兵器材料科学与工程
兵器材料科學與工程
병기재료과학여공정
Ordnance Material Science and Engineering
2010年
2期
11-14
,共4页
牟常伟%王帮峰%葛瑞钧%宁素娟
牟常偉%王幫峰%葛瑞鈞%寧素娟
모상위%왕방봉%갈서균%저소연
变体机翼%波纹式柔性蒙皮%制备方法%SMA
變體機翼%波紋式柔性矇皮%製備方法%SMA
변체궤익%파문식유성몽피%제비방법%SMA
morphing wings%corrugated flexible skin%preparation method%SMA
论述一种适用于变体机翼的具有主动变形能力的波纹式柔性蒙皮基体制备方法,并制作了拉伸测试件,进行拉伸实验.实验结果显示,当伸长量小于4%时,蒙皮基体线性伸长,在此范围内.可利用蒙皮自身的弹性使其恢复到原始形状.测试基于形状记忆合金(SMA)驱动器的波纹式蒙皮的主动变形效果,给SMA驱动器通以电流,利用SMA的形状记忆效应驱动蒙皮基体变形,试验测试不同电流下基体伸长2%所需的时间,及利用自身弹力回复时的残余变形量,蒙皮基体自身产生的变形将大大降低变体机翼蒙皮变形时对驱动力的要求.
論述一種適用于變體機翼的具有主動變形能力的波紋式柔性矇皮基體製備方法,併製作瞭拉伸測試件,進行拉伸實驗.實驗結果顯示,噹伸長量小于4%時,矇皮基體線性伸長,在此範圍內.可利用矇皮自身的彈性使其恢複到原始形狀.測試基于形狀記憶閤金(SMA)驅動器的波紋式矇皮的主動變形效果,給SMA驅動器通以電流,利用SMA的形狀記憶效應驅動矇皮基體變形,試驗測試不同電流下基體伸長2%所需的時間,及利用自身彈力迴複時的殘餘變形量,矇皮基體自身產生的變形將大大降低變體機翼矇皮變形時對驅動力的要求.
논술일충괄용우변체궤익적구유주동변형능력적파문식유성몽피기체제비방법,병제작료랍신측시건,진행랍신실험.실험결과현시,당신장량소우4%시,몽피기체선성신장,재차범위내.가이용몽피자신적탄성사기회복도원시형상.측시기우형상기억합금(SMA)구동기적파문식몽피적주동변형효과,급SMA구동기통이전류,이용SMA적형상기억효응구동몽피기체변형,시험측시불동전류하기체신장2%소수적시간,급이용자신탄력회복시적잔여변형량,몽피기체자신산생적변형장대대강저변체궤익몽피변형시대구동력적요구.
A preparation method of basal body for corrugated skin with active deformability,which was applicable to morphing wings,was introduced in this paper.The basal body specimens were made and the tensile test was performed.Test results show that the basal body elongates linearly as the increase of tensile force when the elongation indicator is less than 4%.Within this range,the basal body could recover to its original shape with the help of its own elastic force.The active deformability of the basal body for corrugated skin was tested basing on shape memory alloy(SMA)actuator.When current is applied to SMA,the basal body will be forced to deform due to the shape memory effect of SMA.The time consuming was measured when the elongation of basal body is 2% under different currents.And the residual deformation of the basal body,with the help of its own elastic force,was also measured.With the SMA actuator,the driving force for the deformation of morphing wing can be reduced significantly.