Modeling and Characteristics of Lateral Bending Vibration for Helicopter Tail Drive Shaft during Maneuvering Flight

摘要：

　　This paper proposed the description method of spatial motion for helicopter maneuver flight,and used the extended Hamiltons principle to establish the lateral bending vibration model of the helicopter oblique tail drive shaft.of which the horizontal shaft is a special case.The effect of spatial maneuver flight on the vibration characteristics of the tail drive shaft has discussed by the combination of mathematical model and numerical simulation.The study results reveal that the spatial maneuvering flight of helicopter will produce additional stiffness effect,damping effect and external excitation force on the bending vibration which may change the center position and size of the motion orbit of the tail drive shaft.

关键词： Helicopter tail drive shaft maneuver flight bending vibration

作者: De Ni Rupeng Zhu Guanghu Jin Fajia Li

作者单位: Jiangsu Key Laboratory of Precision and Micro-Manufacturing Technology,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China

会议类型: 国际会议

会议名称: The 9Th International Conference on Vibration Engineering and Technology of Machinery(第九届振动工程及机械科学技术国际会议)(VETOMAC-IX)

会议地点: 南京

会议语种:英文

页码: 1-6

在线出版日期: 2013-08-20（万方平台首次上网日期，不代表论文的发表时间）