B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01)
Patent
CA 2742404
The present invention provides a shell component for an aircraft or spacecraft. The shell component comprises a skin panel, a plurality of stringers which are arranged on the skin panel, a former which comprises a fibre composite material and is arranged over the stringers so as to cross said stringers, and a former connection structure which comprises a ductile material and a plurality of foot portions fixed to the skin panel. The foot portions each transition integrally into a shoulder portion fixed to the former over an associated fixing span, the fixing spans associated with the foot portions extending along the former substantially continuously over the stringers.
L'invention concerne un élément de coque pour un aéronef ou un vaisseau spatial. L'élément de coque selon l'invention comprend une peau, une pluralité de lisses placées sur la peau, un cadre qui comporte un matériau composite fibreux et qui est placé au-dessus des lisses en les croisant, ainsi qu'une structure de liaison de cadre qui comporte un matériau ductile et une pluralité de parties de pied fixées à la peau. Les parties de pied évoluent chacune d'un seul tenant en une partie d'épaulement fixée au cadre sur une étendue de fixation correspondante, les étendues de fixation correspondant aux parties de pied s'étendant sur les lisses pratiquement sans lacune le long du cadre.
Airbus Operations Gmbh
Oyen Wiggs Green & Mutala Llp
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