Abstract
Supercritical transmission shafts, which have one or more critical speeds below their working speeds, are becoming more popular in new rotorcraft designs. To attenuate the excessive transcritical vibration, dry friction damper is a prevailing choice. In this paper, we focus on the basic working mechanism and parameter influence of the dry friction damper for supercritical transmission shaft. Mathematical model of the dry friction damper, which fully considers the nonlinear rub-impact and side-dry-friction effects, is proposed and integrated with finite element model of the transmission shaft to investigate nonlinear interactions between the shaft and damper. It is demonstrated through systematic numerical simulations that a typical transcritical response with dry friction damper can be divided into 4 sub-regions and the dry friction damper takes effect only within region II and III respectively through hard-stopping and side-dry-friction effects. In addition, effects of nonlinear bearing force, transcritical acceleration and initial location of the damper are discussed in detail. Moreover, influences of 3 key damper parameters, that is the rub-impact clearance, the critical slip force and the circumferential friction coefficient, are further investigated, which provides a guidance for designs of the dry friction damper. Finally, prototypes of the dry friction damper are designed, manufactured and tested on a rotor dynamics test rig. For the first time, the theoretical analysis and numerical simulation results are quantitatively verified by an experiment.
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The data that support the findings of this study are available from the corresponding author, Dan Wang, upon reasonable request.
References
Bozyigit, B., et al.: Free vibration and harmonic response of cracked frames using a single variable shear deformation theory. Struct. Eng. Mech. 74(1), 33–54 (2020a)
Bozyigit, B., et al.: Single variable shear deformation theory for free vibration and harmonic response of frames on flexible foundation. Eng. Struct. 208, 110268 (2020b)
Bozyigit, B., et al.: Transfer matrix formulations and single variable shear deformation theory for crack detection in beam-like structures. Struct. Eng. Mech. 73(2), 109–121 (2020c)
Brunken, J.E.: A new concept in supercritical drive systems for advanced rotorcraft. In: Annual Forum Proceedings-American Helicopter Society, vol. 56, no. 2 (2000)
Dżygadło, Z., Perkowski, W.: Research on dynamics of a supercritical propulsion shaft equipped with a dry friction damper. Aircr. Eng. Aerosp. Technol. 74(5), 447–454 (2002)
Friswell, M.I., et al.: Dynamics of Rotating Machines. Cambridge University Press (2010)
Garhart, J.: Development and qualification of composite tail rotor drive shaft for the UH-60M. In: Annual Forum Proceedings-American Helicopter Society, vol. 64, no. 3 (2008)
Hassan, M.A., et al.: Wavelet-based multiresolution bispectral analysis for detection and classification of helicopter drive-shaft problems. J. Dyn. Syst. Meas. Control 140(6), 061009 (2018)
Henry, T.C., Mills, B.T.: Optimized design for projectile impact survivability of a carbon fiber composite drive shaft. Compos. Struct. 207, 438–445 (2019)
Hetherington, P.L., Kraus, R.F., Darlow, M.S.: Demonstration of a supercritical composite helicopter power transmission shaft. J. Am. Helicopter Soc. 35(1), 23–28 (1990)
Huang, Z., Tan, J., Lu, X.: Phase difference and stability of a shaft mounted a dry friction damper: effects of viscous internal damping and gyroscopic moment. Adv. Mech. Eng. 13(3), 1687814021996919 (2021a)
Huang, Z., et al.: Dynamic characteristics of a segmented supercritical driveline with flexible couplings and dry friction dampers. Symmetry 13(2), 281 (2021b)
Huang, Z., et al.: All-round responses and boundaries of a shaft and dry friction damper assembly. Int. J. Non Linear Mech. 142, 103977 (2022)
Liu, J., et al.: Dynamic modeling and simulation of a flexible-rotor ball bearing system. J. Vib. Control (2021). https://doi.org/10.1177/10775463211034347
Omrani, E., et al.: Tribology and Applications of Self-Lubricating Materials. CRC Press (2017)
Ozaydin, O.: Vibration reduction of helicopter tail shaft by using dry friction dampers. MS thesis, Middle East Technical University (2017)
Ozaydin, O., Cigeroglu, E.: Effect of dry friction damping on the dynamic response of helicopter tail shaft. In: Rotating Machinery, Hybrid Test Methods, Vibro-Acoustics & Laser Vibrometry, vol. 8, pp 23–30 (2017)
Phung-Van, P., et al.: An isogeometric approach of static and free vibration analyses for porous FG nanoplates. Eur. J. Mech. A Solids 78, 103851 (2019)
Prabith, K., Krishna, I.R.: The numerical modeling of rotor–stator rubbing in rotating machinery: a comprehensive review. Nonlinear Dyn. 101(2), 1317–1363 (2020)
Spears, S.: Design and certification of the model 429 supercritical tail rotor driveshaft. In: Annual Forum Proceedings-American Helicopter Society, vol. 64, no. 3 (2008)
Technical manual Operator’s manual for helicopter, attack, AH-64D longbow apache. Headquarters, Department of the Army (2002)
Acknowledgements
The authors are grateful to the financial supports from National Natural Science Foundation of China (Grant No. 52005253), Natural Science Foundation of Jiangsu Province (Grant No. BK20200426) and National Key Laboratory of Science and Technology on Helicopter Transmission (Grant NO. HTL-A-21G07 & HTL-A-22K01).
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Appendices
Appendix
Nonlinear bearing force model
A ball bearing before and after deformation is schematically plotted in Fig.
18, where \(\Delta u\) and \(\Delta v\) respectively denote the relative displacements of the inner ring with respect to the outer ring along \(Y\) and \(Z\) directions. The contact deformation of the \(j\)th roller can be written as:
where \({\delta }_{b0}\) is the backlash of the ball bearing, \({\phi }_{j}\) represents the angular position of the \(j\)th roller relative to the positive \(Y\) direction, which can be written as:
where \({N}_{b}\) denotes the number of the rollers, \(\Omega \) depicts the rotational speed, and \({R}_{bi}\) and \({R}_{bo}\) respectively describe the radius of the inner and outer rings. According to the Hertzian contact theory, the reaction force between the roller and rings is
where \({k}_{b}\) depicts the contact stiffness, \(\Theta \) is defined as in the main body of the paper and retains a value of 1 only when \({\delta }_{j}\ge 0\), otherwise is equal to 0. The total reaction forces between the rollers and rings along \(Y\) and \(Z\) directions can be written as:
Rub-impact force model
There exists an initial clearance \({\delta }_{0}\) between the shaft and damper ring. Rub-impact only takes place when the relative displacement of the shaft related to the damper ring exceeds the clearance. As schematically illustrated in Fig.
19, the rub-impact position is defined by an angle \(\varphi \), and the following expressions hold:
where \({\mathbf{q}}_{d}={\left[{u}_{d},{v}_{d}\right]}^{T}\) and \({\mathbf{q}}_{s}={\left[{u}_{s},{v}_{s}\right]}^{T}\) are respectively the translational displacements of the damper ring and corresponding rub-impact node of the transmission shaft, and \(\delta \) depicts the relative displacement of the transmission shaft related to the damper ring and can be expressed as:
The rub-impact force between the shaft/damper includes two components, that is the radial impact component \({f}_{rr}\) and tangential rub component \({f}_{rt}\). The radial impact component is assumed to be elastic and linearly proportional to the interference between the shaft and damper ring, which can be expressed as:
where \({k}_{r}\) is the radial impact stiffness. The tangential rub component is assumed to be a Coulomb type and always retains a direction opposite to the relative velocity at the contact point and can be expressed as:
where \({\mu }_{r}\) is the tangential friction coefficient and \({v}_{rel}\) denotes the relative velocity at the contact point, which can be expressed as
where \({D}_{so}\) depicts the outer diameter of the shaft and \(\Omega \) represents the rotational speed of the shaft. The radial and tangential components of the rub-impact force can be further written in the \(Y\) and \(Z\) coordinates by taking the following transformation:
Further introduce the function \(\Theta \), which is defined as: \(\Theta =1\), if \(\delta \ge {\delta }_{0}\) and \(\Theta =0\), if \(\delta <{\delta }_{0}\), the rub-impact force can be expressed as
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Wang, D., Song, L., Cao, P. et al. Nonlinear modelling and parameter influence of supercritical transmission shaft with dry friction damper. Int J Mech Mater Des 19, 223–240 (2023). https://doi.org/10.1007/s10999-022-09625-6
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DOI: https://doi.org/10.1007/s10999-022-09625-6