In order to decrease the impact on shooting accuracy caused by human factors in the machine gun type approval testing,a new type testing gun mount system was developed to replace gunner to conduct the automatic shooti...In order to decrease the impact on shooting accuracy caused by human factors in the machine gun type approval testing,a new type testing gun mount system was developed to replace gunner to conduct the automatic shooting.The finite element model was first established and then the natural characteristics of the system were obtained by calculation.On basis of calculation results,the modal testing system was set up and the experimental points,including the exciting points and the measure points were determined.Finally,modal experiment of the system was carried out and the experimental modal parameters were obtained.The simulation and experiment results indicate that the dynamic characteristics of the system have a rational matching with the shooting frequency and the finite element model were well demonstrated.The study provides a new way for shooting accuracy test in type approval testing of firearms and possesses reference value for dynamic modification and optimization design.展开更多
随着航天飞行器面临的力学环境愈发严酷,热与振动环境已成为造成结构损伤和破坏、产品功能下降或失效的关键因素。建立了一种考虑三轴振动与热复合环境的虚拟试验方法,以简化的筒形舱段为对象,分别建立石英灯阵高温加热仿真模型与三轴...随着航天飞行器面临的力学环境愈发严酷,热与振动环境已成为造成结构损伤和破坏、产品功能下降或失效的关键因素。建立了一种考虑三轴振动与热复合环境的虚拟试验方法,以简化的筒形舱段为对象,分别建立石英灯阵高温加热仿真模型与三轴振动仿真模型,并通过实际试验数据得到振动台-夹具传递函数,将三者结合以建立三轴虚拟热振仿真模型。分别通过舱段结构单轴热振试验与三轴热振试验来验证所建模型的准确性,并基于验证后的模型获取三轴振动下结构中央测点随温度时变的传递函数变化情况。由舱段模态试验验证舱段有限元模型的准确性,对比前6阶模态频率误差不超过5%。在单轴热振试验中,仿真模型各测点响应均方根值(root mean square,RMS)与试验加速度响应RMS的误差不超过15%;在三轴向热振试验中RMS误差不超过20%,验证了所建虚拟热振模型的有效性。展开更多
文摘In order to decrease the impact on shooting accuracy caused by human factors in the machine gun type approval testing,a new type testing gun mount system was developed to replace gunner to conduct the automatic shooting.The finite element model was first established and then the natural characteristics of the system were obtained by calculation.On basis of calculation results,the modal testing system was set up and the experimental points,including the exciting points and the measure points were determined.Finally,modal experiment of the system was carried out and the experimental modal parameters were obtained.The simulation and experiment results indicate that the dynamic characteristics of the system have a rational matching with the shooting frequency and the finite element model were well demonstrated.The study provides a new way for shooting accuracy test in type approval testing of firearms and possesses reference value for dynamic modification and optimization design.
文摘随着航天飞行器面临的力学环境愈发严酷,热与振动环境已成为造成结构损伤和破坏、产品功能下降或失效的关键因素。建立了一种考虑三轴振动与热复合环境的虚拟试验方法,以简化的筒形舱段为对象,分别建立石英灯阵高温加热仿真模型与三轴振动仿真模型,并通过实际试验数据得到振动台-夹具传递函数,将三者结合以建立三轴虚拟热振仿真模型。分别通过舱段结构单轴热振试验与三轴热振试验来验证所建模型的准确性,并基于验证后的模型获取三轴振动下结构中央测点随温度时变的传递函数变化情况。由舱段模态试验验证舱段有限元模型的准确性,对比前6阶模态频率误差不超过5%。在单轴热振试验中,仿真模型各测点响应均方根值(root mean square,RMS)与试验加速度响应RMS的误差不超过15%;在三轴向热振试验中RMS误差不超过20%,验证了所建虚拟热振模型的有效性。