Abstract
This paper presents a dynamic modeling method of a gear transmission system considering the barrel roll flight environment. The kinematic equations of gear transmission system component are derived under non-inertial frame. The dynamics model of the gear rotor transmission system with time-varying positions was established using Lagrange energy method, and derived the gear transmission system dynamic contact stress calculation model combined with Hertz formula. The influence laws of barrel rolling acceleration and radius parameters on vibration response, axis trajectory, bearing support force and dynamic contact stress were solved and studied. The results show that considering maneuvering flight conditions, the frequency spectrum of vibration response appears time-varying rotation excitation frequency. The trajectory of the axis deviates with the barrel rolling parameters in different directions, and the influence of the driven gear with larger mass is more significant. The airframe flight will also affect the value and direction of the bearing’s supporting force vector, and the dynamic contact stress increases with the amplification of barrel radius. This paper provides a theoretical basis for the dynamic stress calculation and reliability design of gear transmission in time-varying positions.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Jie, G., Peishen, Z., Zhenghong, G.: Advanced Flight Dynamics. National Defense Industry Press, Beijing (2004)
Kufeld, R., Bousman, W.: High load conditions measured on a UH-60A in maneuvering flight. J. Am. Helicopter Soc. 43(03), 202–211 (1995)
Okamoto, S., Sakata, M., Kimura, K., et al.: Vibration analysis of a high speed and light weight rotor system subjected to a pitching or turning motion. J. Sound Vib. 184(05), 871–885 (1995)
Duchemin, M., Berlioz, A., Ferraris, G.: Dynamic behavior and stability of a rotor under base excitation. J. Vib. Acoust. 128(05), 576–585 (2006)
Dakel, M., Baguet, S., Dufour, R.: Steady-state dynamic behavior of an on-board rotor under combined base motions. J. Vib. Control 20(15), 2254–2287 (2004)
Soni, T., Dutt, J., Das, A.: Parametric stability analysis of active magnetic bearing-supported rotor system with a novel control law subject to periodic base motion. IEEE Trans. Indu. Electron. 67(02), 1160–1170 (2019)
Zhang, A., Wei, J., Shi, L., et al.: Modeling and dynamic response of parallel shaft gear transmission in non-inertial system. Nonlinear Dyn. 98(2), 997–1017 (2019)
Zhang, C.: Mechanical Principle and Mechanical Design, 3rd edn. China Machine Press, Beijing (2018)
Acknowledgments
The author is grateful for the support of the National Natural Science Foundation of China (grant number 51775058), the National Key R&D Program of China (No. 2020YFB2008101) and Innovation Group Science Foundation of Chongqing Natural Science Foundation (No. cstc2019jcyj-cxttX0003).
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2022 The Author(s), under exclusive license to Springer Nature Switzerland AG
About this paper
Cite this paper
Cheng, H., Wei, J., Zhang, A., Peng, B. (2022). Dynamic Response of Gear Transmission System under Barrel Rolling Flight Environment. In: Khang, N.V., Hoang, N.Q., Ceccarelli, M. (eds) Advances in Asian Mechanism and Machine Science. ASIAN MMS 2021. Mechanisms and Machine Science, vol 113. Springer, Cham. https://doi.org/10.1007/978-3-030-91892-7_15
Download citation
DOI: https://doi.org/10.1007/978-3-030-91892-7_15
Published:
Publisher Name: Springer, Cham
Print ISBN: 978-3-030-91891-0
Online ISBN: 978-3-030-91892-7
eBook Packages: EngineeringEngineering (R0)