广西大学学报(自然科学版)
廣西大學學報(自然科學版)
엄서대학학보(자연과학판)
JOURNAL OF GUANGXI UNIVERSITY (NATURAL SCIENCE EDITION)
2013年
4期
982-990
,共9页
张小元%张克实%黄世鸿%顾思远
張小元%張剋實%黃世鴻%顧思遠
장소원%장극실%황세홍%고사원
Q235钢%多轴疲劳%等效应变法%临界面法%寿命评估
Q235鋼%多軸疲勞%等效應變法%臨界麵法%壽命評估
Q235강%다축피로%등효응변법%림계면법%수명평고
Q235 steel%multiaxial fatigue%equivalent strain approach%critical plane approach%life evaluation
对建筑用Q235结构钢分别在单轴和多轴载荷下进行低周疲劳试验,并利用测得的试验结果对寿命评估方法进行研究。研究结果表明:在相同Von Mises等效应变幅值下,材料的比例拉扭路径疲劳寿命高于单轴拉压疲劳寿命,而非比例路径疲劳寿命低于单轴拉压疲劳寿命。按等效应变法进行寿命预测,在非比例加载路径下的预测结果远远超出2倍寿命安全范围区;按临界面法的KBM和Socie模型进行寿命预测能够得到较好的结果,但对圆形路径的高应变幅区得到的结果则过高估计了材料的寿命。在考虑循环过程临界面法向应变影响的基础上,提出了一个改进的考虑临界面拉伸影响的模型,其对比例和非比例路径循环下低周疲劳寿命的评估与实测吻合较好。
對建築用Q235結構鋼分彆在單軸和多軸載荷下進行低週疲勞試驗,併利用測得的試驗結果對壽命評估方法進行研究。研究結果錶明:在相同Von Mises等效應變幅值下,材料的比例拉扭路徑疲勞壽命高于單軸拉壓疲勞壽命,而非比例路徑疲勞壽命低于單軸拉壓疲勞壽命。按等效應變法進行壽命預測,在非比例加載路徑下的預測結果遠遠超齣2倍壽命安全範圍區;按臨界麵法的KBM和Socie模型進行壽命預測能夠得到較好的結果,但對圓形路徑的高應變幅區得到的結果則過高估計瞭材料的壽命。在攷慮循環過程臨界麵法嚮應變影響的基礎上,提齣瞭一箇改進的攷慮臨界麵拉伸影響的模型,其對比例和非比例路徑循環下低週疲勞壽命的評估與實測吻閤較好。
대건축용Q235결구강분별재단축화다축재하하진행저주피로시험,병이용측득적시험결과대수명평고방법진행연구。연구결과표명:재상동Von Mises등효응변폭치하,재료적비례랍뉴로경피로수명고우단축랍압피로수명,이비비례로경피로수명저우단축랍압피로수명。안등효응변법진행수명예측,재비비례가재로경하적예측결과원원초출2배수명안전범위구;안림계면법적KBM화Socie모형진행수명예측능구득도교호적결과,단대원형로경적고응변폭구득도적결과칙과고고계료재료적수명。재고필순배과정림계면법향응변영향적기출상,제출료일개개진적고필림계면랍신영향적모형,기대비례화비비례로경순배하저주피로수명적평고여실측문합교호。
Low cycle fatigue tests on Q235 steel under uniaxial and multiaxial loadings were conduc-ted, and the fatigue life evaluation formulas were studied based on experiments .The low-cycle ex-perimental results of strain show that the fatigue life of the metal under proportionally multiaxial load -ing is longer than that under uniaxial loading , but the fatigue life of the metal under non-proportion-ally multiaxial loading is shorter under the condition of given Von Mises'equivalent strain amplitude controlled by machine .Using the equivalent strain approach to evaluate the low-cycle fatigue life, it can be found that the life value under non-proportionally multiaxial loading was 2 times larger than that given in the experiments .Adopting KBM or Socie model of the critical plane approach , al-though the life prediction become better evidently , over estimation is still inevitable for the low-cycle fatigue under round loading path with large strain amplitude .Based on the consideration of the ten-sion effect on normal of the critical plane during the cycle , a modified critical plane model is pro-posed, in which the tension factor can be determined directly by using the given parameters for a certain loading path .And the life evaluation given by the present model agrees with the experimental result .