| CPC C09J 163/00 (2013.01) [B32B 7/027 (2019.01); B32B 7/12 (2013.01); B32B 15/012 (2013.01); B32B 37/1207 (2013.01); C09J 7/21 (2018.01); C09J 7/35 (2018.01)] | 14 Claims |
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1. A laminate comprising a first material, an adhesive agent layer, and a second material provided in this order,
wherein the first material and the second material have different linear expansion coefficients,
wherein the adhesive agent layer comprises an adhesive agent having a warpage reduction index of not less than 30,
wherein a content of an epoxy resin comprised in the adhesive agent is 85 mass % or more based on 100 mass % of overall resin component of the adhesive agent,
wherein the adhesive agent layer has an average storage elastic modulus of 1 to 400 MPa in a temperature range of 25° C. to 180° C.,
the warpage reduction index of the adhesive agent being determined by:
preparing an analysis model laminate having:
an aluminum plate having a width of 25 mm, a length of 100 mm, and a thickness of 1.6 mm,
a cold-rolled steel plate having a width of 25 mm, a length of 100 mm, and a thickness of 1.6 mm, and
a layer of the adhesive agent between the aluminum plate and the cold-rolled steel plate, the layer of the adhesive agent having a thickness of 0.7 mm;
preparing a reference model laminate having:
an aluminum plate having a width of 25 mm, a length of 100 mm, and a thickness of 1.6 mm, and
a cold-rolled steel plate having a width of 25 mm, a length of 100 mm, and a thickness of 1.6 mm,
wherein the reference model laminate does not have any adhesive agent between the aluminum plate and the cold-rolled steel plate;
determining a displacement amount WA at an end of the analysis model laminate by finite element structure analysis using Computer Aided Engineering (CAE) software while a middle portion of the cold-rolled steel plate is fixed in place and a temperature of the analysis model laminate is changed from a starting temperature of 180° C. to a final temperature of 25° C.;
determining a displacement amount WB at an end of the reference model laminate by finite element structure analysis using Computer Aided Engineering (CAE) software while a middle portion of the cold-rolled steel plate is fixed in place and a temperature of the reference model laminate is changed from a starting temperature of 180° C. to a final temperature of 25° C.; and
calculating the warpage reduction index from the following expression (1):
Warpage reduction index=100−(WA/WB)×100 (1).
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