Societe Lorraine De Construction Aeronautique

Didier Remene

Paulo Francisco

Jean-Luc Pacary

Denis Millepied

Arnaud Bertrand

Valérian Montagne

Valerian Montagne

The invention relates to a composite structuring panel () for the trailing edge of an aircraft element, having: an upper surface (); a lower surface (); an edge () connecting said upper () and lower () surfaces; the upper surface () and the lower surface () being connected by transverse stiffeners () and the structuring panel being made of a unitary part forming the upper surface (), the lower surface (), the edge (), and the transverse stiffeners (). The invention also relates to a method for manufacturing such a panel (), and to an aircraft element comprising such a panel ().

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Buc, France

Didier Remene