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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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