SPLICED LAMINATE FOR AIRCRAFT FUSELAGE

A laminated body panel for aircraft applications comprises first and second metal layers and an adhesive layer. First and second sections in each metal layer are generally coplanar and separated by a splice line. A first splice line in a first metal layer is generally parallel to a second splice lin...

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Bibliographische Detailangaben
Hauptverfasser: OOST, ROB C. V, GREIDANUS, BUWE V. WIMERSMA, GARESCHE, CARL E, ROEBROEKS, GERARDUS H. J. J, GUNNINK, JAN W
Format: Patent
Sprache:eng ; fre
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