发明名称 REPAIR METHOD AND REPAIR STRUCTURE FOR HONEYCOMB SANDWICH STRUCTURAL BODY
摘要 <p>Provided is a repair method comprising: a step (A) in which a honeycomb core (11) containing a damaged area is removed together with a front-side skin (12) to form a repair gap (14); a step (B) in which a repair honeycomb core (21) having a planarized end face (30) to which a repair patch (22) is to be bonded is inserted in the repair gap (14); a step (C) in which a repair patch is positioned on the planarized end face (30) of the repair honeycomb core (21) with a film adhesive (24) therebetween; and a step (D) in which bonding of the repair honeycomb core (21) with the existing honeycomb sandwich structural body (10) and the repair patch (22) and curing of the repair patch (22) are carried out in a reduced-pressure atmosphere accompanied by heating.</p>
申请公布号 WO2013108328(A1) 申请公布日期 2013.07.25
申请号 WO2012JP07538 申请日期 2012.11.22
申请人 MITSUBISHI AIRCRAFT CORPORATION 发明人 SHIGETOMI, TOSHIKAZU
分类号 B32B3/12;F01D25/00;F02C7/00 主分类号 B32B3/12
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