发明名称 STRENGTH ANALYSIS METHOD
摘要 <P>PROBLEM TO BE SOLVED: To provide a strength analysis method capable of maintaining accuracy of strength evaluation and performing the strength evaluation easily and at low cost with respect to a strength analysis object having a junction portion between members, at least one of which has a tapered junction portion of one adherend. <P>SOLUTION: A region A3 formed by bonding a tapered face 11c of a recess 11 and a tapered face 20d of a plug 20 via an adhesive 200 is divided into a plurality of patches A31, A32, ... When the region A3 is divided into the patches A31, A32, ..., thickness dimensions of the recess 11 and the plug 20 are preferably sectioned into a plurality of levels. Each of the patches A31, A32, ... serves as: a shell element E31 of a constant thickness, one face side of which is composed of a material forming the plug 20; a shell element E32 of a constant thickness, the other face side of which is composed of a material forming a member 10; and a solid element E33 composed of the adhesive 200 between the shell element E31 and the shell element E32. <P>COPYRIGHT: (C)2013,JPO&INPIT
申请公布号 JP2013109443(A) 申请公布日期 2013.06.06
申请号 JP20110252285 申请日期 2011.11.18
申请人 MITSUBISHI AIRCRAFT CORP 发明人 SUHARA MASAYOSHI
分类号 G06F17/50 主分类号 G06F17/50
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