Spliced laminate for aircraft fuselage
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United States of America Patent
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-
Jul 4, 1995
Grant Date -
N/A
app pub date -
Jul 9, 1992
filing date -
Jul 9, 1992
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
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 line in a second metal layer, and spaced laterally from the second splice line. An adhesive layer between the metal layers preferably contains reinforcing fibers bridging across the splice lines. An aircraft fuselage or wing or empennage made with spliced body panels of the invention has fewer joints and weighs less than one made with narrower body panels containing unspliced metal layers.
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