With the rapid advancement of electromagnetic launch technology,enhancing the structural stability and thermal resistance of armatures has become essential for improving the overall efficiency and reliability of railg...With the rapid advancement of electromagnetic launch technology,enhancing the structural stability and thermal resistance of armatures has become essential for improving the overall efficiency and reliability of railgun systems.Traditional aluminum alloy armatures often suffer from severe ablation,deformation,and uneven current distribution under high pulsed currents,which limit their performance and service life.To address these challenges,this study employs the Johnson–Cook constitutive model and the finite element method to develop armature models of aluminum matrix composites with varying heterogeneous graphene volume fractions.The temperature,stress,and strain of the armatures during operation were analyzed to investigate the effects of different graphene volume fractions on the deformation and damage behavior of aluminum matrix composite armatures under the multi-field coupling of electromagnetic,thermal,and structural interactions.The results indicate that,compared to the 6061 aluminum alloy matrix,the graphene-reinforced aluminum matrix composite armature significantly suppresses ablation damage at the tail and throat edges.The incorporation of graphene notably reduces the temperature rise during the armature emission process,increases the muzzle velocity under identical current excitation,and mitigates directional deformation of the armature.The 1 wt.% graphene-reinforced aluminum matrix composite armature demonstrates better agreement with experimental results at a strain rate of 2000 s^(-1),while simultaneously improving stress-strain response,reducing temperature rise,and improving velocity performance.展开更多
为了掌握轨道电磁发射中电枢的电流熔蚀特性,对小口径电磁轨道发射装置进行了实验研究。实验装置为20 mm×20 mm,方形口径轨道电磁发射装置,通过控制发射实验中电枢出膛的速度,研究了电流幅值、电枢质量和转角厚度（载流能力）等因...为了掌握轨道电磁发射中电枢的电流熔蚀特性,对小口径电磁轨道发射装置进行了实验研究。实验装置为20 mm×20 mm,方形口径轨道电磁发射装置,通过控制发射实验中电枢出膛的速度,研究了电流幅值、电枢质量和转角厚度（载流能力）等因素对熔蚀的贡献。另外,基于电流幅值递增实验,总结了熔蚀程度的几种模型和相应的电流幅值范围。结果表明：不同的发射条件对电枢的熔蚀程度影响有所差异;电流分布是熔蚀产生的直接原因,能显著影响熔蚀程度;电枢质量对起始时刻的熔蚀有影响;电枢转角厚度对熔蚀的贡献不大（电枢载流能力足够的情况下）;随着电流幅值的增加,电枢表面熔蚀有从电枢中端偏下位置沿棱边向电枢中部和电枢头部延伸的趋势,在此过程中归纳出了3种熔蚀程度及其对应电流范围：轻度熔蚀,对应电流181-293.8 k A;中度熔蚀,对应电流293.8-320.8 k A;极度熔蚀,电流〉320.8 k A。展开更多
基金funded Basic Research Projects of Higher Education Institutions in Liaoning Province(JYTZD20230004)Future Industry Frontier Technology Project in Liaoning Province in 2025(2025JH2/101330141)Key Research and Development Program of Liaoning Province in 2025.
文摘With the rapid advancement of electromagnetic launch technology,enhancing the structural stability and thermal resistance of armatures has become essential for improving the overall efficiency and reliability of railgun systems.Traditional aluminum alloy armatures often suffer from severe ablation,deformation,and uneven current distribution under high pulsed currents,which limit their performance and service life.To address these challenges,this study employs the Johnson–Cook constitutive model and the finite element method to develop armature models of aluminum matrix composites with varying heterogeneous graphene volume fractions.The temperature,stress,and strain of the armatures during operation were analyzed to investigate the effects of different graphene volume fractions on the deformation and damage behavior of aluminum matrix composite armatures under the multi-field coupling of electromagnetic,thermal,and structural interactions.The results indicate that,compared to the 6061 aluminum alloy matrix,the graphene-reinforced aluminum matrix composite armature significantly suppresses ablation damage at the tail and throat edges.The incorporation of graphene notably reduces the temperature rise during the armature emission process,increases the muzzle velocity under identical current excitation,and mitigates directional deformation of the armature.The 1 wt.% graphene-reinforced aluminum matrix composite armature demonstrates better agreement with experimental results at a strain rate of 2000 s^(-1),while simultaneously improving stress-strain response,reducing temperature rise,and improving velocity performance.
文摘为了掌握轨道电磁发射中电枢的电流熔蚀特性,对小口径电磁轨道发射装置进行了实验研究。实验装置为20 mm×20 mm,方形口径轨道电磁发射装置,通过控制发射实验中电枢出膛的速度,研究了电流幅值、电枢质量和转角厚度（载流能力）等因素对熔蚀的贡献。另外,基于电流幅值递增实验,总结了熔蚀程度的几种模型和相应的电流幅值范围。结果表明：不同的发射条件对电枢的熔蚀程度影响有所差异;电流分布是熔蚀产生的直接原因,能显著影响熔蚀程度;电枢质量对起始时刻的熔蚀有影响;电枢转角厚度对熔蚀的贡献不大（电枢载流能力足够的情况下）;随着电流幅值的增加,电枢表面熔蚀有从电枢中端偏下位置沿棱边向电枢中部和电枢头部延伸的趋势,在此过程中归纳出了3种熔蚀程度及其对应电流范围：轻度熔蚀,对应电流181-293.8 k A;中度熔蚀,对应电流293.8-320.8 k A;极度熔蚀,电流〉320.8 k A。
