Experiment study on traveling wave resonance of fatigue fracture of high-speed bevel gear in aero-engne based on acoustic measurement method-CSCIED科技核心评价数据库-手机版

Experiment study on traveling wave resonance of fatigue fracture of high-speed bevel gear in aero-engne based on acoustic measurement method

Experiment study on traveling wave resonance of fatigue fracture of high-speed bevel gear in aero-engne based on acoustic measurement method

ES评分 0 浏览量：32 下载量：0

全文阅读下载引用收藏

DOI	10.1016/j.jsv.2021.116345
刊名	Journal of Sound and Vibration
年，卷(期)	2021, 511()
作者	LUAN Xiaochi1,2,Liu Gongmin1,SHA Yundong2,He Hongbin2,Guo Xiaopeng3,
作者单位	1. Harbin Engineering University. 2.Shenyang Aerospace University; 3.Shenyang Engine Research Institute;
摘要	High-speed, light-weight and high-load gearing is widely used in the transmission systems of modern aero-engines. Some dynamic phenomena, such as the traveling wave resonance, can be more easily encountered. It generally occurs quite suddenly and causes catastrophic accidents. This study presents an experimental investigation of the signal characteristics of the gear fatigue fracture process caused by the traveling wave resonance. The acoustic waveguide system and the dynamic calibration system are developed. The traveling wave resonance monitoring test and the fatigue performance test of the central drive bevel gear in an aero-engine are carried out. The results show the traveling wave resonant frequency and rotational speed of the driven bevel gear are identified and monitored effectively by the acoustic waveguide system. The dangerous rotational speeds range and the sound pressure energy radiated of the vibration are discussed. The results reveal the gear resonant phenomena are narrow rotational speed band sensitivity and more dangerous at high speed. The fracture mode of the driven bevel gear of aero-engine is reproduced. When the gear has initial defects and works within the dangerous rotational speed of the traveling wave resonance, the gear fatigue fracture will occur quickly. The harmonic frequency, the frequency of forward traveling wave (FTW) and backward traveling wave (BTW), and their combination frequency will appear alternately in the noise spectrum of the gear before fatigue fracture.
Abstract	High-speed, light-weight and high-load gearing is widely used in the transmission systems of modern aero-engines. Some dynamic phenomena, such as the traveling wave resonance, can be more easily encountered. It generally occurs quite suddenly and causes catastrophic accidents. This study presents an experimental investigation of the signal characteristics of the gear fatigue fracture process caused by the traveling wave resonance. The acoustic waveguide system and the dynamic calibration system are developed. The traveling wave resonance monitoring test and the fatigue performance test of the central drive bevel gear in an aero-engine are carried out. The results show the traveling wave resonant frequency and rotational speed of the driven bevel gear are identified and monitored effectively by the acoustic waveguide system. The dangerous rotational speeds range and the sound pressure energy radiated of the vibration are discussed. The results reveal the gear resonant phenomena are narrow rotational speed band sensitivity and more dangerous at high speed. The fracture mode of the driven bevel gear of aero-engine is reproduced. When the gear has initial defects and works within the dangerous rotational speed of the traveling wave resonance, the gear fatigue fracture will occur quickly. The harmonic frequency, the frequency of forward traveling wave (FTW) and backward traveling wave (BTW), and their combination frequency will appear alternately in the noise spectrum of the gear before fatigue fracture.
关键词	Aero-engine; Bevel gear; Traveling wave resonance; Fatigue fracture; Acoustic measurement method
KeyWord	Aero-engine; Bevel gear; Traveling wave resonance; Fatigue fracture; Acoustic measurement method
基金项目
页码	116345-

参考文献
相关文献

[1] R.J. Drago, F.W. Brown, The analytical and experimental evaluation of resonant re-sponse in high-speed, lightweight, highly loaded gearing, J. Mech. Design.

103 (2) (1981) 346–356, https://doi.org/10.1115/1.3254914.

[2] H.D. Joshi, K.D. Kothari, Mode and cause of failure of a bevel gear-a review, Adv. Eng. Res. Dev. 1 (2) (2014) 1–9.

[3] P.J.L. Fernandes, Tooth bending fatigue failures in gears, Eng. Fail. Anal. 3 (3) (1996) 219–225, https://doi.org/10.1016/1350-6307(96)00008-8.

[4] N.A. Siddiqui, K M Deen, M.Z. Khan, Investigating the failure of bevel gears in an aircraft engine, Case. Stud. Eng. Fail. Anal. 1 (1) (2013) 24–31, https://doi.

org/10.1016/j.csefa.2012.12.001.

[5] S.J. Qiu, M. Xu, The Investigation of the Traveling Wave Resonance of Driven Helical Gear, ASME International Gas Turbine and Aeroengine Congress and

Exposition, Cincinnati, America, 1993.

[6] G. Litak, M.I. Friswell, Dynamics of a gear system with faults in meshing stiffness, Nonlinear Dyn. 41 (2005) 415–421, https://doi.org/10.1007/s11071-005-

1398-y

[7] A. Parey, M.E. Badaoui, F. Guillet, N. Tandon, Dynamic modelling of spur gear pair and application of empirical mode decomposition-based statistical analysis

for early detection of localized tooth defect, J. Sound Vib. 294 (2006) 547–561, https://doi.org/10.1016/j.jsv.2005.11.021.

[8] H. Ma, J. Zeng, R.J. Feng, X. Pang, Q.B. Wang, B.C. Weng, Review on dynamics of cracked gear systems, Eng. Fail. Anal. 55 (2015) 224–245, https://doi.org/

10.1016/j.engfailanal.2015.06.004.

[9] Y. Pandya, A. Parey, Failure path based modified gear mesh stiffness for spur gear pair with tooth root crack, Eng. Fail. Anal. 27 (2013) 286–296, https://doi.

org/10.1016/j.engfailanal.2012.08.015.

[10] R. Guilbault, S. Lalonde, M. Thomas, Modeling and monitoring of tooth fillet crack growth in dynamic simulation of spur gear set, J. Sound Vib. 343 (2015)

144–165, https://doi.org/10.1016/j.jsv.2015.01.008.

[11] H. Ma, R.Z. Song, X. Pang, B.C. Wen, Time-varying mesh stiffness calculation of cracked spur gears, Eng. Fail. Anal. 44 (2014) 179–194, https://doi.org/

10.1016/j.engfailanal.2014.05.018.

[12] X.J. Zhou, Y.M. Shao, Y.G. Lei, M. Zuo, Time-varying meshing stiffness calculation and vibration analysis for a 16DOF dynamic model with linear crack growth

in a pinion, J. Vib. Acoust. 134 (1) (2012), https://doi.org/10.1115/1.4004683, 011011.1–011011.11.

[13] Z. Chen, Y. Shao, Dynamic simulation of planetary gear with tooth root crack in ring gear, Eng. Fail. Anal. 31 (2013) 8–18, https://doi.org/10.1016/j.

engfailanal.2013.01.012.

[14] H. Ma, X. Pang, J. Zeng, Q.B. Wang, B.C. Wen, Effects of gear crack propagation paths on vibration responses of the perforated gear system, Mech. Syst. Signal Pr

62-63 (10) (2015) 113–128, https://doi.org/10.1016/j.ymssp.2015.03.008.

[15] O.D. Mohammed, M. Rantatalo, J.O. Aidanpa¨a, ¨ U. Kumar, Vibration signal analysis for gear fault diagnosis with various crack progression scenarios, Mech. Syst.

Signal Pr. 41 (2013) 176–195, https://doi.org/10.1016/j.ymssp.2013.06.040.

[16] F.Q. Zhao, Z.G. Tian, Y. Zeng, Uncertainty quantification in gear remaining useful life prediction through an integrated prognostics method, IEEE Trans. Reliab.

62 (1) (2013) 146–159, https://doi.org/10.1109/TR.2013.2241216.

[17] J. Tian, S.G. Hutton, Traveling-wave modal identification based on forced or self-excited resonance for rotating discs, J. Vib. Control. 7 (1) (2001) 3–18, https://

doi.org/10.1177/107754630100700101.

[18] S.A. Tobias, R.N. Arnold, The influence of dynamic imperfections on the vibrations of rotating disks, Proc. Inst. Mech. Eng. 171 (1957) 669–690, https://doi.

org/10.1243/pime_proc_1957_171_056_02.

[19] C.J. Radcliffe, C.D. Mote, Identification and control of rotating disk vibration, J. Dyn. Syst. Meas. Control. Trans. ASME. 105 (1) (1983) 39–45, https://doi.org/

10.1115/1.3139726.

[20] R.V. Southwell, On the free transverse vibration of a uniform circular disk clamped at its centre; and on the effect of rotation, Proc. R. Soc. 101 (1921) 133–153,

https://doi.org/10.1098/rspa.1922.0032.

[21] Y. Honda, H. Matsuhisa, S. Sato, Modal response of a disk to a moving concentrated harmonic force, J. Sound Vib. 102 (4) (1985) 457–472, https://doi.org/

10.1016/S0022-460X(85)80107-3.

[22] Y.Q. Wang, X.H. Guo, Y.G. Li, J. Li, Nonlinear traveling wave vibration of a circular cylindrical shell subjected to a moving concentrated harmonic force,

J. Sound Vib. 329 (3) (2010) 338–352, https://doi.org/10.1016/j.jsv.2009.09.027.

[23] B. Uppaluri, B. Douglass, A validated finite element frequency response criterion for resonant-free gear design of the V-22 tiltrotor aircraft, in: 27th Joint

Propulsion Confer-ence, Sacramento, CA, American, 2013.

[24] C. Carmignani, P. Forte, G. Melani, G.D. Carlo, in: Numerical investigation on traveling wave vibration of bevel gears. 10th International Power Transmission

and Gearing Conference, Las Vegas, Nevada, American, 2007.

[25] X.C. Luan, Y.D. Sha, X.P. Guo, Y.N. Liao, F.T. Zhao, X. Liu, Transient dynamics analysis and experimental research of high-speed bevel gear in aero-engine,

J. Propul. Technol. 40 (12) (2019) 2806–2815, https://doi.org/10.13675/j.cnki.tjjs.180785.

[26] Y.C. Fung, E.E. Sechler, A. Kaplan, On the vibration of thin cylindrical shells under internal pressure, J. Aeronauti. Sci. 24 (1957) 650–660, https://doi.org/

10.1016/S0083-6729(08)60513-0.

[27] H.J. Macke, Traveling-wave vibration of gas-turbine engine shells, J. Eng. Gas Turbines Power. 88 (2) (1966) 179–187, https://doi.org/10.1115/1.3678502.

[28] P.B. Talbert, R.R. Gockel, Modulation of gear tooth loading due to traveling wave vibration, in: Proceedings of the ASME 2003 International Design Engineering

Technical Conferences and Computers and Information in Engineering Conference, Volume 4: 9th International Power Transmission and Gearing Conference,

Parts A and B, Chicago, USA, 2003, pp. 223–230, https://doi.org/10.1115/DETC2003/PTG-48029.

[29] G.A. Hu, L.H. He, G.J. Wu, C.Y. Wu, C. Liu, Acoustic noise and dynamic stress experi-mental study on travelling wave vibration of high-speed bevel gear in aeroengine, J. Propul. Technol. 40 (01) (2019) 166–174, https://doi.org/10.13675/j.cnki.tjjs.180025.

[30] X.C. Luan, Y.D. Sha, X.P. Guo, D.S. Yang, T. Ma, Influences of assembly parameters on rupture failure of accessory casing bevel gears, China Mech. Eng. 31 (04)

(2020) 438–444, https://doi.org/10.3969/j.issn.1004-132X.2020.04.010.

[31] C.H. Chen, S.H. Dong, Y. Guo, Z.Z. Wang, M. Guo, G.R. Fu, Investigation on spiral bevel gear fracture failure of an aero-engine, Gas Turbine Exp. Res. 31 (05)

(2018) 17–20. CNKI:SUN:RQWL.0.2018-05-004, +39.

[32] D.P. Jena, S. Sahoo, S.N. Panigrahi, Gear fault diagnosis using active noise cancellation and adaptive wavelet transform, Measurement 47 (2014) 356–372,

https://doi.org/10.1016/j.measurement.2013.09.006

引用本文

LUAN Xiaochi,,Liu Gongmin,SHA Yundong,He Hongbin,Guo Xiaopeng. Experiment study on traveling wave resonance of fatigue fracture of high-speed bevel gear in aero-engne based on acoustic measurement method [J]. Journal of Sound and Vibration. 2021; 511; (). 116345 - .

文献评论

相关学者

相关机构