大连理工大学学报
大連理工大學學報
대련리공대학학보
JOURNAL OF DALIAN UNIVERSITY OF TECHNOLOGY
2013年
6期
787-793
,共7页
郝鹏%王博%李刚%杜凯繁%张希%唐霄汉%曾杜娟
郝鵬%王博%李剛%杜凱繁%張希%唐霄漢%曾杜娟
학붕%왕박%리강%두개번%장희%당소한%증두연
加筋柱壳%弹塑性屈曲%缺陷敏感性%双曲母线
加觔柱殼%彈塑性屈麯%缺陷敏感性%雙麯母線
가근주각%탄소성굴곡%결함민감성%쌍곡모선
stiffened shell%elastic and plastic buckling%imperfection sensitivity%hyperbolic generatrix
对于加筋柱壳等薄壁结构,轴压承载力对不同结构形式表现出不同的缺陷敏感性,寻找低缺陷敏感度的结构设计形式具有重要的研究意义。首先以分别发生弹性和塑性屈曲的两个直径3m的正交加筋柱壳为例,研究了不同幅度双曲母线形状对两者承载力的影响,发现双曲母线外凸和内凹会分别提高两种加筋柱壳的轴压承载力。然后以特征值屈曲模态和单点凹坑两种缺陷为例,对具有不同幅度双曲母线的加筋柱壳开展了缺陷敏感性分析。结果表明,对于两种加筋柱壳结构均可以通过适当幅度的外凸双曲母线形状降低缺陷敏感性,为提高运载火箭加筋柱壳的可靠性储备提供了一种易实现的结构方案。
對于加觔柱殼等薄壁結構,軸壓承載力對不同結構形式錶現齣不同的缺陷敏感性,尋找低缺陷敏感度的結構設計形式具有重要的研究意義。首先以分彆髮生彈性和塑性屈麯的兩箇直徑3m的正交加觔柱殼為例,研究瞭不同幅度雙麯母線形狀對兩者承載力的影響,髮現雙麯母線外凸和內凹會分彆提高兩種加觔柱殼的軸壓承載力。然後以特徵值屈麯模態和單點凹坑兩種缺陷為例,對具有不同幅度雙麯母線的加觔柱殼開展瞭缺陷敏感性分析。結果錶明,對于兩種加觔柱殼結構均可以通過適噹幅度的外凸雙麯母線形狀降低缺陷敏感性,為提高運載火箭加觔柱殼的可靠性儲備提供瞭一種易實現的結構方案。
대우가근주각등박벽결구,축압승재력대불동결구형식표현출불동적결함민감성,심조저결함민감도적결구설계형식구유중요적연구의의。수선이분별발생탄성화소성굴곡적량개직경3m적정교가근주각위례,연구료불동폭도쌍곡모선형상대량자승재력적영향,발현쌍곡모선외철화내요회분별제고량충가근주각적축압승재력。연후이특정치굴곡모태화단점요갱량충결함위례,대구유불동폭도쌍곡모선적가근주각개전료결함민감성분석。결과표명,대우량충가근주각결구균가이통과괄당폭도적외철쌍곡모선형상강저결함민감성,위제고운재화전가근주각적가고성저비제공료일충역실현적결구방안。
For thin-walled structures , such as stiffened shells , collapse loads show different imperfection sensitivities , and this enhances the significance of finding the designs with low imperfection sensitivities .Based on two orthogrid stiffened shells with a diameter of 3 m (elastic and plastic buckling , respectively ) , the effects of amplitudes of hyperbolic generatrix shapes on the collapse loads of two models are firstly investigated . It is found that the outward and inward hyperbolic generatrix shapes can increase the collapse loads of two models .Then ,the imperfection sensitivities of two models with varying amplitudes of hyperbolic generatrix shapes are studied in detail based on eigenmode-shape and single dimple imperfections .Experimental results indicate that the outward hyperbolic generatrix shapes are capable of reducing the imperfection sensitivities of two types of stiffened shells ,w hich are expected to provide a realistic design ,aiming at increasing the reliability margin for stiffened shells in launch vehicles .