Composite sections for aircraft fuselages and methods and systems for manufacturing such sections are disclosed herein. A composite section configured in accordance with one embodiment of the invention includes a skin and at least first and second stiffeners. The skin can include a plurality of unidirectional...http://www.google.es/patents/US8157212?utm_source=gb-gplus-sharePatente US8157212 - Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
Composite barrel sections for aircraft fuselages and other structures, and ...
