Fiber-reinforced, composite, structural member exhibiting...

B - Operations – Transporting – 32 – B

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Details

B32B 18/00 (2006.01) B32B 19/00 (2006.01) C04B 35/52 (2006.01) C04B 35/83 (2006.01) B64C 25/00 (2006.01)

Patent

CA 2635524

A fiber-reinforced, organic matrix, composite structural member includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the structural member exhibits a non-linear stress-strain response when mechanically loaded to failure. A helicopter landing gear includes a pair of skids and one or more cross members extending between the pair of skids. The one or more cross members includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the cross members exhibit non-linear stress- strain responses when mechanically loaded to failure.

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