船舶力学
船舶力學
선박역학
JOURNAL OF SHIP MECHANICS
2014年
1期
152-157
,共6页
严仁军%周宏飞%刘慧%罗志明
嚴仁軍%週宏飛%劉慧%囉誌明
엄인군%주굉비%류혜%라지명
HTS-A钢%对接接头%萌生寿命%扩展寿命%低周疲劳
HTS-A鋼%對接接頭%萌生壽命%擴展壽命%低週疲勞
HTS-A강%대접접두%맹생수명%확전수명%저주피로
HTS-A steel%weld joint%crack-initiation life%crack-propagation life%low-cycle fatigue
文章将HTS-A钢焊接试件的疲劳寿命分为裂纹萌生寿命和裂纹扩展寿命两部分。裂纹萌生寿命的估算采用局部应力应变法,并考虑平均应力和残余应力的影响。裂纹扩展寿命则基于断裂力学方法采用裂纹扩展速率公式进行估算。文章对HTS-A钢焊接试件进行了试验研究,在试验中,对裂纹何时出现和裂纹扩展情况的记录提出了新的方法。根据裂纹扩展情况回归了HTS-A钢焊趾处裂纹扩展速率参数(C、m),继而反推裂纹从0.5 mm直至试件断裂的扩展寿命。而总寿命减去裂纹扩展寿命则为裂纹萌生寿命。该分析方法统一了初始裂纹深度,对理论上研究焊接接头裂纹萌生寿命和裂纹扩展寿命提供了试验依据。试验结果表明,工程定义的裂纹萌生寿命不可忽略。另外,咬边缺陷对裂纹萌生寿命的影响很大,而对裂纹的扩展寿命影响十分小。通过试验结果的对比,也验证了HTS-A钢对接接头低周疲劳寿命估算方法的可靠性。
文章將HTS-A鋼銲接試件的疲勞壽命分為裂紋萌生壽命和裂紋擴展壽命兩部分。裂紋萌生壽命的估算採用跼部應力應變法,併攷慮平均應力和殘餘應力的影響。裂紋擴展壽命則基于斷裂力學方法採用裂紋擴展速率公式進行估算。文章對HTS-A鋼銲接試件進行瞭試驗研究,在試驗中,對裂紋何時齣現和裂紋擴展情況的記錄提齣瞭新的方法。根據裂紋擴展情況迴歸瞭HTS-A鋼銲趾處裂紋擴展速率參數(C、m),繼而反推裂紋從0.5 mm直至試件斷裂的擴展壽命。而總壽命減去裂紋擴展壽命則為裂紋萌生壽命。該分析方法統一瞭初始裂紋深度,對理論上研究銲接接頭裂紋萌生壽命和裂紋擴展壽命提供瞭試驗依據。試驗結果錶明,工程定義的裂紋萌生壽命不可忽略。另外,咬邊缺陷對裂紋萌生壽命的影響很大,而對裂紋的擴展壽命影響十分小。通過試驗結果的對比,也驗證瞭HTS-A鋼對接接頭低週疲勞壽命估算方法的可靠性。
문장장HTS-A강한접시건적피로수명분위렬문맹생수명화렬문확전수명량부분。렬문맹생수명적고산채용국부응력응변법,병고필평균응력화잔여응력적영향。렬문확전수명칙기우단렬역학방법채용렬문확전속솔공식진행고산。문장대HTS-A강한접시건진행료시험연구,재시험중,대렬문하시출현화렬문확전정황적기록제출료신적방법。근거렬문확전정황회귀료HTS-A강한지처렬문확전속솔삼수(C、m),계이반추렬문종0.5 mm직지시건단렬적확전수명。이총수명감거렬문확전수명칙위렬문맹생수명。해분석방법통일료초시렬문심도,대이론상연구한접접두렬문맹생수명화렬문확전수명제공료시험의거。시험결과표명,공정정의적렬문맹생수명불가홀략。령외,교변결함대렬문맹생수명적영향흔대,이대렬문적확전수명영향십분소。통과시험결과적대비,야험증료HTS-A강대접접두저주피로수명고산방법적가고성。
Fatigue life of HTS-A steel welding test specimen is decomposed into the engineering crack-ini-tiation life and the crack-propagation life. The engineering crack-initiation life is estimated based on the local stress-strain method, with the influence of the mean stress and the residual stress considered. The crack- propagation life is estimated by the use of the crack propagation rate formula based on Linear E-lastic Fracture Mechanics (LEFM) method. Experimental study on HTS-A steel welding test specimens was conducted. New methods of scanning crack-initiation and recording crack propagation were proposed during test. Crack propagation rate parameters (C, m) of HTS-A steel at weld toe can be obtained as regression coefficients. According to above crack propagation rate parameters, the crack-propagation life is calculated from an assigned depth (0.5 mm) to specimen break. Subtraction of the total life from the crack-propaga-tion life is the engineering crack-initiation life. This method unifies initial crack depth, and provides an experimental basis for studying crack-initiation life and the crack-propagation life of the weld joint. The test results show that the engineering crack-initiation life can not be negligible. And welding undercut influ-ences the engineering crack-initiation life significantly, but has no influence on the crack-propagation life. Through the verification of test results, the reliability of present estimating method on low-cycle fatigue life at butt joint of HTS-A steel is confirmed.