Aeronautics and astronautics – Aircraft structure – Details
Reexamination Certificate
2007-07-05
2011-10-25
Dinh, Tien (Department: 3644)
Aeronautics and astronautics
Aircraft structure
Details
C428S057000, C052S801100
Reexamination Certificate
active
08042770
ABSTRACT:
A multilayer structural element, such as a skin panel for an aircraft fuselage, comprises a plurality of metal webs and a plurality of fiber webs arranged as layers in a sandwich structure, where the metal webs of neighbouring layers form stepped connecting regions. A material strip is provided on an outer surface of the sandwich structure for at least partially covering an outlying connecting region, and the material strip enables the placement of rivets at uniform spacing for fastening a structure to the structural element.
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Martin Alexander
Pellenkoft Frederik
Tillich Arthur
Airbus Operations GmbH
Dinh Tien
Fenwick & West LLP
Sanderson Joseph W
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