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飞机高强钢拼焊板高温拉伸试验及高温本构模型研究

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为深入了解B340LA低碳合金钢、B1500HS冷轧钢以及B340LA/B1500HS高强钢拼焊板等飞机制造常用钢材的热变形特性,提升相关企业对于高强度钢的加工能力,对各种高强度钢板料进行拉伸试验,进而获得板料的应力-应变关系数据.在此基础上,采用经过改进的Johnson-Cook模型对板料的应力-应变关系数据进行拟合处理,取得了较为理想的拟合效果,决定系数R2接近于1,代表该模型的拟合结果具有良好的可信度.最后基于所得到的拟合结果建立了B340LA低碳合金钢、B1500HS冷轧钢以及B340LA/B1500HS高强钢拼焊板三种高强度钢板料的本构模型.
High-temperature tensile test and high-temperature constitutive model of aircraft high-strength steel tailored blank
In order to understand the thermal deformation characteristics of B340LA low-carbon alloy steel,B1500HS cold-rolled steel and B340LA/B1500HS high-strength steel tailored blank and other commonly used steels in aircraft manufacturing,and improve the processing capacity of related enterprises for high-strength steel.The tensile test of various high-strength steel sheets was carried out to obtain the stress-strain relationship data of the sheets.On this basis,the improved Johnson-Cook model is used to fit the stress-strain relationship data of the sheet,and an ideal fitting effect is obtained,and the coefficient of determination R2 is close to 1,which means that the fitting results of the model have good reliability.Finally,based on the fitting results,the constitutive models of three high-strength steel sheets,namely B340LA low-carbon alloy steel,B1500HS cold-rolled steel and B340LA/B1500HS high-strength steel tailored blank,were established.

high strength rigiditytensile testfitting relationshipconstitutive model

赵凯

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西安航空职业技术学院,陕西 西安 710089

高强度钢 拉伸试验 拟合关系 本构模型

2024

模具技术
上海交通大学

模具技术

CSTPCD
影响因子:0.219
ISSN:1001-4934
年,卷(期):2024.(6)