Vibration Characteristics Analysis of a Pair of Aviation Herringbone Gears

Ning Zhao; Chen Xi Fu; Yong Zhi Zhao; Meng Qi Zhang

doi:10.4028/www.scientific.net/AMR.706-708.1666

Paper Titles

The Study and Application of Comprehensive Evaluation of Regional Power Grid Power Quality
p.1644

The Mechanical Excavator - Hydraulic System of the Establishment of Co-Simulation and Optimization
p.1651

Topological Optimization Design of the Vertical Machining Center Workbench Based on ANSYS
p.1657

VDT and its Application to Container Loading Device
p.1662

Vibration Characteristics Analysis of a Pair of Aviation Herringbone Gears
p.1666

Vibration Control in Turning Machining
p.1672

Virtual Prototype Based Fatigue Life Research on some Missile Erecting System
p.1676

Force Analysis of Pulp Fiber Particle in the Flow Field and Eulerian Two-Phase Flow Equation
p.1680

P Wave Propagation in the Functionally Graded Materials
p.1685

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 706-708Vibration Characteristics Analysis of a Pair of...

Vibration Characteristics Analysis of a Pair of Aviation Herringbone Gears

Abstract:

The lumped mass model of an aviation herringbone gear is established, which takes coupling relationship between the two helical gear into consideration. Based on this model, motional differential equation is derived, and excitation parameters of gear pair are calculated at the same time. The dynamic differential equations are solved to obtain the dynamic response of each degree of freedom, then vibration characteristics of aviation herringbone gear in different speed and power is analyzed and the appropriate rotational speed and power of different flight status is determined. Research on the reliability analysis of aviation herringbone gear and the dynamic efficiency analysis is of great significance.

You might also be interested in these eBooks

Mechatronics and Intelligent Materials III

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 706-708)

Pages:

1666-1671

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.706-708.1666

Citation:

Cite this paper

Online since:

June 2013

Authors:

Ning Zhao, Chen Xi Fu, Yong Zhi Zhao, Meng Qi Zhang

Keywords:

Aviation, Herringbone Gear, Power, Rotational Speed, Vibration Characteristics

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] H.N. Ozguven and D.R. Houser. Mathematical Models Used in Gear in Dynamics-A Review [J]. Journal of Sound and Vibration, 1988, 121(3): 384-411.

DOI: 10.1016/s0022-460x(88)80365-1

Google Scholar

[2] J.B. Amendola. Single vs Double Helical Gears [J]. Turbomachinery International, 2006, 47(5): 34-38.

Google Scholar

[3] Xinyue Wu and Shijian Zhu. Theoretical Vibration Pattern of Herringbone Gearing [J]. Journal of Naval University of Engineering, 2001, 13(5): 13-19. (in Chinese)

Google Scholar

[4] Zhonghong Bu, Geng Liu and Liyan Wu. Modal Analyses of Herringbone Planetary Gear Train with Journal Bearings [J]. Mechanism and Machine Theory, 2012, 54: 99-115.

DOI: 10.1016/j.mechmachtheory.2012.03.006

Google Scholar

[5] Kish. Sikorsky Aircraft Advanced Rotorcraft Transmission (ART) Program-final Report. NASA CR-191079, ARL-CR-49, 1993.

Google Scholar

[6] Zhonghong Bu, Geng Liu, Liyan Wu, et al. A Modified Method for Determining the Mesh Stiffness and Load Distribution of a Cylinder Gear Based on Linear Programming [J]. Mechanical Science and Technology for Aerospace Engineering, 2008, 27(11): 1365-1368. (in Chinese)

Google Scholar

[7] Runfang Li, Zeguang Tao, Tengjiao Lin, et al. Numerical Simulation for Inner Dynamic Excitation of Gearing [J]. Mechanical Transmission, 2001, 25(2): 1-3. (in Chinese)

Google Scholar

[8] A. Baje and L. Demkowicz. Dynamic Contact/Impact Problems, Energy Conservation, and Planetary Gear Trains [J]. Comp. Meth. Appl. Mech. Eng. 2002, 191: 4159-4191.

DOI: 10.1016/s0045-7825(02)00359-6

Google Scholar