BEADED COMPOSITE STRUCTURAL WEB

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.

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Freeman, Jonathan Alexander, Carlson, David G, Carpenter, JR., Joseph Richard, Hogue, Charles David, Kooiman, James Everett
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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.