Technical Papers
Jan 24, 2022

Study on Fretting Wear of Contact Interface of Curvic Coupling for Circumferential Rod Combined Rotor

Publication: Journal of Aerospace Engineering
Volume 35, Issue 3

Abstract

Fretting wear is a general surface damage form in tightly connected structures. Aimed at the curvic coupling of the disks in combined rotor gas turbine, using the finite-element method and Archard wear theory, the effects of the bolt preload, torque, and transverse vibration on the fretting characteristics of curvic coupling were studied. Additionally, the influences of a single mistuned tie rod and the material properties on the fretting characteristics of curvic coupling have been researched. Finally, a two-disk rotor experiment was carried out to make a comparative study with the simulation. The results showed that with the increase of preload and torque, the contact stress, slide distance, and wear depth gradually increased. Moreover, when the single rod was mistuned, it caused the uneven distribution of fretting characteristics in the circumferential direction. Compared with the Poisson’s ratio and density, the elastic modulus had a notable influences on the fretting characteristics. Comparing the experiment and the transverse lateral load simulation, the simulation results were consistent with the experimental results.

Get full access to this article

View all available purchase options and get full access to this article.

Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

This research was funded by the National Natural Science Foundation of China under Grant No. 11872288, Major projects of aviation engine and gas turbine No. J2019-IV-0021-0089, and the Shaanxi Provincial Natural Science Foundation under Grant No. 2019JM-219.

References

Choi, J. W., and C. S. Kim. 2011. “A study on the stability of curvic coupling for distance to disc in a millturret.” Appl. Mech. Mater. 2011 (100): 1498–1505. https://doi.org/10.4028/www.scientific.net/AMM.110-116.
Ding, J., I. R. McColl, S. B. Leen, and P. H. Shipway. 2007. “A finite element based approach to simulating the effects of debris on fretting wear.” Wear 263 (1–6): 481–491. https://doi.org/10.1016/j.wear.2006.12.056.
Jiang, X. J., Y. Y. Zhang, and S. X. Yuan. 2011. “An investigation and simulation of fretting wear of curvic in a gas turbine engine.” J. Harbin Inst. Technol. 2011 (3): 80–84. https://doi.org/10.1016/B978-0-444-53599-3.10006-X.
Johnson, K. L. 1985. Contact mechanics. London: Cambridge University Press.
Leen, S. B., T. R. Hyde, E. J. Williams, A. A. Becker, I. R. McColl, T. H. Hyde, and J. W. Taylor. 2000. “Development of a representative test specimen for frictional contact in spline joint couplings.” J. Strain Anal. 35 (6): 521–544. https://doi.org/10.1243/0309324001514279.
Li, A., H. Cui, W. Wen, and W. Shi. 2013a. “Prediction of fretting fatigue life based on nonlinear continuum damage mechanics.” Hangkong Xuebao/Acta Aeronaut. Astronaut. Sin. 34 (9): 2122–2129. https://doi.org/10.7527/S1000-6893.2013.0077.
Li, P., Q. J. X. Yuan, J. Gao, X. Liu, and Z. P. Feng. 2013b. “Contact stress analysis of curvic coupling of circumferential tie rotor.” Therm. Turbine 2013 (1): 27–31. https://doi.org/10.13707/j.cnki.31-1922/th.2013.01.010.
Lu, M. J., H. P. Geng, G. H. Xu, and L. Yu. 2017. “Analytical and experimental study on dynamic characters of rod-fastening rotor-bearing system under saturated pretension.” Zhendong Gongcheng Xuebao/J. Vib. Eng. 27 (1): 111–117. https://doi.org/10.16385/j.cnki.issn.1004-4523.2014.01.007.
Macbrien, W. 1992. CT7-9 turboprop training guide. Boston: GE Aircraft Engines.
Madge, J. J., S. B. Leen, and P. H. Shipway. 2007. “The critical role of wear in the analysis of fretting fatigue.” Wear 263 (1–6): 542–551. https://doi.org/10.1016/j.wear.2006.11.021.
McColl, I. R., J. Ding, and S. B. Leen. 2004. “Finite element simulation and experimental validation of fretting wear.” Wear 256 (11): 1114–1127. https://doi.org/10.1016/j.wear.2004.08.003.
Pisani, S. R., and J. J. Rencis. 2000. “Investigating curvic coupling behavior by utiling two and three-dimensional boundary and finite element methods.” Eng. Anal. Bound. Elem. 24 (3): 271–275. https://doi.org/10.1016/S0955-7997(99)00057-0.
Ratsimba, C. H. H., I. R. McColl, E. J. Williams, and S. B. Leen. 2004. “Measurement analysis and prediction of fretting damage in a representative aeroengine spline coupling.” Wear 257 (11): 1193–1206. https://doi.org/10.1016/j.wear.2004.08.003.
Richardson, I. J., T. H. Hyde, A. A. Becker, and J. W. Taylor. 2002. “A validation of the three-dimensional finite element contact method for use with curvic couplings.” Proc. Inst. Mech. Eng., Part G: J. Aerosp. Eng. 216 (2): 63–75. https://doi.org/10.1243/095441002760179771.
Shen, X., and P. Cao. 2017. “Contact state analysis of turboshaft engine rotor with curvic-coupling joint structure.” Aeroengine 43 (4): 35–40. https://doi.org/10.13477/j.cnki.aeroengine.2017.04.007.
Xue, X., S. Wang, and B. Li. 2016. “Modification methodology of fretting wear in involute spline.” Wear 5 (368–369): 435–444. https://doi.org/10.1016/j.wear.2016.10.015.
Yuan, Q., J. P. Gao, P. Li, Y. Liu, and Z. P. Feng. 2013a. “A review for structure and dynamic characteristics of heavy-duty gas turbine rotor.” Therm. Turbine 4 (12): 294–301. https://doi.org/10.13707/j.cnki.31-1922/th.2013.04.013.
Yuan, S., Y. X. Zhang, X. Jiang, and Y. Zhu. 2013b. “Analysis of bolt preload mistuned model and its impact on stress distribution of curvic couplings.” J. Harbin Inst. Technol. 45 (5): 70–75.
Yuan, S. X., Y. Y. Zhang, Y. C. Zhang, and X. J. Jiang. 2010. “Stress distribution and contact status analysis of a bolted rotor with curvic couplings.” Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci. 224 (9): 1815–1829. https://doi.org/10.1243/09544062JMES1853.
Zhang, P., W. X. Lu, X. Liu, M. Zhou, W. Zhai, G. Zhang, W. Zeng, and X. Jiang. 2017. “Torsional fretting wear behavior of CuNiAl against 42CrMo4 under flat on flat contact.” Wear 380–381 (Jun): 6–14. https://doi.org/10.1016/j.wear.2017.03.002.
Zhang, X. F. 1999. “Research on fretting damage: A review.” J. Nanjing Univ. Aeronaut. Astronaut. 31 (5): 545–551. https://doi.org/10.3969/j.issn.1005-2615.1999.05.011.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 35Issue 3May 2022

History

Received: Jun 22, 2021
Accepted: Nov 17, 2021
Published online: Jan 24, 2022
Published in print: May 1, 2022
Discussion open until: Jun 24, 2022

Permissions

Request permissions for this article.

Authors

Affiliations

Associate Professor, State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiaotong Univ., Xi’an, Shaanxi 710049, PR China; Shanxi Key Laboratory of Environment and Control for Flight Vehicle, Xi’an, Shaanxi 710049, PR China; School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an, Shaanxi 710049, PR China (corresponding author). Email: [email protected]
Wei Wu, Ph.D. [email protected]
State Key Laboratory for Strength and Vibration of Mechanical Strucurtes, Xi’an Jiaotong Univ., Xi’an, Shaanxi 710049, PR China. Email: [email protected]
School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an, Shaanxi 710049, PR China. Email: [email protected]
Zhenfa Wang [email protected]
School of Aerospace Engineering, Xi’an Jiaotong Univ., Xi’an, Shaanxi 710049, PR China. Email: [email protected]
The 404 Company Ltd., CNNC (China National Nuclear Corporation), Hecheng West Rd., Jiayuguan, Gansu 7335100, PR China. Email: [email protected]

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share