TY - JOUR
T1 - New constitutive equation based on parallel model for Ti-6Al-4V alloy
AU - Nie, Lei
AU - Li, Fu Guo
AU - Fang, Yong
PY - 2002/3
Y1 - 2002/3
N2 - Taking the flow stress σ of Ti-6Al-4V as and objective function, the influences that forging parameters (deformation temperature, deformation rate, deformation degree) impose on the flow stress are studied systematically by the hot compressive simulation experiments, and more, based on the mathematic theory of statistics, a new constitutive equation is developed, which can reflect synthetically the influences of forging thermal parameters on material forming property; meanwhile, the influence regularities of deformation processing parameters (deformation temperature, equivalent strain rate, equivalent strain) on the objective function are generalized, therefore, a scientific basis is provided for the numerical simulation of forging process of Ti-6Al-4V alloy, as well as the rational choice and control of forging thermal parameter.
AB - Taking the flow stress σ of Ti-6Al-4V as and objective function, the influences that forging parameters (deformation temperature, deformation rate, deformation degree) impose on the flow stress are studied systematically by the hot compressive simulation experiments, and more, based on the mathematic theory of statistics, a new constitutive equation is developed, which can reflect synthetically the influences of forging thermal parameters on material forming property; meanwhile, the influence regularities of deformation processing parameters (deformation temperature, equivalent strain rate, equivalent strain) on the objective function are generalized, therefore, a scientific basis is provided for the numerical simulation of forging process of Ti-6Al-4V alloy, as well as the rational choice and control of forging thermal parameter.
KW - Constitutive equation
KW - Forming property
KW - Parallel model
KW - Thermal parameter
KW - Ti-6Al-4V alloy
UR - http://www.scopus.com/inward/record.url?scp=0036520669&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:0036520669
SN - 1000-6893
VL - 23
SP - 190
EP - 192
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 2
ER -