In order to analyze the effects of forward-swept angle and skin ply-orientation on the static and dynamic aeroelastic characteristics, the aeroelastic modeling and calculation for high-aspect-ratio composite wings wit...In order to analyze the effects of forward-swept angle and skin ply-orientation on the static and dynamic aeroelastic characteristics, the aeroelastic modeling and calculation for high-aspect-ratio composite wings with different forward-swept angles and skin ply-orientation are performed. This paper presents the results of a design study aiming to optimize wings with typical forward-swept angles and skin ply-orientation in an aeroelastic way by using the genetic/sensitivity-based hybrid algorithm. Under the conditions of satiated multiple constraints including strength, displacements, divergence speeds and flutter speeds, the studies are carried out in a bid to minimize the structural weight of a wing with the lay-up thicknesses of wing components as design variabies. In addition, the effects of the power of spanwise variation function of lay-up thicknesses of skins and iugs on the optimized weights are also analyzed.展开更多
针对高速电主轴动态模型中耦合电压的非线性变化对主轴动态性能所产生的影响,通过对比前馈控制和内模控制(Internal model control,IMC)的电压解耦机理,指出IMC能够避免前馈控制时电压解耦效果依赖主轴模型参数与实际参数相匹配的不足,...针对高速电主轴动态模型中耦合电压的非线性变化对主轴动态性能所产生的影响,通过对比前馈控制和内模控制(Internal model control,IMC)的电压解耦机理,指出IMC能够避免前馈控制时电压解耦效果依赖主轴模型参数与实际参数相匹配的不足,并利用170MD15Y20油雾润滑型电主轴和Matlab/Simulink软件分别对两种控制方法进行试验和仿真分析。结果表明,主轴的耦合电压主要受频率和转矩电流变化的影响,改变磁链子系统和转矩子系统的给定电压、以及耦合回路中无功功率在输入功率中的比例,不仅可以对主轴的功率因素、输出转矩、抗扰动能力和动态速度跟随精度等特性参数产生影响,而且使主轴的转矩脉动程度、带负载能力和转差率等随耦合电压的大小成反比例变化。因此可以根据包含上述特征信息的机械特性曲线、功率因素曲线和恒转矩曲线的变化趋势,准确判断高速电主轴的解耦效果,并预测主轴在该控制方式下的动态性能。展开更多
文摘In order to analyze the effects of forward-swept angle and skin ply-orientation on the static and dynamic aeroelastic characteristics, the aeroelastic modeling and calculation for high-aspect-ratio composite wings with different forward-swept angles and skin ply-orientation are performed. This paper presents the results of a design study aiming to optimize wings with typical forward-swept angles and skin ply-orientation in an aeroelastic way by using the genetic/sensitivity-based hybrid algorithm. Under the conditions of satiated multiple constraints including strength, displacements, divergence speeds and flutter speeds, the studies are carried out in a bid to minimize the structural weight of a wing with the lay-up thicknesses of wing components as design variabies. In addition, the effects of the power of spanwise variation function of lay-up thicknesses of skins and iugs on the optimized weights are also analyzed.
文摘针对高速电主轴动态模型中耦合电压的非线性变化对主轴动态性能所产生的影响,通过对比前馈控制和内模控制(Internal model control,IMC)的电压解耦机理,指出IMC能够避免前馈控制时电压解耦效果依赖主轴模型参数与实际参数相匹配的不足,并利用170MD15Y20油雾润滑型电主轴和Matlab/Simulink软件分别对两种控制方法进行试验和仿真分析。结果表明,主轴的耦合电压主要受频率和转矩电流变化的影响,改变磁链子系统和转矩子系统的给定电压、以及耦合回路中无功功率在输入功率中的比例,不仅可以对主轴的功率因素、输出转矩、抗扰动能力和动态速度跟随精度等特性参数产生影响,而且使主轴的转矩脉动程度、带负载能力和转差率等随耦合电压的大小成反比例变化。因此可以根据包含上述特征信息的机械特性曲线、功率因素曲线和恒转矩曲线的变化趋势,准确判断高速电主轴的解耦效果,并预测主轴在该控制方式下的动态性能。
