Influence of Helicopter Maneuvering Flight on the Critical Speed of Tail Drive Shaft

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Journal of Vibration and Shock ›› 2016, Vol. 35 ›› Issue (11) : 109-115.

LU Feng-xia1 ZHU Ru-Peng1 NI De2

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Abstract

All the translational motion components of helicopter and the position parameters of tail drive shaft do not affect the critical speed of tail drive shaft, and only the rotational motion components of helicopter affect the critical speed of tail drive shaft. The influence of the rotational motion components of helicopter on the critical speed of tail drive shaft was analyzed. The results reveal that the yaw angular velocity with the critical speed of horizontal drive shaft is parabola relation, the yaw angular velocity with the critical speed of oblique drive shaft is linear relation and the relation curve is symmetrical. The symmetry axis will offset to the left as the increase of the inclination angle of oblique tail drive shaft. The influence of the pitching angular velocity on the critical speed of tail drive shaft is the same as yaw angular velocity. The relationship between the rolling angular velocity and the critical speed of horizontal drive shaft and oblique drive shaft are all linear relation, and the symmetry axis will offset to the right as the increase of the inclination angle of oblique tail drive shaft. The angular velocity of symmetry axis of the second-order critical speed of drive shaft is about 16 times of the first-order critical speed.

Key words

Helicopter / tail drive shaft / maneuvering flight / bending vibration / critical speed

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LU Feng-xia1 ZHU Ru-Peng1 NI De2 . Influence of Helicopter Maneuvering Flight on the Critical Speed of Tail Drive Shaft[J]. Journal of Vibration and Shock, 2016, 35(11): 109-115

References

[1] Lopez C A, Wells V L. Dynamics and stability of an autorotating rotor/wing unmanned aircraft[J]. Journal of Guidance, Control, and Dynamics, 2004, 27(2): 258-270.
[2] Ananthan S, Leishman J G. Rotor wake aerodynamics in large amplitude maneuvering flight[J]. Journal of the American Helicopter Society, 2006, 51(3): 225-243.
[3] 祝长生, 陈拥军. 机动飞行时航空发动机转子系统的振动特性[J]. 航空学报, 2006, 27(5): 825-841.
ZHU Chang-sheng, CHEN Yong-jun. Vibration characteristics of aeroengine’s rotor system during maneuvering flight[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(5): 825-841. (in Chinese)
[4] 祝长生, 陈拥军. 机动飞行时发动机转子系统动力学统一模型[J]. 航空动力学报, 2009, 24(2): 371-377.
ZHU Chang-sheng, CHEN Yong-jun. General dynamic model of aeroengine’s rotor system during maneuvering flight[J]. Journal of Aerospace Power, 2009, 24(2): 371-377. (in Chinese)
[5] 林富生, 孟光. 飞行器机动飞行时发动机转子等变速运动的动力学特性研究[J]. 航空学报, 2002, 23(4): 356-359.
LIN Fu-sheng, MENG Guang. Dynamics of a maneuvering rotor in constant acceleration and deceleration[J]. Acta Aeronautica et Ast ronautica Sinica, 2002, 23(4): 356-359. (in Chinese)
[6] LIN Fu-sheng, MENG Guang. Study on the dynamics of a rotor in a maneuvering aircraft[J]. Journal of Vibration and Acoustics, 2003, 125(2): 324-327.
[7] 林富生, 孟光, E•韩.飞行器内裂纹转子系统的非线性动力学特性研究[J]. 应用数学和力学, 2004, 25(10): 1042-1052.
LIN Fu-sheng, MENG Guang, Eric Hahn. Nonlinear dynamics of a cracked rotor in a maneuvering aircraft[J]. Applied Mathematics and Mechanics, 2004, 25(10): 1042-1052. (in Chinese)
[8] 林富生, 孟光. 飞行器内SFD-转子系统的动力学特性研究[J]. 振动工程学报, 2004, 17(4): 403-407.
LIN Fu-sheng, MENG Guang. Study on the dynamic characteristics of SFD-rotor system in aircrafts[J]. Journal of Vibration Engineering, 2004, 17(4): 403-407. (in Chinese)
[9] 林富生, 孟光. 飞行器内碰摩转子模型的光滑处理及非线性研究[J]. 振动工程学报, 2004, 17(2): 184-188.
LIN Fu-sheng, MENG Guang. Study on the nonlinear characteristics of a maneuvering rotor system with smoothly treated step impact-rubbing forces[J]. Journal of Vibration Engineering, 2004, 17(2): 184-188. (in Chinese)
[10] 徐敏, 廖明夫, 刘启洲. 机动飞行条件下双盘悬臂转子的振动特性[J]. 航空动力学报, 2002, 17(1): 105-109.
XU Min, LIAO Ming-fu, LIU Qi-zhou. The vibration performance of the double-disk cantilever rotor in flight mission[J]. Journal of Aerospace Power, 2002, 17(1): 105-109. (in Chinese)
[11] 徐敏, 廖明夫. 机动飞行条件下带挤压油膜阻尼器的Jeffcott 转子的振动特性[J]. 航空动力学报, 2003, 18(3): 394-401.
XU Min, LIAO Ming-fu. The vibration performance of the Jeffcott rotor system with SFD in maneuver flight[J]. Journal of Aerospace Power, 2003, 18(3): 394-401. (in Chinese)
[12] 顾致平, 于渊博. 飞机水平盘旋下弹性支承转子的特性研究[J]. 西安工业大学学报, 2008, 28(6): 589-593.
GU Zhi-ping, YU Yuan-bo. Investigation of rotor characteristics with elastic support in aircraft of horizontal circling[J]. Journal of Xi’an Technological University, 2008, 28(6): 589-593. (in Chinese)
[13] 杨永锋, 任兴民, 秦卫阳. 俯冲拉起下裂纹转子的非线性[J]. 振动与冲击, 2007, 26(4): 21-24.
YANG Yong-feng, REN Xing-min, QIN Wei-yang. Nonlinear response analysis of a cracked jeffcott rotor in action of dive-hike[J]. Journal of Vibration and Shock, 2007, 26(4): 21-24. (in Chinese)
[14] 杨永锋, 任兴民, 秦卫阳. 水平盘旋下裂纹转子的非线性响应[J]. 航空动力学报, 2007, 22(6): 1007-1012.
YANG Yong-feng, REN Xing-min, QIN Wei-yang. Study of nonlinear response of cracked Jeffcott rotor in hovering state[J]. Journal of Aerospace Power, 2007, 22(6): 1007-1012. (in Chinese)
[15] 许兆棠. 多支点传动轴动力学的研究[D]. 南京：南京航空航天大学, 2006.
XU Zhao-tang. Research on dynamics of a drive shaft with multi-supports[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2006. (in Chinese)
[16] 倪德, 朱如鹏, 靳广虎, 等. 机动飞行时直升机尾传动轴的横向振动建模与特性[J]. 振动与冲击, 2014, 33(7): 215-220.
NI De, ZHU Rupeng, JIN Guanghu, et al. Modeling and characteristics of bending vibration for helicopter tail drive shaft during maneuver flight[J]. Journal of Vibration and Shock, 2014, 33(7): 215-220. (in Chinese)