The reduced weight and improved efficiency of modern aeronautical structures result in a decreasing separation of frequency ranges of rigid and elastic modes.Particularly,a high-aspect-ratio flexible flying wing is pr...The reduced weight and improved efficiency of modern aeronautical structures result in a decreasing separation of frequency ranges of rigid and elastic modes.Particularly,a high-aspect-ratio flexible flying wing is prone to body freedomflutter(BFF),which is a result of coupling of the rigid body short-periodmodewith 1st wing bendingmode.Accurate prediction of the BFF characteristics is helpful to reflect the attitude changes of the vehicle intuitively and design the active flutter suppression control law.Instead of using the rigid body mode,this work simulates the rigid bodymotion of the model by using the six-degree-of-freedom(6DOF)equation.A dynamicmesh generation strategy particularly suitable for BFF simulation of free flying aircraft is developed.An accurate Computational Fluid Dynamics/Computational Structural Dynamics/six-degree-of-freedom equation(CFD/CSD/6DOF)-based BFF prediction method is proposed.Firstly,the time-domain CFD/CSD method is used to calculate the static equilibrium state of the model.Based on this state,the CFD/CSD/6DOF equation is solved in time domain to evaluate the structural response of themodel.Then combinedwith the variable stiffnessmethod,the critical flutter point of the model is obtained.This method is applied to the BFF calculation of a flyingwing model.The calculation results of the BFF characteristics of the model agree well with those fromthe modalmethod andNastran software.Finally,the method is used to analyze the influence factors of BFF.The analysis results show that the flutter speed can be improved by either releasing plunge constraint or moving the center ofmass forward or increasing the pitch inertia.展开更多
针对船体密封舱、箱柜等狭窄空间普遍存在的机器人难以工作问题,提出了一种新型6-DOF(degrees of freedom)机器人。首先分析了该机器人的机械结构,基于D-H坐标理论建立了机器人D-H坐标表格以及机器人正、逆运动学方程,其次应用MATLAB对...针对船体密封舱、箱柜等狭窄空间普遍存在的机器人难以工作问题,提出了一种新型6-DOF(degrees of freedom)机器人。首先分析了该机器人的机械结构,基于D-H坐标理论建立了机器人D-H坐标表格以及机器人正、逆运动学方程,其次应用MATLAB对机器人的运动学进行了仿真,结果表明所得的机器人正、逆运动学方程完全正确;最后设计了虚拟样机,利用RobotStudio仿真分析了机器人箱体焊接的优点;为进一步验证设计的机器人运动性能,与通用6-DOF机器人做了对比分析。研究结果表明新型机器人运动的可行性,为设计适应箱柜等狭窄空间的工业机器人提供了理论依据。展开更多
基金This work was supported by the National Natural Science Foundation of China(No.11872212)and a project funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions.
文摘The reduced weight and improved efficiency of modern aeronautical structures result in a decreasing separation of frequency ranges of rigid and elastic modes.Particularly,a high-aspect-ratio flexible flying wing is prone to body freedomflutter(BFF),which is a result of coupling of the rigid body short-periodmodewith 1st wing bendingmode.Accurate prediction of the BFF characteristics is helpful to reflect the attitude changes of the vehicle intuitively and design the active flutter suppression control law.Instead of using the rigid body mode,this work simulates the rigid bodymotion of the model by using the six-degree-of-freedom(6DOF)equation.A dynamicmesh generation strategy particularly suitable for BFF simulation of free flying aircraft is developed.An accurate Computational Fluid Dynamics/Computational Structural Dynamics/six-degree-of-freedom equation(CFD/CSD/6DOF)-based BFF prediction method is proposed.Firstly,the time-domain CFD/CSD method is used to calculate the static equilibrium state of the model.Based on this state,the CFD/CSD/6DOF equation is solved in time domain to evaluate the structural response of themodel.Then combinedwith the variable stiffnessmethod,the critical flutter point of the model is obtained.This method is applied to the BFF calculation of a flyingwing model.The calculation results of the BFF characteristics of the model agree well with those fromthe modalmethod andNastran software.Finally,the method is used to analyze the influence factors of BFF.The analysis results show that the flutter speed can be improved by either releasing plunge constraint or moving the center ofmass forward or increasing the pitch inertia.
文摘针对船体密封舱、箱柜等狭窄空间普遍存在的机器人难以工作问题,提出了一种新型6-DOF(degrees of freedom)机器人。首先分析了该机器人的机械结构,基于D-H坐标理论建立了机器人D-H坐标表格以及机器人正、逆运动学方程,其次应用MATLAB对机器人的运动学进行了仿真,结果表明所得的机器人正、逆运动学方程完全正确;最后设计了虚拟样机,利用RobotStudio仿真分析了机器人箱体焊接的优点;为进一步验证设计的机器人运动性能,与通用6-DOF机器人做了对比分析。研究结果表明新型机器人运动的可行性,为设计适应箱柜等狭窄空间的工业机器人提供了理论依据。
