Distribution of point loads in honeycomb panels
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United States of America Patent
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Apr 16, 2013
Grant Date -
Jul 23, 2009
app pub date -
Jan 19, 2008
filing date -
Jan 19, 2008
priority date (Note) -
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status (Latency Note)
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Abstract
Composite panels used in aircraft are formed by a sandwich including a lightweight honeycomb core reinforced by a solid plank in medial regions of the panel. The plank is bonded to the honeycomb and forms an integral part of the core where a strut is attached to the panel. The plank distributes point loads imposed on the panel by the strut.
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Cited Art Landscape
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