Abstract: Rib and spar webs are joined in a composite wingbox to eliminate fasteners by welding the webs along bondlines defined by overlapping sections of the webs. Heat to produce the weld is generally achieved resistively by connecting a multistrip susceptor positioned along the bond line to a current source, since the geometry makes it difficult to heat these web joints inductively. The wingbox is completed without fasteners by welding skins to the rib-spar wingbox.
Type:
Grant
Filed:
June 6, 1995
Date of Patent:
October 24, 2006
Assignee:
Th Boeing Company
Inventors:
Marc R. Matsen, Douglas A. McCarville, Michael M. Stepan