Dynamic Response Analysis of Turbocharger Rotor of UAV during Hovering Movements

摘要：

　　A model of turbocharger rotor of Unmanned Aerial Vehicle (UAV) under hovering movement is presented,while Runge-Kutta numerical method is applied to solve the equation,and the dynamic response analysis under different rotating speeds in a hovering state is developed.The result shows,disk center trajectory of the turbocharger rotor is changed significantly because of UAV horizontal hovering movement,and rotor vibration amplitude varies at different rotating speeds.

关键词： UAV turbocharger rotor hovering dynamical response

作者: Jiao Yang Shu-Qian Cao

作者单位: School of Mechanical Engineering, Tianjin University, Tianjin, China Tianjin Key Laboratory of Nonlinear Dynamics and Chaos Control, Tianjin, China

会议类型: 国际会议

会议名称: 第16届机电一体化技术国际会议

会议地点: 天津

会议语种:英文

页码: 472-476

在线出版日期: 2012-10-16（万方平台首次上网日期，不代表论文的发表时间）