Airbus Espana, S.l.

Maria Pilar Munoz Lopez

Francisco Jose Cruz Dominguez

Jose David Cano Cediel

The invention relates to an integrated multispar torsion box structure of composite material for aircraft, comprising a lower skin (), an upper skin (), several spars (), each of which comprises in turn a chord () and a web (), several stringers () in the lower skin () and several stringers () in the upper skin (), characterized in that the mentioned integrated torsion box structure is achieved by means of joining unitary U-shaped structural elements (), unitary U-shaped structural elements () with a flap and unitary C-shaped structural elements () with a flap. The invention also relates to a method for manufacturing an integrated multispar torsion box structure of composite material for aircraft.

Growing community of inventors

Madrid, Spain

Maria Pilar Munoz Lopez