旋转自紧身管承载性能及工艺参数优化研究OA
Research on Load-Bearing Performance and Process Parameter Optimization of Rotational Autofrettage Gun Barrel
为阐明旋转自紧技术提升火炮身管承载性能的机制,本研究建立了普通身管在膛压载荷下的有限元应力分布模型,并系统对比了不同角速度自紧处理后残余应力场的演化规律.进一步对经自紧处理的身管分别施加450 MPa和320 MPa膛压,计算了其发射过程中的应力响应.研究中提出了基于Mises屈服准则的塑性半径理论修正方法,有效解决了传统Tresca准则的理论解误差问题,修正结果与数值模拟高度吻合.通过量化分析等效应力峰值与自紧工艺参数的关联性,最终确定了该身管旋转自紧工艺的最佳角速度窗口(4 680~5 205 rad·s-1)及最佳自紧度区间(32%~97%),为工程应用提供了关键设计依据.
To elucidate the mechanism enhancing the load-bearing performance of gun barrels by rota-tional autofrettage technology,this study established a finite element model characterizing the stress distri-bution in normal barrels under chamber pressure.A systematic comparative analysis was conducted on the evolution of residual stress fields following autofrettage treatment at varying angular velocities.Subse-quently,chamber pressures of 450 MPa and 320 MPa were applied to the autofrettaged barrels to com-pute their stress responses during simulated firing.The research proposed a theoretical correction method for the plastic radius based on the Von-Mises yield criterion,effectively resolving the inaccuracies inherent in solutions derived from the traditional Tresca criterion.The corrected theoretical results showed excel-lent agreement with numerical simulations.By quantitatively analyzing the correlation between peak Von-Mises stress and autofrettage process parameters,the optimal angular velocity window(4 680~5 205 rad·s-1)and optimal overstrain range(32%~97%)for the rotational autofrettage process of the studied barrel were determined.These findings provide a critical design basis for engineering applications.
常列珍;马新谋
中北大学 航空宇航学院,山西 太原 030051中北大学 智能武器研究院,山西 太原 030051
通用工业技术
旋转自紧身管残余应力自紧度
rotational autofrettagegun barrelresidual stressautofrettage degree
《中北大学学报(自然科学版)》 2026 (1)
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