Aircraft component manufacturing tool and method

B - Operations – Transporting – 21 – D

Patent

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Details

B21D 26/02 (2006.01) B21D 37/02 (2006.01)

Patent

CA 2510154

A creep forming tool modifies the shape of an aircraft component (4) in the form of a wing skin portion. The tool (1) includes a shaped surface (3) defined by removable rib boards (6). The component (4) is forced against the shaped surface (3), via a reusable intermediate plate (12). The shape of the shaped surface (3) may be adjusted, if necessary, by replacing the rib boards with boards (6) of a different shape.

L'invention concerne un outil de formation de fluage conçu pour modifier la forme d'un élément aéronef (4) afin d'obtenir une portion de revêtement de voilure. L'outil (1) décrit dans cette invention comprend une surface formée (3) définie par des plateaux à nervures amovibles (6). L'élément (4) est poussé contre la surface formée (3), par l'intermédiaire d'une plaque intermédiaire réutilisable (12). La forme de la surface formée (3) peut être ajustée, si nécessaire, par remplacement des plateaux à nervures par des plateaux (6) présentant une forme différente.

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