The Boeing Company
Systems and methods for joining composite panels

Abstract:

Disclosed embodiments include a structural assembly having a first panel having a first edge and a first aperture adjacent to the first edge, and a clamp having a first piece that passes through the first aperture, a second piece, and a fastening portion that fastens together the first piece and the second piece. The structural assembly may include a second panel having a second edge and a second aperture adjacent to the second edge, and the second piece passes through the second aperture, and the clamp holds the first panel and the second panel together.