<p>A kit for repairing an opening formed in a composite panel having a laminate skin arranged on opposing sides of a first core material is provided including a plug and a patch. The plug is formed from a second core material and has a cured filler material arranged within at least a portion of the second core material. The patch is formed from a plurality of cured first plies arranged in a stacked orientation. The plug is configured to be received within the opening of the composite panel and the patch is configured to cover the opening of the composite panel.</p>
申请公布号
WO2015126482(A2)
申请公布日期
2015.08.27
申请号
WO2014US65662
申请日期
2014.11.14
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
BREMMER, JONATHAN;ROGG, CHRISTIAN A.;SAUER, JEFFREY G.;TONI, DARRYL MARK;MACALLISTER, ALLAN R. JR.;HOVAN, WILLIAM E. III;DENAVIT, PAUL H.;SIRBU, MIHAIL