发明名称 HIGH EFFICIENCY LOAD TRANSFER IN COMPOSITE STRUCTURE
摘要 Thin perforated sheets of titanium (20) are interleaved between adjacently situated graphite/epoxy plies (12, 14) - in the area where metal fittings are to be installed (16, 22, 18). Epoxy flows through these perforations (24) so as to achieve a gripping mechanism between the titanium (20) sheet and the graphite/epoxy plies (12, 14). The result is efficient transfer of load in the titanium to the composite fiber materials without suffering the cost penalty of extensive graphite/epoxy buildups (without interleaved titanium sheets). Epoxy plugs within the titanium sheet perforations (24) bond to confronting surfaces of the graphite/epoxy plies and provide a fail safe gripping mechanism between the titanium sheet and adjacent graphite/epoxy plies in the unlikely event that the shear bond between the faces of the titanium sheet (20) and the graphite/epoxy plies (12, 14) becomes completely disbonded.
申请公布号 WO9621561(A1) 申请公布日期 1996.07.18
申请号 WO1996US01618 申请日期 1996.01.11
申请人 GRUMMAN AEROSPACE CORPORATION 发明人 PADDEN, VINCENT, T.
分类号 B32B3/24;B32B15/14;(IPC1-7):B32B3/24 主分类号 B32B3/24
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