航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2015年
3期
77-82
,共6页
弹性轴承%等刚度设计%压缩刚度%扭转刚度%有限元仿真
彈性軸承%等剛度設計%壓縮剛度%扭轉剛度%有限元倣真
탄성축승%등강도설계%압축강도%뉴전강도%유한원방진
elastomeric bearing%equivalent rigidity design%compression rigidity%torsion Rigidity%finite element simulation
从理论上推导了叠层球面橡胶-金属弹性轴承各胶层的压缩刚度和扭转刚度计算公式,探讨了胶层压缩刚度、扭转刚度的等刚度设计方法,并将等压缩刚度和等扭转刚度设计方案的理论计算结果、有限元仿真结果分别与未进行等刚度设计方案的结果分别进行了计算和对比,结果表明,等刚度设计可以很大程度上消除不同胶层之间的刚度差异,各胶层压缩刚度和扭转刚度的理论计算结果与仿真结果基本吻合。
從理論上推導瞭疊層毬麵橡膠-金屬彈性軸承各膠層的壓縮剛度和扭轉剛度計算公式,探討瞭膠層壓縮剛度、扭轉剛度的等剛度設計方法,併將等壓縮剛度和等扭轉剛度設計方案的理論計算結果、有限元倣真結果分彆與未進行等剛度設計方案的結果分彆進行瞭計算和對比,結果錶明,等剛度設計可以很大程度上消除不同膠層之間的剛度差異,各膠層壓縮剛度和扭轉剛度的理論計算結果與倣真結果基本吻閤。
종이론상추도료첩층구면상효-금속탄성축승각효층적압축강도화뉴전강도계산공식,탐토료효층압축강도、뉴전강도적등강도설계방법,병장등압축강도화등뉴전강도설계방안적이론계산결과、유한원방진결과분별여미진행등강도설계방안적결과분별진행료계산화대비,결과표명,등강도설계가이흔대정도상소제불동효층지간적강도차이,각효층압축강도화뉴전강도적이론계산결과여방진결과기본문합。
The formulations of compression rigidity and torsion rigidity of laminated spherical rubber-metal elastomeric bearing were de-duced by theoretical means,the designed means of equivalent compression rigidity and equivalent torsion rigidity were studied,for the equivalent rigidity plan and unequal rigidity plan,the theoretical results and finite element simulated results of compression rigidity and torsion rigidity are calculated and taken comparied respectively ,the results show that the equivalent rigidity design can eliminate the rigidity difference between different rubber layer to a large extent,the theoretical calculated results of compression rigidity and torsion rigidity are basically identical with the simulated results in every rubber layer.