Composite material panel with shock-protected edges
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United States of America Patent
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Nov 12, 2002
Issued Date -
N/A
app pub date -
Aug 10, 1999
filing date -
Nov 21, 1997
priority date (Note) -
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Abstract
A panel of composite material, in particular with a thermosetting or thermoplastic matrix, with edges and/or external surface protected from shocks and erosion, for any streamlining element for housings or nacelles of aeronautical motors, comprises, over all or a portion of its edges, a cladding which forms a border overlapping the two opposite surfaces of the panel. The border comprises a metallic cloth connected to the structure of the panel by an adhesive agent, diffused through the cloth. The panel is particularly applicable to aircraft.
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