首页|裂纹位置对推进剂贮箱壳体失效评定曲线的影响研究

裂纹位置对推进剂贮箱壳体失效评定曲线的影响研究

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为获取准确的临界裂纹尺寸2cc以实现可重复使用推进剂贮箱LBB设计及评定,构建了2 种裂纹类型 5 组典型裂纹位置的贮箱壳体失效评定曲线(FAC),并分析了裂纹位置对FAC的影响.结果表明:随着裂纹从圆柱段中心向封头移动(y的增加),2 种裂纹类型壳体极限载荷PL均先保持不变,再显著增加,最后小幅增加,FAC总体上逐渐升高,壳体的安全性增加.工程上采用选择1 和选择2 曲线确定的临界裂纹尺寸2cc 仅能对极少数的载荷工况下特定裂纹位置的贮箱壳体进行准确的LBB分析.建立裂纹位置相关的FAC,可以提高贮箱壳体的结构完整性.
Effects of Crack Location on Failure Assessment Curves(FAC)of Propellant Tank Shells
In order to obtain accurate critical crack size 2cc to realize the LBB design and evaluation of reusable propellant tank,the failure assessment curves(FAC)of cracks with two types and five typical locations were constructed,and the effects of crack location on the FAC were analyzed.The results showed that with the crack moving from the center of the cylinder to the head(y increases),the limit load PL of the shells with two crack types remained unchanged firstly,then increased signif-icantly and finally increased slightly;The FAC gradually increased,and the safety of the shell in-creased.At present,the critical crack size 2cc determined by Choice 1 and Choice 2 curves in engi-neering can only accurately analyze the specific crack location of the tank shells under a few load conditions.In order to improve the structural integrity of the tank shell,it is necessary to establish a FAC related to the crack location.

failure assessment curvepropellant tank shellcrackLBB analysisstructural integrity

范凯、韩冲

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上海空间推进研究所,上海 201112

上海空间发动机工程技术研究中心,上海 201112

失效评定曲线 推进剂贮箱壳体 裂纹 LBB分析 结构完整性

上海市"科技创新计划"启明星培育(扬帆专项)项目

22YF1429400

2024

载人航天
中国载人航天工程办公室

载人航天

CSTPCD北大核心
影响因子:0.411
ISSN:1674-5825
年,卷(期):2024.30(4)
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