A stringer for an aircraft wing and a method of forming thereof

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/18 (2006.01)

Patent

CA 2652661

The present invention relates to a stringer (105) for an aircraft wing and a method of forming such a stringer in which the stringer (105) is formed form a single piece of material and has differential strength along its length.

La présente invention concerne une lisse (105) destinée à une aile d'avion et un procédé de formation d'une telle lisse dans lequel la lisse (105) est formée d'une seule pièce de matériau et présente un niveau de résistance différencié le long de sa longueur.

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