采煤机摇臂壳体是采煤机的重要部件及薄弱环节,其寿命直接影响采煤机的工作性能。为研究采煤机截割复杂煤层时滚筒所受载荷对其摇臂壳体寿命的影响,以MG325型采煤机截割兖州矿区杨村煤矿17层含夹矸煤壁为工程背景,通过虚拟样机技术和离...采煤机摇臂壳体是采煤机的重要部件及薄弱环节,其寿命直接影响采煤机的工作性能。为研究采煤机截割复杂煤层时滚筒所受载荷对其摇臂壳体寿命的影响,以MG325型采煤机截割兖州矿区杨村煤矿17层含夹矸煤壁为工程背景,通过虚拟样机技术和离散单元法-多柔体动力学(Discrete Element Method-Multi Flexible Body Dynamics,DEM-MFBD)双向耦合技术,利用离散元仿真软件EDEM和多体系统动力学仿真软件RecurDyn,基于实际工况获得采煤机螺旋滚筒的外负载。在RecurDyn仿真平台中,建立采煤机摇臂三维实体模型并进行边界条件的设置及摇臂壳体的柔性化,通过软件本身的Durability疲劳耐久分析模块,计算摇臂壳体的疲劳寿命。利用专业绘图软件Origin绘制2个软件后处理的载荷曲线图,发现其走势较为一致,其后处理数据均值,标准差等相接近,证明两者耦合效果较好。结果表明:MG325型采煤机以滚筒转速83.5 r/min,截深600 mm,牵引速度5 m/min截割复杂煤层时,滚筒所受载荷具有较为强烈的载荷波动现象,由等效应力云图可得摇臂壳体的最大等效应力为230.51 MPa,且应力较大处集中位于壳体的各个齿轮轴孔处、凹槽处以及上下耳过渡处,经应力疲劳分析后得其最小寿命位于壳体的齿轮轴孔处,循环次数为8.3215×10~6次。本研究方法可为复杂条件下工矿装备大型结构件的优化设计提供参考。展开更多
掘进机回转台在截割煤岩时承受偏载荷及强冲击作用,其性能影响掘进机的工作效率及安全性。为探究掘进机回转台疲劳寿命的影响因素及最佳服役参数,提出了一种基于Kriging代理模型和DEM-MFBD(discrete element model-multi flexible body ...掘进机回转台在截割煤岩时承受偏载荷及强冲击作用,其性能影响掘进机的工作效率及安全性。为探究掘进机回转台疲劳寿命的影响因素及最佳服役参数,提出了一种基于Kriging代理模型和DEM-MFBD(discrete element model-multi flexible body dynamics,离散单元法-多柔性体动力学)双向耦合技术的回转台疲劳寿命预测方法。首先,建立了掘进机截割部与回转台的空间受力模型,明确了截割部与回转台的受力规律。然后,联合RecurDyn与EDEM软件对回转台进行双向刚柔耦合动力学仿真分析,获得了回转台在工作状态下的应力分布。最后,利用拉丁超立方抽样法选取15组掘进机服役参数作为输入,以回转台疲劳寿命为响应,建立了对应的Kriging代理模型,并利用粒子群优化算法对代理模型进行寻优,得到了回转台在最佳服役参数下的疲劳寿命。结果表明,当掘进机的截割头转速为54 r/min、回转台横摆速度为1.003 m/min、截割臂垂直摆角为7°时,回转台的疲劳寿命最长。结合DEM-MFBD双向耦合技术、Kriging代理模型与粒子群优化算法来探究掘进机的最佳服役参数,可为回转类部件的优化设计提供新思路。展开更多
In order to provide accurate launching pitching angular velocity（LPAV） for the exterior trajectory optimization design, multi-flexible body dynamics（MFBD） technology is presented to study the changing law of LPAV ...In order to provide accurate launching pitching angular velocity（LPAV） for the exterior trajectory optimization design, multi-flexible body dynamics（MFBD） technology is presented to study the changing law of LPAV of the rotating missile based on spiral guideway. An MFBD virtual prototype model of the rotating missile launching system is built using multi-body dynamics modeling technology based on the built flexible body models of key components and the special force model.The built model is verified with the frequency spectrum analysis. With the flexible body contact theory and nonlinear theory of MFBD technology, the research is conducted on the influence of a series of factors on LPAV, such as launching angle change, clearance between launching canister and missile,thrust change, thrust eccentricity and mass eccentricity, etc. Through this research, some useful values of the key design parameters which are difficult to be measured in physical tests are obtained. Finally,a simplified mathematical model of the changing law of LPAV is presented through fitting virtual test results using the linear regression method and verified by physical flight tests. The research results have important significance for the exterior trajectory optimization design.展开更多
文摘采煤机摇臂壳体是采煤机的重要部件及薄弱环节,其寿命直接影响采煤机的工作性能。为研究采煤机截割复杂煤层时滚筒所受载荷对其摇臂壳体寿命的影响,以MG325型采煤机截割兖州矿区杨村煤矿17层含夹矸煤壁为工程背景,通过虚拟样机技术和离散单元法-多柔体动力学(Discrete Element Method-Multi Flexible Body Dynamics,DEM-MFBD)双向耦合技术,利用离散元仿真软件EDEM和多体系统动力学仿真软件RecurDyn,基于实际工况获得采煤机螺旋滚筒的外负载。在RecurDyn仿真平台中,建立采煤机摇臂三维实体模型并进行边界条件的设置及摇臂壳体的柔性化,通过软件本身的Durability疲劳耐久分析模块,计算摇臂壳体的疲劳寿命。利用专业绘图软件Origin绘制2个软件后处理的载荷曲线图,发现其走势较为一致,其后处理数据均值,标准差等相接近,证明两者耦合效果较好。结果表明:MG325型采煤机以滚筒转速83.5 r/min,截深600 mm,牵引速度5 m/min截割复杂煤层时,滚筒所受载荷具有较为强烈的载荷波动现象,由等效应力云图可得摇臂壳体的最大等效应力为230.51 MPa,且应力较大处集中位于壳体的各个齿轮轴孔处、凹槽处以及上下耳过渡处,经应力疲劳分析后得其最小寿命位于壳体的齿轮轴孔处,循环次数为8.3215×10~6次。本研究方法可为复杂条件下工矿装备大型结构件的优化设计提供参考。
文摘掘进机回转台在截割煤岩时承受偏载荷及强冲击作用,其性能影响掘进机的工作效率及安全性。为探究掘进机回转台疲劳寿命的影响因素及最佳服役参数,提出了一种基于Kriging代理模型和DEM-MFBD(discrete element model-multi flexible body dynamics,离散单元法-多柔性体动力学)双向耦合技术的回转台疲劳寿命预测方法。首先,建立了掘进机截割部与回转台的空间受力模型,明确了截割部与回转台的受力规律。然后,联合RecurDyn与EDEM软件对回转台进行双向刚柔耦合动力学仿真分析,获得了回转台在工作状态下的应力分布。最后,利用拉丁超立方抽样法选取15组掘进机服役参数作为输入,以回转台疲劳寿命为响应,建立了对应的Kriging代理模型,并利用粒子群优化算法对代理模型进行寻优,得到了回转台在最佳服役参数下的疲劳寿命。结果表明,当掘进机的截割头转速为54 r/min、回转台横摆速度为1.003 m/min、截割臂垂直摆角为7°时,回转台的疲劳寿命最长。结合DEM-MFBD双向耦合技术、Kriging代理模型与粒子群优化算法来探究掘进机的最佳服役参数,可为回转类部件的优化设计提供新思路。
基金supported by the Key Special Funds for National Defense Basic Scientific Research of China (No. C0320110005)
文摘In order to provide accurate launching pitching angular velocity（LPAV） for the exterior trajectory optimization design, multi-flexible body dynamics（MFBD） technology is presented to study the changing law of LPAV of the rotating missile based on spiral guideway. An MFBD virtual prototype model of the rotating missile launching system is built using multi-body dynamics modeling technology based on the built flexible body models of key components and the special force model.The built model is verified with the frequency spectrum analysis. With the flexible body contact theory and nonlinear theory of MFBD technology, the research is conducted on the influence of a series of factors on LPAV, such as launching angle change, clearance between launching canister and missile,thrust change, thrust eccentricity and mass eccentricity, etc. Through this research, some useful values of the key design parameters which are difficult to be measured in physical tests are obtained. Finally,a simplified mathematical model of the changing law of LPAV is presented through fitting virtual test results using the linear regression method and verified by physical flight tests. The research results have important significance for the exterior trajectory optimization design.
