Analysis of Tensioner Induced Coupling in Serpentine Belt Drive Systems

Size: px
Start display at page:

Download "Analysis of Tensioner Induced Coupling in Serpentine Belt Drive Systems"

Transcription

1 of Tensioner Induced Coupling in Serpentine Belt Drive Systems Copyright 2007 SAE International R. P. Neward and S. Boedo Department of Mechanical Engineering, Rochester Institute of Technology ABSTRACT A primary concern in the design of serpentine belt drive systems is resonant strand vibrations induced from engine excitation. Two analysis approaches to investigate the system vibrational response have been reported in the literature. The first, denoted as the "decoupled analysis" approach, employs longitudinal belt stiffness and takes into account only pulley rotation and tensioner displacement as system degrees of freedom. Transverse belt vibration (normal to belt travel) on all belt strands is decoupled from the analysis. The second, denoted as the "coupled analysis" approach, combines transverse tensioner strand belt motion with pulley rotation and tensioner displacement. Transverse belt vibration on strands between fixed pulleys remains decoupled from the system. This paper provides apparently the first cross comparison of these two analysis techniques on three distinct serpentine belt system configurations reported in the literature. Two of the belt drive systems in this study involve numerical models only, and a third published work involves experimental results was used to confirm the accuracy of both analysis techniques. It was observed that the coupled and decoupled analyses did not agree well for low order modes, and only the coupled formulation was able to predict experimentally determined mode shapes. Both analyses indicated that natural frequenices associated with rotational modes were insensitive to crankshaft speed. Natural frequencies associated with transverse belt span modes as computed with the coupled analysis were less sensitive to changes in crankshaft speeds. INTRODUCTION An engine front-end subsystem utilizing a single V- ribbed belt is known as a serpentine belt drive due to the long and elaborate path that the belt must follow. The advantages of using a serpentine belt drive setup over multiple V-belts include compactness, ease of belt replacement, length of belt life, and the need to employ only a single tensioner mechanism. The function of the belt tensioner is to maintain constant tractive tension throughout the entire belt drive system in the presence of belt wear, assembly variation, and deviation in belt length due to changes in accessory torques, belt speed, and belt temperature. The simplest type of tensioner is comprised of an idler pulley pinned to a rigid moment arm which pivots about a fixed point where a coil spring provides the tensioning load. A primary concern in the design of serpentine belt drive systems are resonant strand vibrations induced from engine excitation. Two analysis approaches to investigate the system vibrational response have been reported in the literature. The first, denoted as "decoupled analysis", employs longitudinal belt stiffness and takes into account only pulley rotation and tensioner displacement as system degrees of freedom. Transverse belt vibration (normal to belt travel) on all belt strands is decoupled from the analysis. The second, denoted as the "coupled analysis", combines transverse tensioner strand belt motion with pulley rotation and tensioner displacement. Transverse belt vibration on strands between fixed pulleys remains decoupled from the system. The basis for the work that has been done in the field of serpentine belt drives is research on the vibration characteristics of axially moving material. Mote [1] studied the vibrational characteristics of band saws and found that the band saw natural frequencies depend upon the relative motion of the band pulley axis. Modeling and analyzing serpentine belt drive systems with a dynamic tensioner was first accomplished by Ulsoy et al. [2] in which they used a mathematical model to examine the transverse vibration and stability of coupled belt-tensioner systems. Gasper and Hawker [3] and Hawker [4] developed a system of governing equations for a serpentine belt drive system and introduced a solution technique that resulted in the eigenvalues and eigenvectors of the complete system which was validated by experimentation. Hwang et al. [5] derived a nonlinear model that governs the longitudinal response of the belt spans in correlation with the rotational response of the crankshaft and accessory pulleys. Solution of the equilibrium equations leads to the tension-speed relationship for the serpentine belt drive system. The overall equations of motion are then linearized about the equilibrium state allowing the

2 rotational mode characteristics to be obtained from the associated eigenvalue problem. Kraver et al. [6] extended the modal vibration analysis to include a viscous belt span and coulomb tensioner arm damping. In order to validate the model, their results were compared against Hwang et al. [5] and found be in good agreement. Using dry friction damping within their model, as opposed to the more commonly used viscous damping, Leamy and Perkins [7] were able to capture the primary and secondary resonances within the belt drive system. All of the works mentioned previously assume that the linear response of belt drives is composed of the superposition of independent transverse and longitudinal modes. However, as shown by Beikmann et al. [8-11], there exists a linear coupling between the transverse and rotational modes in the spans adjacent to the automatic tensioner. This linear coupling is created by the rotational degree of freedom of the tensioner arm. In addition, there exists a nonlinear coupling mechanism between rotational and transverse modes arising from the finite stretching of the belt. This coupling can become greatly magnified under conditions leading to internal or autoparametric resonance. Beikmann also introduced a tensioner support constant η which is an indicator of the systems ability to maintain tractive tension (despite load and speed variations), and an indicator of the stability of the reference equilibrium state. Zhang and Zu [12, 13] employed the three pulley model developed by Beikmann to extend the understanding of serpentine belt drive behavior. Belt bending stiffness, which is assumed to be negligible in the previous works, was studied extensively by Wasfy and Leamy [14] and Kong and Parker [15, 16]. In these works, belt bending stiffness is introduced into the models which require additional techniques to solve for the vibration characteristics. serpentine belt drive sample application suitable for cross-comparison. Experimental results from a third serpentine belt drive system reported by Beikmann [8] will be used to confirm the accuracy of both analysis techniques. A parametric engine speed study will be presented to assess the impact of each analysis method on the predicted natural frequencies and associated mode shapes of each belt drive system. SYSTEM GEOMETRY Figure 1 shows the geometry of the serpentine belt drive system employed in both decoupled and coupled analysis approaches. The system is comprised of n pulleys with radii R j, j = 1, n, connected by a single serpentine belt represented by n belt strands between adjacent pulleys. The rotational axes of the n-1 pulleys are fixed, while the nth tensioner pulley is attached to a movable spring-loaded tensioner arm. Pulley 1 is attached to the engine crankshaft rotating at fixed angular velocity ω 1, and the belt is thus driven by the crankshaft at a fixed linear speed V. The absolute rotation of the jth pulley is defined as Θ j (t) = ω j t + θ j (t) (1) where pulley angular velocity ω j is given by with ω j = V / R j (2) V = R 1 ω 1 (3) θ t Parker [17] formulated an efficient method for calculating the eigensolutions and dynamic responses of coupled serpentine belt drive systems. The speed of solution is drastically reduced and the numerical problems that hinder other published methods are eliminated. However, by coupling the rotational and transverse motions in the spans adjacent to the tensioner, the system of equations becomes significantly more complex than modeling the motions as uncoupled. As a result, the solution techniques required to solve these models demand considerably more computational power. P n Y S n w i-1 P i-1 θ 1 V This paper provides apparently the first crosscomparison of decoupled and coupled analysis techniques on three different serpentine belt systems. The decoupled and coupled analysis approaches are taken from the representative studies of Hwang et al. [5] and Parker [17], respectively. These particular papers were chosen based on the fact that each captures the essential features of the assumptions inherent in each analysis approach, and each paper provides a distinct X P 1 w i θ i R i P 2 P 3 S 2 ω 1 S 1 Fig. 1 Belt drive system geometry Assuming crankshaft angular velocity ω 1 is constant, phase angle θ j (t) represents the angular motion of the jth pulley as viewed by an observer rotating at the respective (constant) angular velocity of the jth pulley.

3 In other words, θ j (t) represents the motion of the jth pulley as observed by a stroboscope tuned to the respective frequency ω j. Transverse belt displacement on the ith belt strand is represented by a function W i (x i,t), i = 1, n, where x i is the spatial coordinate as measured between the two connected pulleys. Assuming crankshaft angular velocity ω 1 is constant, W i (x i,t) represents the transverse motion of the ith belt stand moving with an axial velocity of V. Under conditions of fixed crankshaft angular velocity ω 1 and no external disturbances, the belt drive system assumes an equilibrium configuration θ e [θ 2 θ 3 θ n θ t ] T e, W i (x i,t) = 0, where phase angles take on constant values and strand transverse motions are zero. Small disturbances from equilibrium arise primarily from crankshaft and camshaft torsional excitations, and this paper examines the natural frequencies and associated mode shapes of the linearized belt drive system about a specified equilibrium configuration. DECOUPLED FORMULATION The theoretical formulation for the decoupled analysis of the serpentine belt drive system is taken directly from Hwang et al. [5] and is outlined here in condensed form for completeness. The assumptions used in developing the governing equations include: -- The belt does not slip on the pulleys. -- The belt is uniform, perfectly flexible, and stretches in a quasi-static manner. -- Transverse belt response on all strands are decoupled from longitudinal belt response. -- The crankshaft motion and any torque inputs from accessories are prescribed (either zero or determined from experiments). -- The tensioner executes small motions about some steady state position. Moreover the tensioner mechanism is designed to be dissipative and is the dominant source of dissipation. This dissipation is assumed to be linear viscous damping, and dissipation in the belt and fixed pulleys is assumed to be negligibly small. The linearized equations of motion for the decoupled system take on the form M D 2 z + C D z + K z = 0 (4) where the degrees of freedom z [ ε 2 ε n ε t ] T represent the set of small pulley phase motion and tensioner arm rotation about an equilibrium configuration, with (time) differential operator D d/dt. Mass, damping, and stiffness matrices M, C, and K depend primarily upon strand stiffness, component polar moment of inertia, tensioner rotational stiffness, and equilibrium strand tensions, all of which depend on crank angular velocity ω 1. The equilibrium system configuration θ e and system vibrational response given by equation (4) are both relative to a reference tension (constant on all strands) obtained by setting V = 0. Defining z = Z exp(iλt), the natural frequencies λ and mode shapes Z of the system can be found in the usual manner from the eigenvalue problem [ λ 2 M - iλ C + K ] Z = 0 (5) The m = 1, natural frequencies associated with all belt strand transverse vibration (including those attached to the tensioner) are assumed completely decoupled from equation (5) and are given by Abrate [18] as λ belt = (mπ/l j )[(P j - ηρv 2 ) /ρ) 1/2 x [1 - (1-η)V 2 /c 2 ](1 + ηv 2 /C 2 ) -1/2 (6) where, for the jth strand, L j is the belt strand length, ρ is belt strand density, and P j is the equilibrium strand tension at engine speed ω 1. Parameter η depends upon the relative stiffness of the pulley supports and axial belt stiffness, and c = (P j / ρ) 1/2. COUPLED FORMULATION The theoretical formulation for the coupled analysis of the serpentine belt drive system is taken directly from Parker [17] and is outlined here in condensed form for completeness. Key assumptions preserved in this coupled formulation include: --The belt properties and belt speed are uniform. --Belt bending stiffness is negligible. -- Damping is not modeled. -- Belt-pulley wedging and belt slip at the belt-pulley interfaces are not considered. Referring to Figure 1, the transverse belt strand displacements W i-1 (x,t), W i (x,t) attached to the tensioner pulley are now assumed coupled to pulley rotations and tensioner pulley translation. Transverse strand vibration is governed by the partial differential equation ρ ( 2 W j / t 2 ) 2ρV ( 2 W j / x t) (P j ρv 2 ) ( 2 W j / x 2 ) = 0 j = i-1, i (7) Boundary conditions on each strand require zero belt transverse displacement at points attached to the fixed pulleys and displacements which are constrained to move with the center motion of the tensioner pulley.

4 Belt strand transverse displacement for those strands attached to the tensioner is represented by a linear combination of r orthogonal mode shapes α r (ξ i-1 ) and γ r (ξ i ) of the form W i-1 (x i-1,t) = R 1 Σ a r (t) α r (ξ i-1 ) (8) W i (x i,t) = R 1 Σ b r (t) γ r (ξ i ) (9) where ξ i = x i /L i and mode shapes α r and γ r satisfy the belt strand boundary conditions. Employing this modal formulation for the belt strands, incorporating reference strand tension, and linearizing the system about an equilibrium engine speed, the coupled analysis as described by Parker [17] once again takes the form M D 2 z + C D z + K z = 0 (10) Table 1 Belt Drive System: Case Study 1 Pulley Type Center Pulley Location (x,y) Radius 1 Crankshaft 0, Air Cond , Power Strg. 252, Idler 90.3, Alternator 86, Water Pump 0, Tensioner 151.2, where z [ a 1 a r b 1 b r ε 2 ε n ε t ] T now includes r modal contribution factors for each of the belt strands attached to the tensioner. The natural frequencies and mode shapes of this system will now involve coupling of pulley phase angles and modal contribution factors. The natural frequencies of transverse vibration for belt strands which are attached to fixed pulleys remain decoupled from the system and are given by equation (6) above. Tensioner Arm Pivot Location (x,y) Tensioner Arm Effective Length L t Tensioner Arm Installation Angle θ 0 (deg) 142, CASE STUDY 1 Table 1 provides data for a sample serpentine belt drive system denoted as Case Study 1, taken from Hwang et al. [5] based on the setup of an actual engine. The geometric configuration of the belt drive system representing Case Study 1 is shown in Figure 2. P6 P1 S5 Y P5 S4 P4 X S6 θ 0 S7 P7 S1 S3 P3 P2 Fig. 2 Belt drive system: Case Study 1 S2 Table 2 provides a set of mode shapes starting at the lowest natural frequency obtained from both decoupled and coupled analyses at an crankshaft speed of rev/min. (Modes and natural frequencies for transverse modes on belt strands between fixed pulleys are not included here.) In either analysis, each resulting mode shape for the system is dominated by a single rotational or transverse vibration on a single pulley or tensioner strand. Thus, the identification "P5 - Rotational -1" indicates that this mode shape is essentially dominated by rotational motion of pulley 5, and that it is the first mode shape encountered with this property as computed in the decoupled analysis. For this case, relative amplitudes on the remaining pulleys are small compared to pulley 5. (The second mode shape dominated by rotational motion of pulley 5 would be identified as "P5 - Rotational -2" and so on.) As a check, the relative amplitudes of pulley rotations corresponding to each mode shape obtained from the decoupled analysis were found to match well with those provided in the decoupled analysis by Hwang et al. [5]. Table 3 compares the corresponding natural frequencies obtained for each mode shape as computed from the decoupled and coupled analyses at a crankshaft speed of rev/min. Results from the decoupled analysis compare well with those obtained by Hwang et al. [5]. The mode shapes obtained from the coupled analysis are similar to those obtained from the decoupled analysis, as indicated by modal assurance values near 1 [19]. The corresponding natural frequencies found in the coupled analysis, however, are generally greater,

5 especially for mode shape 3 characterized by coupled rotation of the tensioner arm (TA) and tensioner pulley 7. Figure 3 shows that the natural frequencies associated with mode shapes 4, 5, 8, and 9 representing transverse motion of tensioner strands decrease with engine speed for both decoupled and coupled analyses. The reduction in natural frequency is less pronounced in the coupled analysis, indicating that the transverse belt motion acts as a stiffening mechanism on those respective modes. Table 2 Mode Shapes: Case 1 (P = pulley, TA = tensioner arm, S = belt span) Mode Shape 1 P5 Rotational 1 2 P2 Rotational 1 3 TA Rotational 1 4 S7 Transverse 1 5 TA/P7 Rotational 1 6 S6 Transverse 1 7 P3 Rotational 1 8 S7 Transverse 2 9 S6 Transverse 2 10 P7 Rotational 2 11 P4 Rotational 1 (a) decoupled analysis Table 3 Natural Frequencies: Case 1 (MA = modal assurance criterion) Mode Decoupled (Hz) Coupled (Hz) MA Hwang et al. [5] (b) coupled analysis Fig. 3 Natural frequencies associated with transverse modes on belt spans attached to the tensioner: Case Study 1 The natural frequencies for the remaining rotational mode shapes are essentially unaffected by crankshaft speed for both decoupled and coupled analyses. The decoupled results are again in agreement with trends obtained by Hwang et al. [5]. Figure 4 shows the effect of engine speed on the natural frequencies associated with mode shapes on the belt spans between fixed pulleys as computed from equation (6). Note that these natural frequencies fall in the range of those found in the system analyses.

6 P5 S4 S5 S6 P7 θ 0 P4 S3 P3 S7 S2 P6 Y P1 X P2 S1 Fig. 4 Natural frequencies associated with transverse modes on belt spans between fixed spans: Case Study 1 CASE STUDY 2 Table 4 provides data for a sample serpentine belt drive system denoted as Case Study 2, taken from Parker [17] based on an automotive system that was experiencing a noise and vibration problem. The geometric configuration of the belt drive system representing Case Study 2 is shown in Figure 5. Table 4 Belt Drive System: Case Study 2 Pulley Type Center Location (x,y) Pulley Radius 1 Crankshaft 0, Air Cond , Alternator 231.7, Idler 79.6, Power Strg , Water Pump -200, Tensioner -45.1, Tensioner Arm Pivot Location (x,y) Tensioner Arm Effective Length L t Tensioner Arm Installation Angle θ 0 (deg) 33, Fig. 5 Belt drive system: Case Study 2 Table 5 provides a set of mode shapes starting at the lowest natural frequency obtained from both decoupled and coupled analyses at an crankshaft speed of 680 rev/min. (Modes and natural frequencies for transverse modes on belt strands between fixed pulleys are not included here.) In this case, modes 2 and 11 exhibit dominant rotational motions on both pulleys 6 and 7, identified as "P6/P7". Table 5 Mode Shapes: Case 2 (P = pulley, TA = tensioner arm, S = belt span) Mode Shape 1 P3 Rotational 1 2 P6/P7 Rotational 1 3 P2 Rotational 1 4 P5 Rotational 1 5 S6 Transverse 1 6 S7 Transverse 1 7 P4 Rotational 1 8 S6 Transverse 2 9 S7 Transverse 2 10 P4 Rotational 2 11 P6/P7 Rotational 2 Table 6 compares the corresponding natural frequencies obtained for each mode shape as computed from the decoupled and coupled analyses at a crankshaft speed of 680 rev/min. Results from the coupled analysis compare well with those obtained by Parker [17]. However, low modal assurance values indicate that mode shapes 2, 3, and 4 obtained from the decoupled analysis are substantially different from those obtained

7 from the coupled analysis. The influence of tensioner strand coupling on the resulting system response is thus quite strong for this case study, as its inclusion substantially alters three of the predicted mode shapes. For the remaining set of mode shapes, the corresponding natural frequencies found in the coupled analysis are once again generally greater than those predicted using the decoupled analysis. Y P3 S2 X θ 0 S3 P2 S1 P1 Table 6 Natural Frequencies: Case 2 (MA = modal assurance criterion) Mode Decoupled Coupled MA Parker [17] (Hz) (Hz) The natural frequencies associated with mode shapes 5, 6, 8, and 9 representing transverse motion of tensioner strands exhibit the same trend with engine speed for both decoupled and coupled analyses as that found in Case Study 1. Moreover, the natural frequencies for the remaining rotational mode shapes are once again essentially unaffected by engine speed for both decoupled and coupled analyses. The coupled results are again in quantitative agreement with trends obtained by Parker [17]. The effect of engine speed on the natural frequencies associated with mode shapes on the belt spans between fixed pulleys follow the same trends as in Case Study 1, and these natural frequencies also fall in the range of those found in the system analyses. CASE STUDY 3 Table 7 provides data for a sample serpentine belt drive system denoted as Case Study 3, taken from Beikmann [8] based on an experimental test stand. The geometric configuration of the belt drive system representing Case Study 3 is shown in Figure 6. Although the system presented here is much smaller than those presented in the previous two case studies, it contains all the necessary components critical to a serpentine belt drive system including a driving pulley, automatic tensioner, and a driven pulley. Fig. 6 Belt drive system: Case Study 3 Table 7 Belt Drive System: Case Study 3 Pulley Type Center Location (x,y) Pulley Radius 1 Crankshaft 552.5, Tensioner 347.7, Idler 0, Tensioner Arm Pivot Location (x,y) Tensioner Arm Effective Length L t Tensioner Arm Installation Angle θ 0 (deg) 250.8, Table 8 provides a set of mode shapes starting at the lowest natural frequency obtained from both decoupled and coupled analyses at zero crankshaft speed. Table 9 compares the corresponding natural frequencies obtained for each mode shape as computed from the decoupled and coupled analyses at zero crankshaft speed. It is observed that decoupled formulation fails to capture the experimentally observed tensioner arm rotational mode shape. The coupled analysis predicts both the transverse span 2 and the tensioner arm rotational mode shapes, and the corresponding natural frequencies agree well with experiment. The higher order modes and corresponding natural frequencies are captured equally well by the decoupled and coupled formulations. Table 10 shows that the natural frequency predicted by equation (6) for transverse vibration of the span between fixed pulleys agrees very well with experiment.

8 Table 8 Mode Shapes: Case 3 (P = pulley, TA = tensioner arm, S = belt span) Mode Shape 1 S2 Transverse 1 2 P3 Rotational 1 3 S2 Transverse 2 4 S1 Transverse 1 5 P3 Rotational 2 6 S1 Transverse 2 7 P2 Rotational 1 8 TA Rotational 1 Table 9 Natural Frequencies: Case 3 (MA = modal assurance criterion) Mode Decoupled Coupled MA Beikmann [8] (Hz) (Hz) Table 10 Natural Frequency Comparison on Fixed-Fixed Tensioner Strand: Case 3 Equation (6) 31.9 Hz Experimental 33 Hz (Biekmann [8]) CONCLUSIONS Despite the comparative simplicity of the decoupled analysis, the results obtained from the three case studies clearly indicate that rotational pulley motion is indeed coupled to the transverse motions of the spans adjacent to the tensioner. The lowest ordered natural frequencies and associated mode shapes are clearly influenced by this coupling, while the decoupled analysis is adequate for higher ordered modes. The coupled analysis is shown to produce the more accurate results based on the comparison to the experimental data. A parametric study showed that natural frequencies associated with pulley rotations were insensitive to changes in crankshaft speed, regardless of whether the decoupled or coupled analysis methods was used. For the belt spans adjacent to the tensioner, the natural frequencies decreased with increasing engine speed, but this decrease was mitigated in the coupled analysis. Experimental data which allows for a more complete validation of analysis methods is clearly lacking, as least in published form. It is hoped this paper will provide some guidance for future papers related to testing. REFERENCES 1. Mote, C.D. A Study of Band Saw Vibrations. Journal of The Franklin Institute 279 (1965): Ulsoy, A.G., Whitesell, J.E., Hooven, M.D. Design of Belt-Tensioner Systems for Dynamic Stability. ASME Journal of Vibration, Acoustics, Stress, and Reliability in Design (1985): Gasper, R.G.S., Hawker, L.E. Resonance Frequency Prediction of Automotive Serpentine Belt Drive Systems by Computer Modeling. Machinery Dynamics - Applications and Vibration Control Problems, September ASME, Hawker, L.E. "A Vibration of Automotive Serpentine Accessory Drive Systems." Diss., University of Windsor, Windsor, ON, Canada, Hwang, S.J., Perkins, N.C., Ulsoy, A.G., Meckstroth, R.J. Rotational Response and Slip Prediction of Serpentine Belt Drive Systems. ASME Journal of Vibration and Acoustics 116 (1994): Kraver, T.C., Fan, G.W., Shah, J.J. Complex Modal of a Flat Belt Pulley System With Belt Damping and Coulomb-Damped Tensioner. ASME Journal of Mechanical Design 118 (1996): Leamy, M.J., Perkins, N.C. Nonlinear Periodic Response of Engine Accessory Drives With Dry Friction Tensioners. ASME Journal of Vibration and Acoustics 120 (1998): Beikmann, R.S. "Static and Dynamic Behavior of Serpentine Belt Drive Systems: Theory and Experiment." Diss., University of Michigan, Ann Arbor, MI, 1992.

9 9. Beikmann, R.S., Perkins, N.C., Ulsoy, A.G. Free Vibration of Serpentine Belt Drive Systems. ASME Journal of Vibration and Acoustics 118 (1996): Beikmann, R.S., Perkins, N.C., Ulsoy, A.G. Nonlinear Coupled Vibration Response of Serpentine Belt Drive Systems. ASME Journal of Vibration and Acoustics 118 (1996): Beikmann, R.S., Perkins, N.C., Ulsoy, A.G. Design and of Automotive Serpentine Belt Drive Systems for Steady State Performance. ASME Journal of Mechanical Design 119 (1997): Zhang, L., Zu, J.W. Modal of Serpentine Belt Drive Systems. Journal of Sound and Vibration 222 (1999): Zhang, L., Zu, J.W. One-To-One Auto-Parametric Resonance in Serpentine Belt Drive Systems. Journal of Sound and Vibration 232 (2000): Wasfy, T.M., Leamy, M. Effect of Bending Stiffness on the Dynamic and Steady-State Responses of Belt Drives. ASME Design Engineering Technical Conferences and Computer and Information in Engineering Conference ASME, Kong, L., Parker, R.G. Coupled Belt-Pulley Vibration in Serpentine Drives with Belt Bending Stiffness. ASME Journal of Applied Mechanics 71 (2004): Kong, L., Parker, R.G. Equilibrium and Belt-Pulley Vibration Coupling in Serpentine Belt Drives. ASME Journal of Applied Mechanics 70 (2003): Parker, R.G. Efficient Eigensolution, Dynamic Response, and Eigensensitivity of Serpentine Belt Drives. Journal of Sound and Vibration 270 (2004): Abrate, S. Vibrations of Belts and Belt Drives. Mechanism and Machine Theory 27 (1992): Ewins, D.J. Modal Testing: Theory and Practice. England: Research Studies Press Ltd., 1986.

Validation of a Flexible Multibody Belt-Drive Model

Validation of a Flexible Multibody Belt-Drive Model Paper received: 23.12.2010 DOI:10.5545/sv-jme.2010.257 Paper accepted: 12.05.2011 Validation of a Flexible Multibody Belt-Drive Model Čepon, G. Manin, L. Boltežar, M. Gregor Čepon 1 Lionel Manin 2 Miha

More information

NONLINEAR DYNAMICS OF ONE-WAY CLUTCHES AND DRY FRICTION TENSIONERS IN BELT-PULLEY SYSTEMS DISSERTATION

NONLINEAR DYNAMICS OF ONE-WAY CLUTCHES AND DRY FRICTION TENSIONERS IN BELT-PULLEY SYSTEMS DISSERTATION NONLINEAR DYNAMICS OF ONE-WAY CLUTCHES AND DRY FRICTION TENSIONERS IN BELT-PULLEY SYSTEMS DISSERTATION Presented in Partial Fulfillment of the Requirements of the Degree Doctor of Philosophy in the Graduate

More information

Non-Contact Measurement of Dynamic Belt Span Tension in Automotive FEAD Systems

Non-Contact Measurement of Dynamic Belt Span Tension in Automotive FEAD Systems Non-Contact Measurement of Dynamic Belt Span Tension in Automotive FEAD Systems by Thelma Jayne Neudorf A thesis submitted in conformity with the requirements for the degree of Master of Applied Science

More information

Dynamics of Machinery

Dynamics of Machinery Dynamics of Machinery Two Mark Questions & Answers Varun B Page 1 Force Analysis 1. Define inertia force. Inertia force is an imaginary force, which when acts upon a rigid body, brings it to an equilibrium

More information

Advanced Vibrations. Elements of Analytical Dynamics. By: H. Ahmadian Lecture One

Advanced Vibrations. Elements of Analytical Dynamics. By: H. Ahmadian Lecture One Advanced Vibrations Lecture One Elements of Analytical Dynamics By: H. Ahmadian ahmadian@iust.ac.ir Elements of Analytical Dynamics Newton's laws were formulated for a single particle Can be extended to

More information

ANALYTICAL MODELING OF PLANETARY GEAR AND SENSITIVITY OF NATURAL FREQUENCIES

ANALYTICAL MODELING OF PLANETARY GEAR AND SENSITIVITY OF NATURAL FREQUENCIES ANALYTICAL MODELING OF PLANETARY GEAR AND SENSITIVITY OF NATURAL FREQUENCIES MAJID MEHRABI 1, DR. V.P.SINGH 2 1 Research Scholar, Department of Mechanical Engg. Department-PEC University of Technology

More information

Mechatronics. MANE 4490 Fall 2002 Assignment # 1

Mechatronics. MANE 4490 Fall 2002 Assignment # 1 Mechatronics MANE 4490 Fall 2002 Assignment # 1 1. For each of the physical models shown in Figure 1, derive the mathematical model (equation of motion). All displacements are measured from the static

More information

Introduction to Continuous Systems. Continuous Systems. Strings, Torsional Rods and Beams.

Introduction to Continuous Systems. Continuous Systems. Strings, Torsional Rods and Beams. Outline of Continuous Systems. Introduction to Continuous Systems. Continuous Systems. Strings, Torsional Rods and Beams. Vibrations of Flexible Strings. Torsional Vibration of Rods. Bernoulli-Euler Beams.

More information

Solvability condition in multi-scale analysis of gyroscopic continua

Solvability condition in multi-scale analysis of gyroscopic continua Journal of Sound and Vibration 309 (2008) 338 342 Short Communication Solvability condition in multi-scale analysis of gyroscopic continua Li-Qun Chen a,b,, Jean W. Zu c JOURNAL OF SOUN AN VIBRATION a

More information

Vibration Dynamics and Control

Vibration Dynamics and Control Giancarlo Genta Vibration Dynamics and Control Spri ringer Contents Series Preface Preface Symbols vii ix xxi Introduction 1 I Dynamics of Linear, Time Invariant, Systems 23 1 Conservative Discrete Vibrating

More information

Modelling of lateral-torsional vibrations of the crank system with a damper of vibrations

Modelling of lateral-torsional vibrations of the crank system with a damper of vibrations Modelling of lateral-torsional vibrations of the crank system with a damper of vibrations Bogumil Chiliński 1, Maciej Zawisza 2 Warsaw University of Technology, Institute of Machine Design Fundamentals,

More information

DETC98/PTG-5788 VIBRO-ACOUSTIC STUDIES OF TRANSMISSION CASING STRUCTURES

DETC98/PTG-5788 VIBRO-ACOUSTIC STUDIES OF TRANSMISSION CASING STRUCTURES Proceedings of DETC98: 1998 ASME Design Engineering Technical Conference September 13-16, 1998, Atlanta, GA DETC98/PTG-5788 VIBRO-ACOUSTIC STUDIES O TRANSMISSION CASING STRUCTURES D. Crimaldi Graduate

More information

Chapter 23: Principles of Passive Vibration Control: Design of absorber

Chapter 23: Principles of Passive Vibration Control: Design of absorber Chapter 23: Principles of Passive Vibration Control: Design of absorber INTRODUCTION The term 'vibration absorber' is used for passive devices attached to the vibrating structure. Such devices are made

More information

An Analysis Technique for Vibration Reduction of Motor Pump

An Analysis Technique for Vibration Reduction of Motor Pump An Analysis Technique for Vibration Reduction of Motor Pump Young Kuen Cho, Seong Guk Kim, Dae Won Lee, Paul Han and Han Sung Kim Abstract The purpose of this study was to examine the efficiency of the

More information

2108. Free vibration properties of rotate vector reducer

2108. Free vibration properties of rotate vector reducer 2108. Free vibration properties of rotate vector reducer Chuan Chen 1, Yuhu Yang 2 School of Mechanical Engineering, Tianjin University, Tianjin, 300072, P. R. China 1 Corresponding author E-mail: 1 chenchuan1985728@126.com,

More information

AA 242B / ME 242B: Mechanical Vibrations (Spring 2016)

AA 242B / ME 242B: Mechanical Vibrations (Spring 2016) AA 242B / ME 242B: Mechanical Vibrations (Spring 206) Solution of Homework #3 Control Tab Figure : Schematic for the control tab. Inadequacy of a static-test A static-test for measuring θ would ideally

More information

Table of Contents. Preface... 13

Table of Contents. Preface... 13 Table of Contents Preface... 13 Chapter 1. Vibrations of Continuous Elastic Solid Media... 17 1.1. Objective of the chapter... 17 1.2. Equations of motion and boundary conditions of continuous media...

More information

Final Exam Solution Dynamics :45 12:15. Problem 1 Bateau

Final Exam Solution Dynamics :45 12:15. Problem 1 Bateau Final Exam Solution Dynamics 2 191157140 31-01-2013 8:45 12:15 Problem 1 Bateau Bateau is a trapeze act by Cirque du Soleil in which artists perform aerial maneuvers on a boat shaped structure. The boat

More information

VIBRATION ENERGY FLOW IN WELDED CONNECTION OF PLATES. 1. Introduction

VIBRATION ENERGY FLOW IN WELDED CONNECTION OF PLATES. 1. Introduction ARCHIVES OF ACOUSTICS 31, 4 (Supplement), 53 58 (2006) VIBRATION ENERGY FLOW IN WELDED CONNECTION OF PLATES J. CIEŚLIK, W. BOCHNIAK AGH University of Science and Technology Department of Robotics and Mechatronics

More information

PROJECT 1 DYNAMICS OF MACHINES 41514

PROJECT 1 DYNAMICS OF MACHINES 41514 PROJECT DYNAMICS OF MACHINES 454 Theoretical and Experimental Modal Analysis and Validation of Mathematical Models in Multibody Dynamics Ilmar Ferreira Santos, Professor Dr.-Ing., Dr.Techn., Livre-Docente

More information

Figure 5.28 (a) Spring-restrained cylinder, (b) Kinematic variables, (c) Free-body diagram

Figure 5.28 (a) Spring-restrained cylinder, (b) Kinematic variables, (c) Free-body diagram Lecture 30. MORE GENERAL-MOTION/ROLLING- WITHOUT-SLIPPING EXAMPLES A Cylinder, Restrained by a Spring and Rolling on a Plane Figure 5.28 (a) Spring-restrained cylinder, (b) Kinematic variables, (c) Free-body

More information

WEEKS 8-9 Dynamics of Machinery

WEEKS 8-9 Dynamics of Machinery WEEKS 8-9 Dynamics of Machinery References Theory of Machines and Mechanisms, J.J.Uicker, G.R.Pennock ve J.E. Shigley, 2011 Mechanical Vibrations, Singiresu S. Rao, 2010 Mechanical Vibrations: Theory and

More information

Structural Dynamics Lecture 7. Outline of Lecture 7. Multi-Degree-of-Freedom Systems (cont.) System Reduction. Vibration due to Movable Supports.

Structural Dynamics Lecture 7. Outline of Lecture 7. Multi-Degree-of-Freedom Systems (cont.) System Reduction. Vibration due to Movable Supports. Outline of Multi-Degree-of-Freedom Systems (cont.) System Reduction. Truncated Modal Expansion with Quasi-Static Correction. Guyan Reduction. Vibration due to Movable Supports. Earthquake Excitations.

More information

C7047. PART A Answer all questions, each carries 5 marks.

C7047. PART A Answer all questions, each carries 5 marks. 7047 Reg No.: Total Pages: 3 Name: Max. Marks: 100 PJ DUL KLM TEHNOLOGIL UNIVERSITY FIRST SEMESTER.TEH DEGREE EXMINTION, DEEMER 2017 ourse ode: E100 ourse Name: ENGINEERING MEHNIS PRT nswer all questions,

More information

UNIT-I (FORCE ANALYSIS)

UNIT-I (FORCE ANALYSIS) DHANALAKSHMI SRINIVASAN INSTITUTE OF RESEACH AND TECHNOLOGY DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK ME2302 DYNAMICS OF MACHINERY III YEAR/ V SEMESTER UNIT-I (FORCE ANALYSIS) PART-A (2 marks)

More information

Advanced Vibrations. Distributed-Parameter Systems: Exact Solutions (Lecture 10) By: H. Ahmadian

Advanced Vibrations. Distributed-Parameter Systems: Exact Solutions (Lecture 10) By: H. Ahmadian Advanced Vibrations Distributed-Parameter Systems: Exact Solutions (Lecture 10) By: H. Ahmadian ahmadian@iust.ac.ir Distributed-Parameter Systems: Exact Solutions Relation between Discrete and Distributed

More information

1859. Forced transverse vibration analysis of a Rayleigh double-beam system with a Pasternak middle layer subjected to compressive axial load

1859. Forced transverse vibration analysis of a Rayleigh double-beam system with a Pasternak middle layer subjected to compressive axial load 1859. Forced transverse vibration analysis of a Rayleigh double-beam system with a Pasternak middle layer subjected to compressive axial load Nader Mohammadi 1, Mehrdad Nasirshoaibi 2 Department of Mechanical

More information

DYNAMICS OF MACHINERY 41514

DYNAMICS OF MACHINERY 41514 DYNAMICS OF MACHINERY 454 PROJECT : Theoretical and Experimental Modal Analysis and Validation of Mathematical Models in Multibody Dynamics Holistic Overview of the Project Steps & Their Conceptual Links

More information

Lecture 19. Measurement of Solid-Mechanical Quantities (Chapter 8) Measuring Strain Measuring Displacement Measuring Linear Velocity

Lecture 19. Measurement of Solid-Mechanical Quantities (Chapter 8) Measuring Strain Measuring Displacement Measuring Linear Velocity MECH 373 Instrumentation and Measurements Lecture 19 Measurement of Solid-Mechanical Quantities (Chapter 8) Measuring Strain Measuring Displacement Measuring Linear Velocity Measuring Accepleration and

More information

An improved brake squeal source model in the presence of kinematic and friction nonlinearities

An improved brake squeal source model in the presence of kinematic and friction nonlinearities An improved brake squeal source model in the presence of kinematic and friction nonlinearities Osman Taha Sen, Jason T. Dreyer, and Rajendra Singh 3 Department of Mechanical Engineering, Istanbul Technical

More information

Modal Analysis: What it is and is not Gerrit Visser

Modal Analysis: What it is and is not Gerrit Visser Modal Analysis: What it is and is not Gerrit Visser What is a Modal Analysis? What answers do we get out of it? How is it useful? What does it not tell us? In this article, we ll discuss where a modal

More information

Structural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian

Structural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian Structural Dynamics Lecture Eleven: Dynamic Response of MDOF Systems: (Chapter 11) By: H. Ahmadian ahmadian@iust.ac.ir Dynamic Response of MDOF Systems: Mode-Superposition Method Mode-Superposition Method:

More information

Chapter a. Spring constant, k : The change in the force per unit length change of the spring. b. Coefficient of subgrade reaction, k:

Chapter a. Spring constant, k : The change in the force per unit length change of the spring. b. Coefficient of subgrade reaction, k: Principles of Soil Dynamics 3rd Edition Das SOLUTIONS MANUAL Full clear download (no formatting errors) at: https://testbankreal.com/download/principles-soil-dynamics-3rd-editiondas-solutions-manual/ Chapter

More information

A Guide to linear dynamic analysis with Damping

A Guide to linear dynamic analysis with Damping A Guide to linear dynamic analysis with Damping This guide starts from the applications of linear dynamic response and its role in FEA simulation. Fundamental concepts and principles will be introduced

More information

Dynamic analysis of the Empact CVT Ratio and slip dependent, non-minimum phase dynamics

Dynamic analysis of the Empact CVT Ratio and slip dependent, non-minimum phase dynamics Dynamic analysis of the Empact CVT Ratio and slip dependent, non-minimum phase dynamics T.W.G.L. Klaassen, B.G. Vroemen and M. Steinbuch Eindhoven University of Technology, Department of Mechanical Engineering

More information

Structural Dynamics Lecture 2. Outline of Lecture 2. Single-Degree-of-Freedom Systems (cont.)

Structural Dynamics Lecture 2. Outline of Lecture 2. Single-Degree-of-Freedom Systems (cont.) Outline of Single-Degree-of-Freedom Systems (cont.) Linear Viscous Damped Eigenvibrations. Logarithmic decrement. Response to Harmonic and Periodic Loads. 1 Single-Degreee-of-Freedom Systems (cont.). Linear

More information

Theory of Vibrations in Stewart Platforms

Theory of Vibrations in Stewart Platforms Theory of Vibrations in Stewart Platforms J.M. Selig and X. Ding School of Computing, Info. Sys. & Maths. South Bank University London SE1 0AA, U.K. (seligjm@sbu.ac.uk) Abstract This article develops a

More information

Final Exam April 30, 2013

Final Exam April 30, 2013 Final Exam Instructions: You have 120 minutes to complete this exam. This is a closed-book, closed-notes exam. You are allowed to use a calculator during the exam. Usage of mobile phones and other electronic

More information

Development of a test apparatus that consistently generates squeak to rate squeak propensity of a pair of materials

Development of a test apparatus that consistently generates squeak to rate squeak propensity of a pair of materials Development of a test apparatus that consistently generates squeak to rate squeak propensity of a pair of materials Gil Jun LEE 1 ; Jay KIM 2 1, 2 Department of Mechanical and Materials Engineering, University

More information

WORK SHEET FOR MEP311

WORK SHEET FOR MEP311 EXPERIMENT II-1A STUDY OF PRESSURE DISTRIBUTIONS IN LUBRICATING OIL FILMS USING MICHELL TILTING PAD APPARATUS OBJECTIVE To study generation of pressure profile along and across the thick fluid film (converging,

More information

Simple Modeling and Modal Analysis of Reciprocating Compressor Crankshaft System

Simple Modeling and Modal Analysis of Reciprocating Compressor Crankshaft System Purdue University Purdue e-pubs International Compressor Engineering Conference School of Mechanical Engineering 2010 Simple Modeling and Modal Analysis of Reciprocating Compressor Crankshaft System Binyan

More information

6. Find the net torque on the wheel in Figure about the axle through O if a = 10.0 cm and b = 25.0 cm.

6. Find the net torque on the wheel in Figure about the axle through O if a = 10.0 cm and b = 25.0 cm. 1. During a certain period of time, the angular position of a swinging door is described by θ = 5.00 + 10.0t + 2.00t 2, where θ is in radians and t is in seconds. Determine the angular position, angular

More information

C. points X and Y only. D. points O, X and Y only. (Total 1 mark)

C. points X and Y only. D. points O, X and Y only. (Total 1 mark) Grade 11 Physics -- Homework 16 -- Answers on a separate sheet of paper, please 1. A cart, connected to two identical springs, is oscillating with simple harmonic motion between two points X and Y that

More information

Dr.Vinod Hosur, Professor, Civil Engg.Dept., Gogte Institute of Technology, Belgaum

Dr.Vinod Hosur, Professor, Civil Engg.Dept., Gogte Institute of Technology, Belgaum STRUCTURAL DYNAMICS Dr.Vinod Hosur, Professor, Civil Engg.Dept., Gogte Institute of Technology, Belgaum Overview of Structural Dynamics Structure Members, joints, strength, stiffness, ductility Structure

More information

Simulating Two-Dimensional Stick-Slip Motion of a Rigid Body using a New Friction Model

Simulating Two-Dimensional Stick-Slip Motion of a Rigid Body using a New Friction Model Proceedings of the 2 nd World Congress on Mechanical, Chemical, and Material Engineering (MCM'16) Budapest, Hungary August 22 23, 2016 Paper No. ICMIE 116 DOI: 10.11159/icmie16.116 Simulating Two-Dimensional

More information

Sound Radiation Of Cast Iron

Sound Radiation Of Cast Iron Purdue University Purdue e-pubs International Compressor Engineering Conference School of Mechanical Engineering 2002 Sound Radiation Of Cast Iron N. I. Dreiman Tecumseh Products Company Follow this and

More information

e jωt = cos(ωt) + jsin(ωt),

e jωt = cos(ωt) + jsin(ωt), This chapter introduces you to the most useful mechanical oscillator model, a mass-spring system with a single degree of freedom. Basic understanding of this system is the gateway to the understanding

More information

Mechanical Design in Optical Engineering

Mechanical Design in Optical Engineering OPTI Buckling Buckling and Stability: As we learned in the previous lectures, structures may fail in a variety of ways, depending on the materials, load and support conditions. We had two primary concerns:

More information

1820. Selection of torsional vibration damper based on the results of simulation

1820. Selection of torsional vibration damper based on the results of simulation 8. Selection of torsional vibration damper based on the results of simulation Tomasz Matyja, Bogusław Łazarz Silesian University of Technology, Faculty of Transport, Gliwice, Poland Corresponding author

More information

Structural Dynamics A Graduate Course in Aerospace Engineering

Structural Dynamics A Graduate Course in Aerospace Engineering Structural Dynamics A Graduate Course in Aerospace Engineering By: H. Ahmadian ahmadian@iust.ac.ir The Science and Art of Structural Dynamics What do all the followings have in common? > A sport-utility

More information

Sound Propagation through Media. Nachiketa Tiwari Indian Institute of Technology Kanpur

Sound Propagation through Media. Nachiketa Tiwari Indian Institute of Technology Kanpur Sound Propagation through Media Nachiketa Tiwari Indian Institute of Technology Kanpur LECTURE-13 WAVE PROPAGATION IN SOLIDS Longitudinal Vibrations In Thin Plates Unlike 3-D solids, thin plates have surfaces

More information

Modelling and Finite Element Analysis of Double Wishbone Suspension

Modelling and Finite Element Analysis of Double Wishbone Suspension Modelling and Finite Element Analysis of Double Wishbone Suspension Amol Patil, Varsha Patil, Prashant Uhle P.G. Student, Dept. of Mechanical Engineering, S S B T S College of Engineering, Jalgaon, Maharastra,

More information

Program System for Machine Dynamics. Abstract. Version 5.0 November 2017

Program System for Machine Dynamics. Abstract. Version 5.0 November 2017 Program System for Machine Dynamics Abstract Version 5.0 November 2017 Ingenieur-Büro Klement Lerchenweg 2 D 65428 Rüsselsheim Phone +49/6142/55951 hd.klement@t-online.de What is MADYN? The program system

More information

NUMERICAL MODELLING OF RUBBER VIBRATION ISOLATORS

NUMERICAL MODELLING OF RUBBER VIBRATION ISOLATORS NUMERICAL MODELLING OF RUBBER VIBRATION ISOLATORS Clemens A.J. Beijers and André de Boer University of Twente P.O. Box 7, 75 AE Enschede, The Netherlands email: c.a.j.beijers@utwente.nl Abstract An important

More information

Effects of mass distribution and buoyancy on the sound radiation of a fluid loaded cylinder

Effects of mass distribution and buoyancy on the sound radiation of a fluid loaded cylinder Effects of mass distribution and buoyancy on the sound radiation of a fluid loaded cylinder Hongjian Wu, Herwig Peters, Roger Kinns and Nicole Kessissoglou School of Mechanical and Manufacturing, University

More information

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad - 500 043 AERONAUTICAL ENGINEERING DEFINITIONS AND TERMINOLOGY Course Name : ENGINEERING MECHANICS Course Code : AAEB01 Program :

More information

Numerical simulation of the coil spring and investigation the impact of tension and compression to the spring natural frequencies

Numerical simulation of the coil spring and investigation the impact of tension and compression to the spring natural frequencies Numerical simulation of the coil spring and investigation the impact of tension and compression to the spring natural frequencies F. D. Sorokin 1, Zhou Su 2 Bauman Moscow State Technical University, Moscow,

More information

TOPIC E: OSCILLATIONS EXAMPLES SPRING Q1. Find general solutions for the following differential equations:

TOPIC E: OSCILLATIONS EXAMPLES SPRING Q1. Find general solutions for the following differential equations: TOPIC E: OSCILLATIONS EXAMPLES SPRING 2019 Mathematics of Oscillating Systems Q1. Find general solutions for the following differential equations: Undamped Free Vibration Q2. A 4 g mass is suspended by

More information

Static and Dynamic Analysis of mm Steel Last Stage Blade for Steam Turbine

Static and Dynamic Analysis of mm Steel Last Stage Blade for Steam Turbine Applied and Computational Mechanics 3 (2009) 133 140 Static and Dynamic Analysis of 1 220 mm Steel Last Stage Blade for Steam Turbine T. Míšek a,,z.kubín a aškoda POWER a. s., Tylova 57, 316 00 Plzeň,

More information

Structural Dynamic Modification Studies Using Updated Finite Element Model

Structural Dynamic Modification Studies Using Updated Finite Element Model Structural Dynamic Modification Studies Using Updated Finite Element Model Gupta A. K., Nakra B. C. 1 and Kundra T. K. 2 IRDE Dehradun 1 NSIT New Delhi 2 Deptt. of Mechanical Engg. IIT New Delhi ABSTRACT.

More information

Dynamics of structures

Dynamics of structures Dynamics of structures 2.Vibrations: single degree of freedom system Arnaud Deraemaeker (aderaema@ulb.ac.be) 1 Outline of the chapter *One degree of freedom systems in real life Hypothesis Examples *Response

More information

ROLLER BEARING FAILURES IN REDUCTION GEAR CAUSED BY INADEQUATE DAMPING BY ELASTIC COUPLINGS FOR LOW ORDER EXCITATIONS

ROLLER BEARING FAILURES IN REDUCTION GEAR CAUSED BY INADEQUATE DAMPING BY ELASTIC COUPLINGS FOR LOW ORDER EXCITATIONS ROLLER BEARIG FAILURES I REDUCTIO GEAR CAUSED BY IADEQUATE DAMPIG BY ELASTIC COUPLIGS FOR LOW ORDER EXCITATIOS ~by Herbert Roeser, Trans Marine Propulsion Systems, Inc. Seattle Flexible couplings provide

More information

This equation of motion may be solved either by differential equation method or by graphical method as discussed below:

This equation of motion may be solved either by differential equation method or by graphical method as discussed below: 2.15. Frequency of Under Damped Forced Vibrations Consider a system consisting of spring, mass and damper as shown in Fig. 22. Let the system is acted upon by an external periodic (i.e. simple harmonic)

More information

a) Find the equation of motion of the system and write it in matrix form.

a) Find the equation of motion of the system and write it in matrix form. .003 Engineering Dynamics Problem Set Problem : Torsional Oscillator Two disks of radius r and r and mass m and m are mounted in series with steel shafts. The shaft between the base and m has length L

More information

1.053J/2.003J Dynamics and Control I Fall Final Exam 18 th December, 2007

1.053J/2.003J Dynamics and Control I Fall Final Exam 18 th December, 2007 1.053J/2.003J Dynamics and Control I Fall 2007 Final Exam 18 th December, 2007 Important Notes: 1. You are allowed to use three letter-size sheets (two-sides each) of notes. 2. There are five (5) problems

More information

COPYRIGHTED MATERIAL. Index

COPYRIGHTED MATERIAL. Index Index A Admissible function, 163 Amplification factor, 36 Amplitude, 1, 22 Amplitude-modulated carrier, 630 Amplitude ratio, 36 Antinodes, 612 Approximate analytical methods, 647 Assumed modes method,

More information

Coupled Drive Apparatus Modelling and Simulation

Coupled Drive Apparatus Modelling and Simulation University of Ljubljana Faculty of Electrical Engineering Victor Centellas Gil Coupled Drive Apparatus Modelling and Simulation Diploma thesis Menthor: prof. dr. Maja Atanasijević-Kunc Ljubljana, 2015

More information

Dynamic Model of a Badminton Stroke

Dynamic Model of a Badminton Stroke ISEA 28 CONFERENCE Dynamic Model of a Badminton Stroke M. Kwan* and J. Rasmussen Department of Mechanical Engineering, Aalborg University, 922 Aalborg East, Denmark Phone: +45 994 9317 / Fax: +45 9815

More information

Chapter 14 Oscillations. Copyright 2009 Pearson Education, Inc.

Chapter 14 Oscillations. Copyright 2009 Pearson Education, Inc. Chapter 14 Oscillations Oscillations of a Spring Simple Harmonic Motion Energy in the Simple Harmonic Oscillator Simple Harmonic Motion Related to Uniform Circular Motion The Simple Pendulum The Physical

More information

General Physics I. Lecture 12: Applications of Oscillatory Motion. Prof. WAN, Xin ( 万歆 )

General Physics I. Lecture 12: Applications of Oscillatory Motion. Prof. WAN, Xin ( 万歆 ) General Physics I Lecture 1: Applications of Oscillatory Motion Prof. WAN, Xin ( 万歆 ) inwan@zju.edu.cn http://zimp.zju.edu.cn/~inwan/ Outline The pendulum Comparing simple harmonic motion and uniform circular

More information

COMPARISON OF MODE SHAPE VECTORS IN OPERATIONAL MODAL ANALYSIS DEALING WITH CLOSELY SPACED MODES.

COMPARISON OF MODE SHAPE VECTORS IN OPERATIONAL MODAL ANALYSIS DEALING WITH CLOSELY SPACED MODES. IOMAC'5 6 th International Operational Modal Analysis Conference 5 May-4 Gijón - Spain COMPARISON OF MODE SHAPE VECTORS IN OPERATIONAL MODAL ANALYSIS DEALING WITH CLOSELY SPACED MODES. Olsen P., and Brincker

More information

Efficient Reduced Order Modeling of Low- to Mid-Frequency Vibration and Power Flow in Complex Structures

Efficient Reduced Order Modeling of Low- to Mid-Frequency Vibration and Power Flow in Complex Structures Efficient Reduced Order Modeling of Low- to Mid-Frequency Vibration and Power Flow in Complex Structures Yung-Chang Tan Graduate Student Research Assistant Matthew P. Castanier Assistant Research Scientist

More information

on the figure. Someone has suggested that, in terms of the degrees of freedom x1 and M. Note that if you think the given 1.2

on the figure. Someone has suggested that, in terms of the degrees of freedom x1 and M. Note that if you think the given 1.2 1) A two-story building frame is shown below. The mass of the frame is assumed to be lumped at the floor levels and the floor slabs are considered rigid. The floor masses and the story stiffnesses are

More information

3 Mathematical modeling of the torsional dynamics of a drill string

3 Mathematical modeling of the torsional dynamics of a drill string 3 Mathematical modeling of the torsional dynamics of a drill string 3.1 Introduction Many works about torsional vibrations on drilling systems [1, 12, 18, 24, 41] have been published using different numerical

More information

41514 Dynamics of Machinery

41514 Dynamics of Machinery 41514 Dynamics of Machinery Theory, Experiment, Phenomenology and Industrial Applications Ilmar Ferreira Santos 1. Recapitulation Mathematical Modeling & Steps 2. Example System of Particle 3. Example

More information

LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR.

LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR. LANMARK UNIVERSITY OMU-ARAN, KWARA STATE DEPARTMENT OF MECHANICAL ENGINEERING COURSE: MECHANICS OF MACHINE (MCE 322). LECTURER: ENGR. IBIKUNLE ROTIMI ADEDAYO SIMPLE HARMONIC MOTION. Introduction Consider

More information

A consistent dynamic finite element formulation for a pipe using Euler parameters

A consistent dynamic finite element formulation for a pipe using Euler parameters 111 A consistent dynamic finite element formulation for a pipe using Euler parameters Ara Arabyan and Yaqun Jiang Department of Aerospace and Mechanical Engineering, University of Arizona, Tucson, AZ 85721,

More information

1. Multiple Degree-of-Freedom (MDOF) Systems: Introduction

1. Multiple Degree-of-Freedom (MDOF) Systems: Introduction 1. Multiple Degree-of-Freedom (MDOF) Systems: Introduction Lesson Objectives: 1) List examples of MDOF structural systems and state assumptions of the idealizations. 2) Formulate the equation of motion

More information

T1 T e c h n i c a l S e c t i o n

T1 T e c h n i c a l S e c t i o n 1.5 Principles of Noise Reduction A good vibration isolation system is reducing vibration transmission through structures and thus, radiation of these vibration into air, thereby reducing noise. There

More information

1 2 Models, Theories, and Laws 1.5 Distinguish between models, theories, and laws 2.1 State the origin of significant figures in measurement

1 2 Models, Theories, and Laws 1.5 Distinguish between models, theories, and laws 2.1 State the origin of significant figures in measurement Textbook Correlation Textbook Correlation Physics 1115/2015 Chapter 1 Introduction, Measurement, Estimating 1.1 Describe thoughts of Aristotle vs. Galileo in describing motion 1 1 Nature of Science 1.2

More information

EQUIVALENT SINGLE-DEGREE-OF-FREEDOM SYSTEM AND FREE VIBRATION

EQUIVALENT SINGLE-DEGREE-OF-FREEDOM SYSTEM AND FREE VIBRATION 1 EQUIVALENT SINGLE-DEGREE-OF-FREEDOM SYSTEM AND FREE VIBRATION The course on Mechanical Vibration is an important part of the Mechanical Engineering undergraduate curriculum. It is necessary for the development

More information

Vibrations in Mechanical Systems

Vibrations in Mechanical Systems Maurice Roseau Vibrations in Mechanical Systems Analytical Methods and Applications With 112 Figures Springer-Verlag Berlin Heidelberg New York London Paris Tokyo Contents Chapter I. Forced Vibrations

More information

Abstract. 1 Introduction

Abstract. 1 Introduction Consideration of medium-speed four-stroke engines in ship vibration analyses I. Asmussen, A. Muller-Schmerl GermanischerLloyd, P.O. Box 111606, 20416Hamburg, Germany Abstract Vibration problems were recently

More information

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each.

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. GTE 2016 Q. 1 Q. 9 carry one mark each. D : SOLID MECHNICS Q.1 single degree of freedom vibrating system has mass of 5 kg, stiffness of 500 N/m and damping coefficient of 100 N-s/m. To make the system

More information

Design and Analysis of a Simple Nonlinear Vibration Absorber

Design and Analysis of a Simple Nonlinear Vibration Absorber IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE) e-issn: 78-1684,p-ISSN: 30-334X, Volume 11, Issue Ver. VI (Mar- Apr. 014), PP 84-90 Design and Analysis of a Simple Nonlinear Vibration Absorber

More information

CHAPTER 1: PHYSICAL QUANTITIES AMD MEASUREMENT

CHAPTER 1: PHYSICAL QUANTITIES AMD MEASUREMENT CHAPTER 1: PHYSICAL UANTITIES AMD MEASUREMENT 11 Physical uantities and Units a) State basic quantities and their respective SI units: length (m), time (s), mass (kg), electrical current (A), temperature

More information

A body is displaced from equilibrium. State the two conditions necessary for the body to execute simple harmonic motion

A body is displaced from equilibrium. State the two conditions necessary for the body to execute simple harmonic motion 1. Simple harmonic motion and the greenhouse effect (a) A body is displaced from equilibrium. State the two conditions necessary for the body to execute simple harmonic motion. 1. 2. (b) In a simple model

More information

PLEASURE VESSEL VIBRATION AND NOISE FINITE ELEMENT ANALYSIS

PLEASURE VESSEL VIBRATION AND NOISE FINITE ELEMENT ANALYSIS PLEASURE VESSEL VIBRATION AND NOISE FINITE ELEMENT ANALYSIS 1 Macchiavello, Sergio *, 2 Tonelli, Angelo 1 D Appolonia S.p.A., Italy, 2 Rina Services S.p.A., Italy KEYWORDS pleasure vessel, vibration analysis,

More information

Structural Dynamics Modification and Modal Modeling

Structural Dynamics Modification and Modal Modeling SEM Handboo of Experimental Structural Dynamics - Structural Dynamics Modification and Modal Modeling Structural Dynamics Modification and Modal Modeling Structural Dynamics Modification (SDM) also nown

More information

EMA 545 Final Exam - Prof. M. S. Allen Spring 2011

EMA 545 Final Exam - Prof. M. S. Allen Spring 2011 EMA 545 Final Exam - Prof. M. S. Allen Spring 2011 Honor Pledge: On my honor, I pledge that this exam represents my own work, and that I have neither given nor received inappropriate aid in the preparation

More information

TOPIC E: OSCILLATIONS SPRING 2019

TOPIC E: OSCILLATIONS SPRING 2019 TOPIC E: OSCILLATIONS SPRING 2019 1. Introduction 1.1 Overview 1.2 Degrees of freedom 1.3 Simple harmonic motion 2. Undamped free oscillation 2.1 Generalised mass-spring system: simple harmonic motion

More information

Dynamics of Ocean Structures Prof. Dr. Srinivasan Chandrasekaran Department of Ocean Engineering Indian Institute of Technology, Madras

Dynamics of Ocean Structures Prof. Dr. Srinivasan Chandrasekaran Department of Ocean Engineering Indian Institute of Technology, Madras Dynamics of Ocean Structures Prof. Dr. Srinivasan Chandrasekaran Department of Ocean Engineering Indian Institute of Technology, Madras Module - 1 Lecture - 20 Orthogonality of modes (Refer Slide Time:

More information

Advanced Vibrations. Distributed-Parameter Systems: Approximate Methods Lecture 20. By: H. Ahmadian

Advanced Vibrations. Distributed-Parameter Systems: Approximate Methods Lecture 20. By: H. Ahmadian Advanced Vibrations Distributed-Parameter Systems: Approximate Methods Lecture 20 By: H. Ahmadian ahmadian@iust.ac.ir Distributed-Parameter Systems: Approximate Methods Rayleigh's Principle The Rayleigh-Ritz

More information

Identification of Damping Using Proper Orthogonal Decomposition

Identification of Damping Using Proper Orthogonal Decomposition Identification of Damping Using Proper Orthogonal Decomposition M Khalil, S Adhikari and A Sarkar Department of Aerospace Engineering, University of Bristol, Bristol, U.K. Email: S.Adhikari@bristol.ac.uk

More information

Why You Can t Ignore Those Vibration Fixture Resonances Peter Avitabile, University of Massachusetts Lowell, Lowell, Massachusetts

Why You Can t Ignore Those Vibration Fixture Resonances Peter Avitabile, University of Massachusetts Lowell, Lowell, Massachusetts Why You Can t Ignore Those Vibration Fixture Resonances Peter Avitabile, University of Massachusetts Lowell, Lowell, Massachusetts SOUND AND VIBRATION March 1999 Vibration fixtures, at times, have resonant

More information

ScienceDirect. The Stability of a Precessing and Nutating Viscoelastic Beam with a Tip Mass

ScienceDirect. The Stability of a Precessing and Nutating Viscoelastic Beam with a Tip Mass Available online at www.sciencedirect.com ScienceDirect Procedia Engineering 144 (2016 ) 68 76 12th International Conference on Vibration Problems, ICOVP 2015 The Stability of a Precessing and Nutating

More information

Cardan s Coupling Shaft as a Dynamic Evolutionary System

Cardan s Coupling Shaft as a Dynamic Evolutionary System American Journal of Modern Physics and Application 2017; 4(2): 6-11 http://www.openscienceonline.com/journal/ajmpa Cardan s Coupling Shaft as a Dynamic Evolutionary System Petr Hrubý 1, Zdeněk Hlaváč 2,

More information

Investigation of a Ball Screw Feed Drive System Based on Dynamic Modeling for Motion Control

Investigation of a Ball Screw Feed Drive System Based on Dynamic Modeling for Motion Control Investigation of a Ball Screw Feed Drive System Based on Dynamic Modeling for Motion Control Yi-Cheng Huang *, Xiang-Yuan Chen Department of Mechatronics Engineering, National Changhua University of Education,

More information

Experimental investigation on the dynamic characteristics and transverse vibration instabilities of transmission belts

Experimental investigation on the dynamic characteristics and transverse vibration instabilities of transmission belts Experimental investigation on the dynamic characteristics and transverse vibration instabilities of transmission belts Lionel MANIN a, François BESSON a, Guilhem MICHON b, and Regis DUFOUR a a LaMCoS,

More information

Francisco Paulo Lépore Neto. Marcelo Braga dos Santos. Introduction 1. Nomenclature. Experimental Apparatus and Formulation

Francisco Paulo Lépore Neto. Marcelo Braga dos Santos. Introduction 1. Nomenclature. Experimental Apparatus and Formulation Francisco Paulo Lépore Neto and Marcelo Braga dos Santos Francisco Paulo Lépore Neto fplepore@mecanica.ufu.br Federal University of Uberlandia School of Mechanical Engineering 38408-902 Uberlandia, MG,

More information