BEADED COMPOSITE STRUCTURAL WEB

An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.

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Bibliographic Details
Main Authors Freeman, Jonathan Alexander, Carlson, David G, Carpenter, JR., Joseph Richard, Hogue, Charles David, Kooiman, James Everett
Format Patent
LanguageEnglish
Published 26.09.2024
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An aircraft is described and includes a fuselage; wings attached to the fuselage; and a torque box within the fuselage, the torque box including a side panel, the side panel comprising a composite laminate material including a plurality of stiffening beads integrated therewith.
Bibliography:Application Number: US202318188132