Shell element as part of an aircraft fuselage

B - Operations – Transporting – 29 – C

Patent

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Details

B29C 70/00 (2006.01) B64C 1/00 (2006.01) B64C 1/12 (2006.01)

Patent

CA 2671920

The present invention provides a shell element (4) as part of an aircraft fuselage, wherein the shell element (4) is formed as a curved sheet-like element and is at least partially or completely of CRP construction.

L'invention concerne un élément coque (4) constituant une partie d'un fuselage d'aéronef. Cet élément coque (4) se présente sous la forme d'un élément de type tôle incurvée et il est au moins partiellement ou totalement fabriqué à partir de plastique renforcé par fibres de carbone.

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