Structures and methods for joining composite fuselage sections and other panel assemblies together are disclosed herein. In one embodiment, a shell structure configured in accordance with the present invention includes a first panel portion positioned adjacent to a second panel portion. The first panel...http://www.google.fr/patents/US8061035?utm_source=gb-gplus-shareBrevet US8061035 - Splice joints for composite aircraft fuselages and other structures
Splice joints for composite aircraft fuselages and other structures
