Device for bracing a shell in an aircraft fuselage

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Reexamination Certificate

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Reexamination Certificate

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07124982

ABSTRACT:
A device for bracing a shell surface in an aircraft fuselage against deformations and consisting of a continuous profile that is arranged so as, after conformation, to be mounted against the shell surface. Notches are spaced at regular distances apart from each other in at least a portion of the profile. The notches extend through a base surface in the profile, and through an intermediate part perpendicular to the base surface. The notches are delimited upwardly by an upper surface that is not encompassed by the notches.

REFERENCES:
patent: 2233969 (1941-03-01), Woods
patent: 2389767 (1945-11-01), Dalton
patent: 2427853 (1947-09-01), Goodlett
patent: 4310132 (1982-01-01), Robinson et al.
patent: 5242523 (1993-09-01), Willden et al.
patent: 6114012 (2000-09-01), Amaoka et al.
patent: 6364250 (2002-04-01), Brinck et al.
patent: 6427945 (2002-08-01), Bansemir
patent: 198 44 035 (1999-11-01), None

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