机械工程学报
機械工程學報
궤계공정학보
CHINESE JOURNAL OF MECHANICAL ENGINEERING
2014年
20期
93-99
,共7页
邵青%何宇廷%张腾%伍黎明
邵青%何宇廷%張騰%伍黎明
소청%하우정%장등%오려명
搅拌摩擦焊%加筋板%剪切稳定性%有限元法
攪拌摩抆銲%加觔闆%剪切穩定性%有限元法
교반마찰한%가근판%전절은정성%유한원법
friction stir weld%stiffened panel%shear stability%finite element method(FEM)
对2024-T3铝合金搅拌摩擦焊接加筋壁板的剪切稳定性能进行试验研究,得到该结构的剪切失稳形式及屈曲载荷、承载能力及破坏形式。应用有限元法对该焊接加筋壁板结构进行简化建模,对该结构的稳定性和承载能力进行计算,将计算结果与试验结果进行比较。试验及有限元计算结果表明,结构的剪切失稳形式表现为筋条间平板的局部屈曲;屈曲后结构进入张力场受力状态,破坏形式主要表现为平板的塑性变形和边缘撕裂、筋条的弯扭变形以及焊接区的局部脱焊;出现脱焊现象的试验件其承载能力较未出现脱焊现象的试验件下降7.7%;线性和非线性屈曲计算所得屈曲载荷分别比试验平均值高出18.4%和26.2%,而非线性计算所得承载能力比试验平均值高出5.7%,焊接引起的初始缺陷对结构承载能力的影响小于对屈曲载荷的影响;有限元分析得到的结构屈曲形式和失效形式与试验现象吻合,验证了有限元模型的合理性,但其仍需要进一步改进以考虑初始缺陷来减小计算误差。
對2024-T3鋁閤金攪拌摩抆銲接加觔壁闆的剪切穩定性能進行試驗研究,得到該結構的剪切失穩形式及屈麯載荷、承載能力及破壞形式。應用有限元法對該銲接加觔壁闆結構進行簡化建模,對該結構的穩定性和承載能力進行計算,將計算結果與試驗結果進行比較。試驗及有限元計算結果錶明,結構的剪切失穩形式錶現為觔條間平闆的跼部屈麯;屈麯後結構進入張力場受力狀態,破壞形式主要錶現為平闆的塑性變形和邊緣撕裂、觔條的彎扭變形以及銲接區的跼部脫銲;齣現脫銲現象的試驗件其承載能力較未齣現脫銲現象的試驗件下降7.7%;線性和非線性屈麯計算所得屈麯載荷分彆比試驗平均值高齣18.4%和26.2%,而非線性計算所得承載能力比試驗平均值高齣5.7%,銲接引起的初始缺陷對結構承載能力的影響小于對屈麯載荷的影響;有限元分析得到的結構屈麯形式和失效形式與試驗現象吻閤,驗證瞭有限元模型的閤理性,但其仍需要進一步改進以攷慮初始缺陷來減小計算誤差。
대2024-T3려합금교반마찰한접가근벽판적전절은정성능진행시험연구,득도해결구적전절실은형식급굴곡재하、승재능력급파배형식。응용유한원법대해한접가근벽판결구진행간화건모,대해결구적은정성화승재능력진행계산,장계산결과여시험결과진행비교。시험급유한원계산결과표명,결구적전절실은형식표현위근조간평판적국부굴곡;굴곡후결구진입장력장수력상태,파배형식주요표현위평판적소성변형화변연시렬、근조적만뉴변형이급한접구적국부탈한;출현탈한현상적시험건기승재능력교미출현탈한현상적시험건하강7.7%;선성화비선성굴곡계산소득굴곡재하분별비시험평균치고출18.4%화26.2%,이비선성계산소득승재능력비시험평균치고출5.7%,한접인기적초시결함대결구승재능력적영향소우대굴곡재하적영향;유한원분석득도적결구굴곡형식화실효형식여시험현상문합,험증료유한원모형적합이성,단기잉수요진일보개진이고필초시결함래감소계산오차。
Shear experiment on friction stir welded 2024-T3 aluminum alloy stiffened panel specimens is conducted to obtain the buckling behavior and carrying capability of the structure. Finite element method(FEM) is applied to analyze the stability performance of the simplified structure model and the results are compared with experimental results. It is found that, buckling mode of the structure is local buckling of plate between stiffeners, post-buckling mode is under the state of diagonal tension, the failure patterns mainly contain the plastic deformation and tearing of plate, distortion of stiffeners and local weld debonding. Average carrying capability of specimens failed with weld debonding is 7.7%lower than that of other specimens. Buckling loads obtained by linear and nonlinear analysis are separately 18.4% and 26.2% higher than average experimental result, while carrying capability obtained by nonlinear analysis is 5.7%higher than average experimental result, which indicates that the carrying capability is less sensitive to the weld induced initial imperfections than buckling load. Buckling mode and failure pattern obtained by FEM accords well with experimental phenomenon, which validates the rationality of the finite element model, however, it still needs to be further modified to account for weld induced imperfections to reduce the calculation errors..