/ DIAMOND SHAPED WINDOW FOR A COMPOSITE AND/OR METALLIC AIRFRAME

摘要

The aircraft fuselage may include a cylindrical section having a lateral region. The bodies may include a first incision and a second incision formed in the lateral region in a side by side relationship. The fuselage can provide a direct load path extending along the tubular section. The load path may extend substantially continuously from the lower portion of the lateral region below the first incision to the upper portion of the lateral region above the second incision.