发明名称 HONEYCOMB CORE SANDWICH STRUCTURE REPAIR METHOD, AND REPAIR RESULT
摘要 PROBLEM TO BE SOLVED: To provide a honeycomb core sandwich structure repair method being capable of shortening the time required for repairing a part to be repaired and adhering a patch that requires securing surface outer rigidity to the part to be repaired.SOLUTION: The honeycomb core sandwich structure repair method is a repair method for a defect part reaching a core 10 through a first surface skin 11 and having occurred in a honeycomb core sandwich structure sandwiching the core 10 of honeycomb structure between the first surface skin 11 and a second surface skin 12, and is characterized to include a repair material placing step for placing a repair material having a patch 21 for covering the opening of a defect and a single or multiple support post 22 for supporting the patch, a patch adhesion step for adhering the patch 21 to the first surface skin 11, and a support post adhesion step for adhering the support post 22 to the second surface skin 12 or the core 10.
申请公布号 JP2014188996(A) 申请公布日期 2014.10.06
申请号 JP20130069371 申请日期 2013.03.28
申请人 MITSUBISHI AIRCRAFT CORP 发明人 MIZUNO KOTOYO;SHIGETOMI TOSHIKAZU;TANAKA HIDEAKI;ISHIDA MORIMASA;MUTO SHUHEI
分类号 B29C73/04;B32B3/12;B64C1/00;B64F5/00 主分类号 B29C73/04
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