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PREDICTING METHOD OF BENDING RADIUS AT BUCKLING LIMIT IN BENDING ALUMINUM ALLOY SHAPE, PREDICTING METHOD OF WIDTHT TO THICKNESS RATIO, AT BUCKLING LIMIT, BENDING METHOD OF ALUMINUM ALLOY SHAPE AND RECORDING MEDIUM
PREDICTING METHOD OF BENDING RADIUS AT BUCKLING LIMIT IN BENDING ALUMINUM ALLOY SHAPE, PREDICTING METHOD OF WIDTHT TO THICKNESS RATIO, AT BUCKLING LIMIT, BENDING METHOD OF ALUMINUM ALLOY SHAPE AND RECORDING MEDIUM
PROBLEM TO BE SOLVED: To predict a bending radius at a buckling limit of a shape made of aluminum alloy in a high precision. ;SOLUTION: For a bending radius at a buckling limit in bending a shape made of aluminum alloy, a bending center radius R satisfying the formulas 1, 2 in the following is obtained. (t is a thickness of object section to predict a buckling limit among a shape, b is a plate width, h is a distance from a bending neutral axis to a bending most inside part of the object section as taking a bending direction in a positive direction, k is a buckling coefficient, (A, B, C) are coefficients different in the case that a shape is T1 heat treated material or T5 heat treated material, η is a constant showing a stress state (-h'/h), h' is a distance from a neutral axis to a bending most outside part of the object section as taking a bending direction in a positive direction, (D, E, F) are coefficients different when the object section is a protruded flange or except the protruded flange).;COPYRIGHT: (C)2001,JPO
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机译:解决的问题:高精度地预测铝合金制成的形状在屈曲极限处的弯曲半径。 ;解决方案:对于在弯曲铝合金制成的形状时在屈曲极限处的弯曲半径,可以获得满足以下公式1、2的弯曲中心半径R。 (t是预测形状中屈曲极限的对象部分的厚度,b是板的宽度,h是从弯曲中性轴到对象部分的弯曲最内侧部分的距离,取正方向的弯曲方向k是屈曲系数,(A,B,C)是形状为T1热处理材料或T5热处理材料时不同的系数,η是表示应力状态的常数(-h'/ h ),h'是从中性轴到对象部分弯曲的最外侧部分的距离,以正方向上的弯曲方向为准,(D,E,F)是当对象部分是凸起的凸缘或;版权:(C)2001,JPO
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