B - Operations – Transporting – 29 – C
Patent
B - Operations, Transporting
29
C
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.
Dolzinski Wolf-Dietrich
Herrmann Ralf
Kolax Michael
Wentzel Hans-Peter
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
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