COMPOSITE WING STRUCTURE AND METHODS OF MANUFACTURE

A method of making a composite skin (199) for a tiltrotor aircraft includes providing a first skin (201) in a mold (220), the first skin (201) having a periphery (201p) defined by a forward edge (201a), an aft edge (201b), and outboard ends (201c, 201d); providing a plurality of honeycomb panels (20...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: CARLSON, David G, BAINES, Andrew G, DECKER, George R, McCULLOUGH, John R, WOLFE, Douglas K
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!