, a single access opening is provided on the side panels, the openings arranged alternately on the first and second side panels.

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patent: 2007/0120010 (2007-05-01), Huggins et al.
patent: 2007/0228213 (2007-10-01), Diochon et al.
patent: 0 429 100 (1991-05-01), None

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