The Boeing Company
ASSEMBLY LINE FABRICATION AND ASSEMBLY OF AIRCRAFT WINGS

Abstract:

Systems and methods are provided for fabricating a wing panel. Methods include aligning a strongback over a wing panel, vacuum attaching a wing panel surface and pogos extending beneath the strongback, and adjusting the length of pogos to enforce a contour to the wing panel. Systems include a strongback to extend over a wing panel, adjustable-length pogos extending beneath the strongback, and vacuum couplers to attach to a wing panel surface. Other systems include a track, work stations along the track, a strongback to extend over the wing panel and move along the track, adjustable-length pogos extending beneath the strongback, and vacuum couplers to attach to a wing panel surface. Apparatus includes a shuttle having adapters that mate the shuttle with a track, adjustable-length carriers with vacuum couplers to couple with a wing panel surface, and indexing units that interact with indexing features in a manufacturing excess of the wing panel.