PROCÉDÉ DE MONTAGE DE BOITES DE TORSION POUR L'AÉRONAUTIQUE

摘要

The method basically consists of mounting the spars (2, 2') and the ribs (3) with reference to the skin (4) in such a manner that, once the spars (2, 2') are positioned with their proper reference in an assembly jig (12), the ribs (3) are transversely positioned with the condition that they are adjusted making contact against the inner surface of the skin (4). The device comprises a template element (15) which is used for previously providing the skin with the theoretical form it must acquire once mounted, and to firmly maintain that theoretical form by including means for securing and tightening (16) the skin (4), as well as means (17, 18, 19, 20) for supporting and positioning the skin (4).