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Spliced laminate for aircraft fuselage

  • US 5,429,326 A
  • Filed: 07/09/1992
  • Issued: 07/04/1995
  • Est. Priority Date: 07/09/1992
  • Status: Expired due to Term
First Claim
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1. A laminated panel comprising at least:

  • (a) a first metal layer having a thickness of less than about 1 mm and comprising a first section, a second section generally coplanar with the first section and a first splice line between the first and second sections;

    (b) a second metal layer having a thickness of less than about 1 mm and comprising a first section, a second section generally coplanar with the first section and a second splice line between the first and second sections, the second splice line being spaced laterally from the first splice line by at least several centimeters; and

    (c) a fiber reinforced adhesive layer between the first and second metal layers.

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