发明名称 Fiber-Reinforced, Composite, Structural Member Exhibiting Non-Linear Strain-to-Failure and Method of Making Same
摘要 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.
申请公布号 US2011210201(A1) 申请公布日期 2011.09.01
申请号 US20090999227 申请日期 2009.06.19
申请人 FEWS ROBERT CLIVE;DERISI BIJAN;HOA SUONG VAN;HOJJATI MEHDI 发明人 FEWS ROBERT CLIVE;DERISI BIJAN;HOA SUONG VAN;HOJJATI MEHDI
分类号 B64C25/52;B32B1/08;B32B5/12;B32B9/00;B32B17/02;B32B27/04;B32B27/08 主分类号 B64C25/52
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