Distribution of point loads in honeycomb panels

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United States of America Patent

PATENT NO 8418962
APP PUB NO 20090184204A1
SERIAL NO

12017009

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Abstract

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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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Patent Owner(s)

  • THE BOEING COMPANY

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Frisch, Douglas A Renton, US 9 92
Kajita, Kirk B Newcastle, US 14 408
Piehl, Marc J Renton, US 29 407

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