Abstract
Bolted joints are prevalent in most assembled structures; however, predictive models for their behavior do not exist. Calibrated models, such as the Iwan model, are able to predict the response of a jointed structure over a range of excitations once calibrated at a nominal load. The Iwan model, though, is not widely adopted due to the high computational expense of implementation. To address this, an analytical solution of the Iwan model is derived under the hypothesis that for an arbitrary load reversal, there is a new distribution of dry friction elements, which are now stuck, that approximately resemble a scaled version of the original distribution of dry friction elements. The dry friction elements internal to the Iwan model do not have a uniform set of parameters and are described by a distribution of parameters, i.e., which internal dry friction elements are stuck or slipping at a given load, that ultimately governs the behavior of the joint as it transitions from microslip to macroslip. This hypothesis allows the model to require no information from previous loading cycles. Additionally, the model is extended to include the pinning behavior inherent in a bolted joint. Modifications of the resulting framework are discussed to highlight how the constitutive model for friction can be changed (in the case of an Iwan–Stribeck formulation) or how the distribution of dry friction elements can be changed (as is the case for the Iwan plasticity model). The reduced Iwan plus pinning model is then applied to the Brake–Reuß beam in order to discuss methods to deduce model parameters from experimental data.
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Notes
Thus, the three regimes defined above hold for a narrow range of u and \(\varphi \), including when \(u=\varphi \). Otherwise, microslip and macroslip must be defined in terms of u, and pinning must be defined in terms of \(\varphi \).
Technically, Hertz’s formulation is for two cylinders contacting each other, not one cylinder inside another cylinder. However, it is assumed that this case can be represented with Hertz’s model without loss of accuracy.
Though, the measurement of \(\phi _{\mathrm{MAX}}\) instead of \(F_S\) is often more practical as testing to macroslip is not always feasible.
This model is proposed purely as an example of how to apply the RIPP joint formulation to other constitutive models. The burden associated with parameter estimation is too high to consider this a practical model for analysts to use.
References
Armstrong-Hélouvry, B., Dupont, P., Canudas de Wit, C.: A survey of models, analysis tools and compensation methods for the control of machines with friction. Automatica 30, 1083–1138 (1994)
Bauschinger, J.: On the change of Position of the elastic limit of iron and steel under cyclic variations of stress. Mitt. Mech. Tech. Lab. Munchen 13, 1–115 (1886)
Bonney, M.S., et al.: Experimental determination of frictional interface models. In: 34t International Modal Analysis Conference (IMAC XXXIV). Orlando (2016)
Brake, M.R.: The role of epistemic uncertainty of contact models in the design and optimization of mechanical systems with aleatoric uncertainty. Nonlinear Dyn. 77, 899–922 (2014)
Brake, M.R., et al.: Variability and repeatability of jointed structures with frictional interfaces. In: 32nd International Modal Analysis Conference (IMAC XXXII). Orlando (2014)
Cigeroglu, E., An, N., Menq, C.-H.: A microslip friction model with normal load variation induced by normal motion. Nonlinear Dyn. 50, 609–626 (2007)
Deaner, B.: Modeling the nonlinear damping of jointed structures using modal models. Masters Dissertation. University of Wisconsin-Madison, Madison (2013)
Deaner, B.J., et al.: Investigation of modal Iwan models for structures with bolted joints. In: 31st International Modal Analysis Conference (IMAC XXXI). Garden Grove (2013)
Deaner, B.J., et al.: Application of viscous and Iwan modal damping models to experimental measurements from bolted structures. ASME J. Vib. Acoust. 137, 021012 (2015)
Deckstein, D., Traufetter, G.: Weight loss for superjumbos: the A380 and the aviation engineering dilemma. In: Der Spiegel (2012)
Di Maio, D., Schwingshackl, C., Sever, I.A.: Development of a test planning methodology for performing experimental model validation of bolted flanges. Nonlinear Dyn. 83, 983–1002 (2016)
Gaul, L., Nitsche, R.: Friction control for vibration suppression. Mech. Syst. Signal Process. 14, 139–150 (2000)
Gaul, L., Nitsche, R.: The role of friction in mechanical joints. ASME Appl. Mech. Rev. 54, 93–110 (2001)
Ishlinskii, A.Y.: Some applications of statistical methods to describing deformations of bodies. Izv. Akad. Nauk SSSR 9, 580–590 (1944)
Iwan, W.D.: A distributed-element model for hysteresis and its steady state dynamic response. ASME J. Appl. Mech. 33, 893–900 (1966)
Iwan, W.D.: On a class of models for the yielding behavior of continuous and composite systems. ASME J. Appl. Mech. 34, 612–617 (1967)
Jayakumar, P.: Modeling and identification in structural dynamics. Doctoral Dissertation. California Institute of Technology, Pasadena (1987)
Jenkins, G.M.: Analysis of the stress–strain relationships in reactor grade graphite. Br. J. Appl. Phys. 13, 30–32 (1962)
Johnson, K.L.: Contact Mechanics. Cambridge University Press, Cambridge (1985)
Kerschen, G., et al.: Past, present and future of nonlinear system identification in structural dynamics. Mech. Syst. Signal Process. 20, 505–592 (2006)
Kuether, R.J., Brake, M.R.W.: Instantaneous frequency and damping from transient ring-down data. In: 34t International Modal Analysis Conference (IMAC XXXIV). Orlando (2016)
Liang, J.W., Feeny, B.F.: Identifying Coulomb and viscous friction from free-vibration decrements. Nonlinear Dyn. 16, 337–347 (1998)
Masing, G: Self-stretching and hardening for brass. In: Proceedings of the 2nd International Congress for Applied Mechanics, pp. 332–335 (1926)
Meyer, J.J., Adams, D.E.: Theoretical and experimental evidence for using impact modulation to assess bolted joints. Nonlinear Dyn. 81, 103–117 (2015)
Petrov, E.P., Ewins, D.J.: Generic friction models for time-domain vibration analysis of bladed disks. ASME J. Turbomach. 126, 184–192 (2004)
Prandtl, L.: Ein Gedankenmodell zur kinetischen Theorie der festen Korper. Z. Angew. Math. Mech. 8, 85–106 (1928)
Roettgen, D.R., Allen, M.S.: Nonlinear characterization of a bolted, industrial structure using a modal framework. In: Mechanical Systems and Signal Processing (2016). doi:10.1016/j.ymssp.2015.11.010
Roettgen, D.R., et al.: Feasibility of describing joint nonlinearity in exhaust components with modal Iwan models. In: ASME International Design Engineering Technical Conferences IDETC/CIE. Buffalo (2014)
Segalman, D.J.: A four-parameter Iwan model for lap-type joints. ASME J. Appl. Mech. 72, 752–760 (2005)
Segalman, D.J., Starr, M.J.: Relationships among certain joint constitutive models. Technical Report SAND2004-4321. Sandia National Laboratories, Albuquerque (2004)
Segalman, D.J., et al.: Handbook on dynamics of jointed structures. Technical Report SAND2009-4164. Sandia National Laboratories, Albuquerque (2009)
Smallwood, D.O., Gregory, D.L., Coleman, R.G.: A three parameter constitutive model for a joint which exhibits a power law relationship between energy loss and relative displacement. In: 72nd Shock and Vibration Symposium. Destin (2001)
Sracic, M.W., Allen, M.S., Sumali, H.: Identifying the modal properties of nonlinear structures using measured free response time histories from a scanning laser Doppler vibrometer. In: 30th International Modal Analysis Conference (IMAC XXX). Jacksonville (2012)
Van de Vrande, B.L., Van Campen, D.H., de Kraker, A.: An approximate analysis of dry-friction-induced stick–slip vibrations by a smoothing procedure. Nonlinear Dyn. 19, 157–169 (1999)
Wang, X.Q., Mignolet, M.P.: Stochastic Iwan-type model of a bolted joint: formulation and identification. In: 32nd International Modal Analysis Conference (IMAC XXXII). Orlando (2014)
Acknowledgments
The author would like to thank Rob Kuether, Caroline Nielsen, and Scott Smith for their development of the STFT algorithms used in the examples.
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Sandia National Laboratories is a multi-mission laboratory managed and operated by Sandia Corporation, a wholly owned subsidiary of Lockheed Martin Corporations, for the US Department of Energy’s National Nuclear Security Administration under Contract DE-AC04-94AL85000.
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Brake, M.R.W. A reduced Iwan model that includes pinning for bolted joint mechanics. Nonlinear Dyn 87, 1335–1349 (2017). https://doi.org/10.1007/s11071-016-3117-2
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DOI: https://doi.org/10.1007/s11071-016-3117-2