首页|2195铝锂合金火箭贮箱焊接接头强度分析

2195铝锂合金火箭贮箱焊接接头强度分析

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为确定火箭贮箱搅拌摩擦焊(FSW)焊接接头疲劳寿命,完成对贮箱结构的疲劳分析,对2195铝锂合金母材标准试件与搅拌摩擦焊焊接接头标准试验件进行静力试验与常幅疲劳试验,得出母材与FSW焊接接头的拉伸强度等力学性能参数,同时绘制其S-N曲线.在试验数据基础上,应用ABAQUS软件对贮箱进行静力分析,联合NCODE软件估算贮箱模型在给定工况载荷下的疲劳寿命.结果表明:应力最严重位置为筒段焊缝处,最先破坏位置发生在筒段横竖焊缝交接处.在疲劳寿命分析的基础上应用ABAQUS-FRANC3D软件联合仿真,在焊缝破坏位置处插入角裂纹,模拟三维裂纹扩展,当裂纹扩展为穿透裂纹时,计算终止.计算了三维表面裂纹的应力强度因子和裂纹扩展寿命,为贮箱损伤容限提供了评估思路.
Strength Analysis of Elded Joints of 2195 Aluminum-Lithium Alloy Rocket Tank
In order to determine the fatigue life of the friction stir welding(FSW)welded joints of the rocket tank and complete the fatigue analysis of the tank structure,the static and the normal fatigue tests on the standard specimens of 2195 aluminum-lithium and FSW welded joints were carried out to abtain the mechanical properties of tensile strength of the base metal and the FSW welded joint etc.,and the S-N curve was drawn concurrently.Based on the test data,the static analysis of the tank was conducted by ABAQUS software,and the fatigue life of the tank model under the given load was estimated with the NCODE software.The results show that the most severe stress position is at the weld seam of cylinder section,and the first failure position occures at the junction of the horizontal and vertical welds of the cylinder section.On the basis of the fatigue life analysis,the ABAQUS-FRANC3D software co-simulation is applied to insert corner cracks at the failure position of the weld and simulate the three-dimensional crack propagation.When the crack expands into a penetrating crack,the calculation is terminated.The calculated stress intensity factor and crack propagation life of three-dimensional surface cracks provide thinking for evaluating the damage tolerance of the tank.

friction stir weldingfatiguecrack growthfatigue testing

马佳琳、张恒珲、李磊、童明波、王芳丽

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南京航空航天大学航空学院,江苏南京 210016

金陵科技学院机电工程学院,江苏南京 211169

搅拌摩擦焊 疲劳 裂纹扩展 疲劳试验

2024

机械制造与自动化
南京机械工程学会 南京机电产业(集团)有限公司

机械制造与自动化

CSTPCD
影响因子:0.29
ISSN:1671-5276
年,卷(期):2024.53(1)
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