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Journal of Energy Technologies and Policy                                                                 www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012



   Effects of Clearance Size on the Dynamic Response of Planar
 Multi-body Systems with Differently Located Frictionless Revolute
                         Clearance Joints
                                       Mutuku Muvengei1* John Kihiu1 Bernard Ikua2
     1.    Department of Mechanical Engineering, Jomo Kenyatta University of Agriculture and Technology PO Box
           62000-00200, Nairobi, Kenya
     2.    Department of Mechatronic Engineering, Jomo Kenyatta University of Agriculture and Technology PO Box
           62000-00200, Nairobi, Kenya.
                                    *Corresponding Author: ommuvengei@gmail.com


Abstract
This paper numerically investigates the effects of clearance size of differently located revolute clearance joints
without friction on the overall dynamic characteristics of a multi-body system. A typical planar slider-crank
mechanism is used as a demonstration case in which the effects of clearance size of a revolute clearance joint
between the crank and connecting rod (c-cr), and between the connecting rod and slider (s-cr) are separately
investigated with comprehensive observations numerically presented. It is observed that, different joints in a
multi-body system have different sensitivities to the clearance size. Therefore the dynamic behavior of one clearance
revolute joint cannot be used as a general case for a mechanical system. Also the location of the clearance revolute
joint and the clearance size play a crucial role in predicting accurately the dynamic responses of the system.
Keywords: Chaotic behavior, Contact-impact force, Dynamic response, Multi-body mechanical system, Periodic
behavior, Poincare Map, Quasi-periodic behavior, revolute clearance joint.


1. Introduction
In traditional dynamic modeling of multi-body systems, the effect of clearance at the joints is routinely ignored in order
to simplify the dynamic model. The increasing requirement for high-speed and precise machines, mechanisms and
manipulators demands that the kinematic joints be treated in a realistic way. This is because in a real mechanical joint,
a clearance which permits the relative motion between the connected bodies as well as the components assemblage is
always present.
There is a significant amount of literature available which discuses theoretical and experimental analysis of imperfect
kinematic joints in a variety of planar and spatial mechanical systems with rigid or flexible links (Muvengei et al.
2011b). Many of these works focus on the planar systems in which only one kinematic joint is modeled as an imperfect
joint. Although, the results from such experimental and analytical models have been shown to provide important
insights on the behavior of mechanical systems with imperfect joints, the models do not allow for study of the
interactions of multiple kinematic imperfect joints. Furthermore a real mechanical system does not have only one real
joint, but practically all joints are real. This led several researchers such as Flores (2004) and Cheriyan (2006) to
strongly recommend for their work to be extended to include multi-body mechanical systems with multiple imperfect
joints, and with a variety of joints such as prismatic and universal joints. Few recent papers by Erkaya and Uzmay
(2009; 2010) and by Flores (2010a) have considered the nonlinear dynamic analysis of multi-body systems with two
imperfect joints. However in these research papers, only mechanisms with rigid links have been considered and the
interaction effects of the imperfect joints on the overall response of a multi-body system were not investigated. Also,
Erkaya and Uzmay (2009; 2010) modeled the clearance in the journal bearing as a massless imaginary link whose
length is equal to the clearance size. This assumption is not valid especially at large clearances because the journal and
bearing will not be in contact at all times.


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Journal of Energy Technologies and Policy                                                                 www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012


Majority of the research works on the study of clearance joints have assumed that differently located revolute joints
in a multi-body system when modeled as clearance joints affect the dynamic behavior of the system in a similar
manner. Hence the inherent observations derived from investigating the dynamic behavior of one clearance revolute
joint have been used as general cases for all the joints in the mechanical system. Therefore, the primary objective of
this research work is to investigate numerically if the clearance size of differently located revolute clearance joints in
a multi-body system affect the behavior of the system in a similar dynamic manner or not. This work will provide
inherent information which can be of great use in the analysis of multi-body systems with clearance joints especially
as it regards to the effective design and control tasks of these systems. This study will also form a base towards the
investigation of dynamic interaction of multiple revolute clearance joints in a multi-body mechanical system.


2. Equation of Motion of Multi-body Systems
The methodology adopted in this work to derive the dynamic equations of multi-body systems follows closely that of
Nikravesh (1988) in which the generalized Cartesian coordinates and the Newton-Euler's approach are utilized. The
methodology presented is implemented in a MATLAB code, which is capable of automatically generating and
solving the equations of motion for the multi-body systems.
Computationally, the dynamic analysis of a multi-body mechanical system with real or ideal joints involves solving
                                            ••
Equation (1) for the acceleration vector    q    and vector of Langrage multipliers λ (Shabana 1994). Then, in each
integration time step, the accelerations vector, together with velocities vector are integrated in order to obtain the
system velocities and positions for the next time step. This procedure is repeated until the final analysis time is
reached.

                                                                 Qe               
                                        C q  q                                 
                                               ••
                                 M       T
                                             =                                                        (1)
                                 C      0  λ                                  
                                  q                    •    •         •

                                                    − (C q q) q q − 2C qt q − Ctt 
                                                                                   
M is the mass matrix, Cq is the Jacobi matrix and Qe is the vector containing the known external forces. The code
developed in this work was able to derive automatically the overall matrices in Equation (1) and subsequently solve
for the vectors of acceleration and Langrage multipliers, and finally integrate the vector for velocity and acceleration
to get the system positions and velocities for the next time step.
Since the system of the motion equations shown in Equation (1) does not use explicitly the position and velocity
equations associated with the kinematic constraints, chances are that the original constraint equations will be violated
during simulation. Due to simplicity and easiness of computational implementation, the Baumgarte Stabilization
Method (Baumgarte 1972) is employed in this work to control the position and velocity constraint violations brought
about by direct integration of Equation (1). By using the Baumgarte's approach, the equations of motion for a
dynamic system subjected to holonomic constraints are represented as,
                                               ••
                                 M     C q  q  
                                          T
                                                          Qe         
                                             =         •                                              (2)
                                 C      0  λ   Qd − 2α C − β 2C 
                                  q                             
Where C is the vector of constraint equations and       α and β are   termed as feedback parameters which should be
arbitrary chosen.
2.1. Kinematic Model of a Revolute Joint with Clearance
Figure 1 shows two bodies i and j connected with a revolute joint with clearance. Part of body i is the bearing while

                                                            8
Journal of Energy Technologies and Policy                                                                www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012


part of body j is the journal.
The eccentricity vector which connects the centers of the bearing and the journal is given as,
                                 →
                                 e = rPj − rpi = (R j + Aj uPj ) − ( Ri + Ai uPi )                          (3)

The magnitude of the eccentricity vector is

                                                           →T →
                                                   e= e e                                                   (4)

The penetration depth due to the impact between the journal and the bearing can be shown to be,

                                                   δ = e−c                                                  (5)
Where c is the radial clearance at the joint which is the difference between the radius of the bearing and the radius of
the journal of the clearance joint. The contact points on bodies i and j during indentation are Ci and Cj respectively as
shown in Figure 1.

                                                           →
                                                   →       e
                                                   n=                                                       (6)
                                                           e
The velocity of the contact points in the global coordinate system is,

                                                                           →
                                      •        •       •                   •
                                      r Ci = R i + Ai u Pi + RB n                                           (7)


                                                                           →
                                      •        •       •                   •
                                      r Cj = R j + A j u Pj + RJ n                                          (8)


         →
Where    n is the unit vector in the direction of indentation due to impact between the journal and the bearing, and
RB and RJ are the bearing and journal radii respectively.
The components of the relative velocity of the contact points in the normal and tangential plane of collision are given
as,

                                           →           •       •       →
                                           v N = (r Cj − r Ci ) n                                          (9)

                                           →           •       •       →
                                           v T = (r Cj − r Ci ) t                                         (10)

         →                                         →
Where    t is a unit vector obtained by rotating n anticlockwise by 900.
2.2. Dynamic Model of a Revolute Joint with Clearance
When the journal makes contact with the bearing, then impacts occur and contact-impact forces are created at the
                                                                   9
Journal of Energy Technologies and Policy                                                                www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012


joint. Closer inspection of Equation (5) shows that:
    •    When the journal is not in contact with the bearing, e<c and the indentation has a negative value. In this
         case, the journal is in free-flight motion inside the bearing, and no impact-contact forces are created.
    •    When contact between the journal and the bearing is established, the indentation has a value equal or greater
         than zero. In this case, impact-contact forces at the joint are established.
Therefore the computational algorithm developed for dynamic analysis of a system with revolute clearance joint
should ensure that impact-contact forces are applied when the depth of penetration is greater or equal to zero.
Since there are velocity components in the normal and tangential directions of the collision between the journal and
the bearings as given in Equation (9) and (10) then forces are generated in these two directions. The force normal to
the direction of collision FN can be evaluated using the contact force laws, such as Hertz, Lankarani-Nikravesh,
Dubowsky-Freudenstein or ESDU-78035 contact models, while the force tangential to the direction of collision FT
which is the frictional force is evaluated using the appropriate frictional laws.
In this paper, it is assumed that no frictional forces are generated during the collision of the bearing and the journal;
however friction will be included in further work. Since the direction of the normal unit vector is used as the working
direction for the contact forces, then the contact forces at body i is;
                                                              →
                                                  FNi = FN n                                              (11)

From the Newton's third law of motion, the contact reaction force at body j will be;

                                                  FNj = − FNi                                             (12)

These forces which act at the contact points are transferred to the center of masses of bodies i and j as shown in
Figure 2. This transfer of forces from contact forces to the center of masses contributes to the moments given as,

                                       M i = ( xCi − xi ) FNiY − ( yCi − yi ) FNiX                        (13)


                                       M j = ( xCi − xi ) FNjY − ( yCi − yi ) FNjX                        (14)

Once these forces and moments are known and added to the generalized vector of external forces Qe in Equation (2),
then the description of the revolute joint with clearance is complete. No kinematic constraint was used when
modeling the real joint; instead force constraints have been used.


2.3. Contact Force Models
Once the journal makes contact with the bearing, forces normal to the direction of contact are created. In this work
the nonlinear continuous contact force models between two colliding bodies will be used since they represent the
physical nature of the contacting surfaces. These contact force modes include; Hertz, Lankarani-Nikravesh,
Dubowsky-Freudenstein and ESDU-78035 contact force models. A detailed description of these contact-force
models is available in (Muvengei et al. 2011b).
It has been shown by several researchers such as (Flores et al. 2006;Muvengei et al. 2011a) that the two cylindrical
contact models (that is, Dubowsky-Freudenstein and ESDU-78035 contact models) do not present any added
advantage compared to the elastic spherical contact model (that is, the Hertz contact model).             However, the
cylindrical models are nonlinear and implicit functions, and therefore they require an iterative procedure such as
Newton-Raphson algorithm to solve them which is computationally time consuming. In this work therefore,
                                                             10
Journal of Energy Technologies and Policy                                                                   www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012


Lankarani-Nikravesh contact force model represented in Equation (15) is used to evaluate the force normal to the
direction of collision since it accounts for energy dissipation during the impact process.

                                                                 •
                                                                  
                                                     3(1 − ce2 ) δ 
                                        FN = Kδ 1 +n
                                                           •
                                                                                                              (15)
                                                                  
                                                      4δ (−) 


Exponent n=1.5 for metallic surfaces and the generalized stiffness K which depends on the material properties and
the shape of the contacting surfaces is given as;
                                                                               1
                                                    4         R1 R2  2
                                            K=                                                             (16)
                                               3(σ 1 + σ 2 )  R1 + R2 
Where R1 and R2 are the radii of the contacting spheres (the radius is negative for concave surfaces and positive for
convex surfaces), and σi‘s are material parameters given by,

                                                         1 − υ i2
                                                  σi =            for i=1, 2
                                                           Ei

With Ei and υi being the Young’s modulus and the Poisson’s ratio of each contacting sphere.


3. Results and Discussion
This section contains extensive results obtained from computational simulations of a slider-crank mechanism with a
revolute clearance joint. This study takes into account two main functional parameters of the slider-crank mechanism,
that is, the location of the considered clearance joint and the clearance size.


3.1 Description of the Slider-Crank Mechanism
A typical slider-crank mechanism as shown in Figure 3 is used as a demonstrative example to study the parametric
effect of revolute joint clearance on the dynamic response of a multi-body mechanical system.
The slider-crank mechanism considered has the following parameters: Length of crank LOA=0.05m, length of the
coupler link LAB=0.12m, mass of the crank m2=0.3kg, mass of the coupler m3=0.21kg, mass of the slider m4=0.14kg,
moment of inertia of crank I2=0.00001kg.m2 and moment of inertia of coupler I3=0.00025kg.m2. In addition all the
links are assumed to be uniform such that their centers of gravity are at their geometric centers. The following are
other parameters used for the different contact models: Nominal bearing diameter d=10mm, Length of the cylindrical
contact between the journal and the bearing L=20mm, Coefficient of restitution ce=0.9, Young's modulus E=207MPa,
Poisson's ratio υ=0.3 and reporting time step is 0.000001s.
The dynamic response of the slider-crank mechanism is presented by plotting the variations with time of the slider
velocity, slider acceleration and torque required to maintain constant speed of the crank. The behavior of the revolute
clearance joints is also illustrated by using the slider velocity and the slider acceleration to plot the phase portraits at
different test scenarios.


3.2 Influence of the Clearance Size

                                                             11
Journal of Energy Technologies and Policy                                                                  www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012


In this subsection, the influence of the clearance size at c-cr joint and also at s-cr joint on the dynamic behavior of the
slider-crank mechanism is investigated and comparisons presented. The range of the clearances used at each joint is
0.01mm, 0.1mm, 0.3mm and 0.5mm, and the crank rotates uniformly at 5000rev/min.
Figures 4 and 6 show that increasing the clearance size of a revolute joint, the mechanism experiences increased
peaks of the slider acceleration. This implies that at higher joint clearances, higher impacts followed by rebounds
take place, instead of continuous or permanent contact between the journal and the bearing walls. When the
clearance is small, the system response tends to be closer to the ideal response as evident in Figures 4(a) and 6(a).
This implies that at smaller clearance, the journal and the bearing of the joint experience a smaller number of impacts
and the journal follows the bearing wall. This is also evident in the phase portraits presented in Figures 5 for c-cr
from which it is clearly observed that increasing the radial clearance of this joint from 0.01mm to 0.5mm, the
behavior of the system changes from periodic to quasi-periodic. This quasi-periodic behavior is evident in the phase
portrait diagram because at large clearance sizes (0.3mm and 0.5mm), cycles of the mechanism fill up the diagram in
a fully predictable manner. When the clearance is small (0.01mm and 0.1mm), the behavior of the system tends to be
periodic since the cycles of the mechanism follow the same path in the phase portrait diagram. However, increasing
the clearance size beyond 0.5mm the behavior of the system changed from quasi-periodic to chaotic. At large
clearance sizes such as 0.3mm and 0.5mm, the three types of journal motion inside the bearing are clearly observed,
namely, the free-flight motion, the impact mode and the permanent or continuous contact mode.
However, as seen in Figure 7 increasing the radial clearance of the s-cr joint from 0.01mm to 0.5mm, the behavior of
the system changes from periodic to quasi-periodic, and then to chaotic. The chaotic behavior is evident in Figure 7(d)
since at a joint clearance of 0.5mm, different cycles of the mechanism lead to different curves in the phase portrait
diagram in an unpredictable manner. These observations are consistent with those made by (Flores et al. 2010b,
Flores et al. 2007) who investigated the effect of clearance size of a gudgeon joint (s-cr joint) on the behavior of a
slider-crank mechanism. This behavior is different from the one witnessed when only c-cr joint was modeled as a
revolute clearance joint, in which at a clearance of 0.5mm the behavior of the system was still quasi-periodic. This
shows that the dynamics of the revolute clearance s-cr joint in the slider-crank mechanism is more sensitive to the
clearance size as compared to that of revolute clearance c-cr joint. This confirms the already made observation that,
dynamic response peaks of the mechanism when s-cr joint is modeled as a real joint are higher than the peaks
produced when c-cr joint is modeled as a real joint with the same radial clearances. Although, the clearances of
different joints in a system show almost the same effects on the dynamic response of the system, it has been shown
that the joints will have different sensitivities to the clearance size. Therefore in order to design effective controllers
for eliminating fully the chaotic behaviors brought about by the non-linearities of joints with clearances, the dynamic
effect of each joint on the system should be understood, that is, the effects of clearance sizes in one joint cannot be
used as a general case in a mechanical system.


4. Conclusions
From the numerical simulations presented in this work, it can be concluded that the dynamic response of a
multi-body mechanical system with revolute clearance joint depends on the location of the joint and the clearance
size of the joint. It is clear that the dynamics of the revolute clearance joint in a mechanical system is quite sensitive
to the clearance size such that by slightly changing the value of the clearance size, the response of the system can
shift from chaotic to periodic behavior. However, the degree of sensitivity to the clearance size varies from one joint
to another. For instance in a slider-crank mechanism, the joint between the slider and connecting rod is more
sensitive to the clearance size than the joint between the crank and the connecting rod. This explains why many
researchers have emphasized on modeling the joint between the slider and connecting rod as a clearance joint.
Therefore in order to design effective controllers for eliminating fully the chaotic behaviors brought about by the
non-linearities of joints with clearances, the dynamic effect of each joint on the system should be understood. This is
because the effects of the clearance sizes in one clearance joint cannot be used as a general case in a mechanical
system.



                                                            12
Journal of Energy Technologies and Policy                                                               www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012


References
Baumgarte, J. (1972), “Stabilization of constraints and integrals of motion in dynamical systems,” Journal of
Computer Methods in Applied Mechanics and Engineering, vol. 1, pp. 1–16.
Cheriyan, S. K. (2006), “Characterization of Mechanical Systems with Real Joints and Flexible Links”, PhD. Thesis,
Wichita State University.
Erkaya, S., & Uzmay, I. (2009), “Investigation on effect of joint clearance on dynamics of four-bar mechanism”
Journal of Nonlinear Dynamics, vol. 58, pp. 179–198.
Erkaya, S., & Uzmay, I. (2010) “Experimental investigation of joint clearance effects on the dynamics of a slider-crank
mechanism” Journal of Multibody System Dynamics, vol. 24, pp. 81–102.
Flores, P. (2004a), “Dynamic Analysis of Mechanical Systems with Imperfect Kinematic Joints”, PhD. Thesis,
UNIVERSIDADE DO MINHO PARA.
Flores, P., & Ambrosio, J. (2004b), “Revolute joints with clearance in multibody systems,” Journal of Computers and
Structures, vol. 82, pp. 1359–1369.
Flores, P., Ambrosio, J., Claro, J. C. P., Lankarani, H. M. & Koshy, C. S. (2006a), “A study on dynamics of mechanical
systems including joints with clearance and lubrication”, Journal of Mechanism and Machine Theory, vol. 41, pp.
247-261.
Flores, P., Ambrosio, J., Claro, J. C. P., & Lankarani, H. M. (2006b), “Influence of the contact-impact force model on
the dynamic response of multi-body systems”, Journal of Multibody Dynamics, vol. 220, pp. 21-34.
Flores, P., Ambrosio, J., Claro, J. C. P., & Lankarani, H. M. (2007), “Dynamic behavior of planar rigid multibody
systems including revolute joints with clearance, Journal of Multibody Dynamics 161-174.
Flores, P., (2010a), “A parametric study on the dynamic response of planar multibody systems with multiple clearance
joints” Journal of Nonlinear Dynamics, vol. 4, pp. 633–653.
Flores, P., Koshy, C., Lankarani, H., Ambrosio, J., & Claro, J. (2010b), “Numerical and experimental investigation on
multibody systems with revolute clearance joints”, Journal of Nonlinear Dynamics.
Lankarani, H. M., & Nikravesh, P. E. (1990), “A contact force model with hysteresis damping for impact analysis of
multibody systems” Journal of Mechanical Design, vol. 112, pp. 369–376.
Muvengei, O., Kihiu, J. and Ikua, B. (2011a) “Effects of input speed on the dynamic response of planar multi-body
systems with differently located frictionless revolute clearance joints”. International Journal Mechanical and Materials
Engineering, vol. 4, pp. 234-243.
Muvengei, O. M. Kihiu, J. & Ikua, B. (2011b), “Dynamic Analysis of Multi-Body Mechanical Systems with
Imperfect Kinematic Joints: A Literature Survey and Review”, Sustainable Research and Innovation Conference,
JKUAT.
Nikravesh, P.E. (1988), Computer-Aided Analysis of Mechanical Systems, Prentice Hall, Englewood Cliffs, New
Jersey.
Shabana, A. A. (1994), Computational Dynamics, John Wiley & Sons, New York.




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Journal of Energy Technologies and Policy                                                      www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012




               Figure 1: Penetration depth due to impact between the bearing and the journal




                  Figure 2: Transfer of impact forces to the center of masses of the bodies




                                     Figure 3: Slider-crank mechanism

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Journal of Energy Technologies and Policy                                                              www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012




Figure 4. Slider acceleration responses for different clearance sizes at c-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d)
                                                         0.5mm




                                                         15
Journal of Energy Technologies and Policy                                                           www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012




   Figure 5. Phase portraits for different clearance sizes at c-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d)0.5mm




                                                        16
Journal of Energy Technologies and Policy                                                              www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012




Figure 6. Slider acceleration responses for different clearance sizes at s-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d)
                                                         0.5mm




                                                         17
Journal of Energy Technologies and Policy                                                           www.iiste.org
ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online)
Vol.2, No.3, 2012




   Figure 7. Phase portraits for different clearance sizes at s-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d)0.5mm




                                                        18
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Effects of clearance size on the dynamic response of planar multi body systems with differently located frictionless revolute clearance joints

  • 1. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Effects of Clearance Size on the Dynamic Response of Planar Multi-body Systems with Differently Located Frictionless Revolute Clearance Joints Mutuku Muvengei1* John Kihiu1 Bernard Ikua2 1. Department of Mechanical Engineering, Jomo Kenyatta University of Agriculture and Technology PO Box 62000-00200, Nairobi, Kenya 2. Department of Mechatronic Engineering, Jomo Kenyatta University of Agriculture and Technology PO Box 62000-00200, Nairobi, Kenya. *Corresponding Author: ommuvengei@gmail.com Abstract This paper numerically investigates the effects of clearance size of differently located revolute clearance joints without friction on the overall dynamic characteristics of a multi-body system. A typical planar slider-crank mechanism is used as a demonstration case in which the effects of clearance size of a revolute clearance joint between the crank and connecting rod (c-cr), and between the connecting rod and slider (s-cr) are separately investigated with comprehensive observations numerically presented. It is observed that, different joints in a multi-body system have different sensitivities to the clearance size. Therefore the dynamic behavior of one clearance revolute joint cannot be used as a general case for a mechanical system. Also the location of the clearance revolute joint and the clearance size play a crucial role in predicting accurately the dynamic responses of the system. Keywords: Chaotic behavior, Contact-impact force, Dynamic response, Multi-body mechanical system, Periodic behavior, Poincare Map, Quasi-periodic behavior, revolute clearance joint. 1. Introduction In traditional dynamic modeling of multi-body systems, the effect of clearance at the joints is routinely ignored in order to simplify the dynamic model. The increasing requirement for high-speed and precise machines, mechanisms and manipulators demands that the kinematic joints be treated in a realistic way. This is because in a real mechanical joint, a clearance which permits the relative motion between the connected bodies as well as the components assemblage is always present. There is a significant amount of literature available which discuses theoretical and experimental analysis of imperfect kinematic joints in a variety of planar and spatial mechanical systems with rigid or flexible links (Muvengei et al. 2011b). Many of these works focus on the planar systems in which only one kinematic joint is modeled as an imperfect joint. Although, the results from such experimental and analytical models have been shown to provide important insights on the behavior of mechanical systems with imperfect joints, the models do not allow for study of the interactions of multiple kinematic imperfect joints. Furthermore a real mechanical system does not have only one real joint, but practically all joints are real. This led several researchers such as Flores (2004) and Cheriyan (2006) to strongly recommend for their work to be extended to include multi-body mechanical systems with multiple imperfect joints, and with a variety of joints such as prismatic and universal joints. Few recent papers by Erkaya and Uzmay (2009; 2010) and by Flores (2010a) have considered the nonlinear dynamic analysis of multi-body systems with two imperfect joints. However in these research papers, only mechanisms with rigid links have been considered and the interaction effects of the imperfect joints on the overall response of a multi-body system were not investigated. Also, Erkaya and Uzmay (2009; 2010) modeled the clearance in the journal bearing as a massless imaginary link whose length is equal to the clearance size. This assumption is not valid especially at large clearances because the journal and bearing will not be in contact at all times. 7
  • 2. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Majority of the research works on the study of clearance joints have assumed that differently located revolute joints in a multi-body system when modeled as clearance joints affect the dynamic behavior of the system in a similar manner. Hence the inherent observations derived from investigating the dynamic behavior of one clearance revolute joint have been used as general cases for all the joints in the mechanical system. Therefore, the primary objective of this research work is to investigate numerically if the clearance size of differently located revolute clearance joints in a multi-body system affect the behavior of the system in a similar dynamic manner or not. This work will provide inherent information which can be of great use in the analysis of multi-body systems with clearance joints especially as it regards to the effective design and control tasks of these systems. This study will also form a base towards the investigation of dynamic interaction of multiple revolute clearance joints in a multi-body mechanical system. 2. Equation of Motion of Multi-body Systems The methodology adopted in this work to derive the dynamic equations of multi-body systems follows closely that of Nikravesh (1988) in which the generalized Cartesian coordinates and the Newton-Euler's approach are utilized. The methodology presented is implemented in a MATLAB code, which is capable of automatically generating and solving the equations of motion for the multi-body systems. Computationally, the dynamic analysis of a multi-body mechanical system with real or ideal joints involves solving •• Equation (1) for the acceleration vector q and vector of Langrage multipliers λ (Shabana 1994). Then, in each integration time step, the accelerations vector, together with velocities vector are integrated in order to obtain the system velocities and positions for the next time step. This procedure is repeated until the final analysis time is reached.  Qe  C q  q    •• M T    =   (1) C 0  λ     q    • • •  − (C q q) q q − 2C qt q − Ctt   M is the mass matrix, Cq is the Jacobi matrix and Qe is the vector containing the known external forces. The code developed in this work was able to derive automatically the overall matrices in Equation (1) and subsequently solve for the vectors of acceleration and Langrage multipliers, and finally integrate the vector for velocity and acceleration to get the system positions and velocities for the next time step. Since the system of the motion equations shown in Equation (1) does not use explicitly the position and velocity equations associated with the kinematic constraints, chances are that the original constraint equations will be violated during simulation. Due to simplicity and easiness of computational implementation, the Baumgarte Stabilization Method (Baumgarte 1972) is employed in this work to control the position and velocity constraint violations brought about by direct integration of Equation (1). By using the Baumgarte's approach, the equations of motion for a dynamic system subjected to holonomic constraints are represented as, •• M C q  q   T Qe     =  •  (2) C 0  λ   Qd − 2α C − β 2C   q     Where C is the vector of constraint equations and α and β are termed as feedback parameters which should be arbitrary chosen. 2.1. Kinematic Model of a Revolute Joint with Clearance Figure 1 shows two bodies i and j connected with a revolute joint with clearance. Part of body i is the bearing while 8
  • 3. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 part of body j is the journal. The eccentricity vector which connects the centers of the bearing and the journal is given as, → e = rPj − rpi = (R j + Aj uPj ) − ( Ri + Ai uPi ) (3) The magnitude of the eccentricity vector is →T → e= e e (4) The penetration depth due to the impact between the journal and the bearing can be shown to be, δ = e−c (5) Where c is the radial clearance at the joint which is the difference between the radius of the bearing and the radius of the journal of the clearance joint. The contact points on bodies i and j during indentation are Ci and Cj respectively as shown in Figure 1. → → e n= (6) e The velocity of the contact points in the global coordinate system is, → • • • • r Ci = R i + Ai u Pi + RB n (7) → • • • • r Cj = R j + A j u Pj + RJ n (8) → Where n is the unit vector in the direction of indentation due to impact between the journal and the bearing, and RB and RJ are the bearing and journal radii respectively. The components of the relative velocity of the contact points in the normal and tangential plane of collision are given as, → • • → v N = (r Cj − r Ci ) n (9) → • • → v T = (r Cj − r Ci ) t (10) → → Where t is a unit vector obtained by rotating n anticlockwise by 900. 2.2. Dynamic Model of a Revolute Joint with Clearance When the journal makes contact with the bearing, then impacts occur and contact-impact forces are created at the 9
  • 4. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 joint. Closer inspection of Equation (5) shows that: • When the journal is not in contact with the bearing, e<c and the indentation has a negative value. In this case, the journal is in free-flight motion inside the bearing, and no impact-contact forces are created. • When contact between the journal and the bearing is established, the indentation has a value equal or greater than zero. In this case, impact-contact forces at the joint are established. Therefore the computational algorithm developed for dynamic analysis of a system with revolute clearance joint should ensure that impact-contact forces are applied when the depth of penetration is greater or equal to zero. Since there are velocity components in the normal and tangential directions of the collision between the journal and the bearings as given in Equation (9) and (10) then forces are generated in these two directions. The force normal to the direction of collision FN can be evaluated using the contact force laws, such as Hertz, Lankarani-Nikravesh, Dubowsky-Freudenstein or ESDU-78035 contact models, while the force tangential to the direction of collision FT which is the frictional force is evaluated using the appropriate frictional laws. In this paper, it is assumed that no frictional forces are generated during the collision of the bearing and the journal; however friction will be included in further work. Since the direction of the normal unit vector is used as the working direction for the contact forces, then the contact forces at body i is; → FNi = FN n (11) From the Newton's third law of motion, the contact reaction force at body j will be; FNj = − FNi (12) These forces which act at the contact points are transferred to the center of masses of bodies i and j as shown in Figure 2. This transfer of forces from contact forces to the center of masses contributes to the moments given as, M i = ( xCi − xi ) FNiY − ( yCi − yi ) FNiX (13) M j = ( xCi − xi ) FNjY − ( yCi − yi ) FNjX (14) Once these forces and moments are known and added to the generalized vector of external forces Qe in Equation (2), then the description of the revolute joint with clearance is complete. No kinematic constraint was used when modeling the real joint; instead force constraints have been used. 2.3. Contact Force Models Once the journal makes contact with the bearing, forces normal to the direction of contact are created. In this work the nonlinear continuous contact force models between two colliding bodies will be used since they represent the physical nature of the contacting surfaces. These contact force modes include; Hertz, Lankarani-Nikravesh, Dubowsky-Freudenstein and ESDU-78035 contact force models. A detailed description of these contact-force models is available in (Muvengei et al. 2011b). It has been shown by several researchers such as (Flores et al. 2006;Muvengei et al. 2011a) that the two cylindrical contact models (that is, Dubowsky-Freudenstein and ESDU-78035 contact models) do not present any added advantage compared to the elastic spherical contact model (that is, the Hertz contact model). However, the cylindrical models are nonlinear and implicit functions, and therefore they require an iterative procedure such as Newton-Raphson algorithm to solve them which is computationally time consuming. In this work therefore, 10
  • 5. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Lankarani-Nikravesh contact force model represented in Equation (15) is used to evaluate the force normal to the direction of collision since it accounts for energy dissipation during the impact process. •   3(1 − ce2 ) δ  FN = Kδ 1 +n • (15)    4δ (−)  Exponent n=1.5 for metallic surfaces and the generalized stiffness K which depends on the material properties and the shape of the contacting surfaces is given as; 1 4  R1 R2  2 K=   (16) 3(σ 1 + σ 2 )  R1 + R2  Where R1 and R2 are the radii of the contacting spheres (the radius is negative for concave surfaces and positive for convex surfaces), and σi‘s are material parameters given by, 1 − υ i2 σi = for i=1, 2 Ei With Ei and υi being the Young’s modulus and the Poisson’s ratio of each contacting sphere. 3. Results and Discussion This section contains extensive results obtained from computational simulations of a slider-crank mechanism with a revolute clearance joint. This study takes into account two main functional parameters of the slider-crank mechanism, that is, the location of the considered clearance joint and the clearance size. 3.1 Description of the Slider-Crank Mechanism A typical slider-crank mechanism as shown in Figure 3 is used as a demonstrative example to study the parametric effect of revolute joint clearance on the dynamic response of a multi-body mechanical system. The slider-crank mechanism considered has the following parameters: Length of crank LOA=0.05m, length of the coupler link LAB=0.12m, mass of the crank m2=0.3kg, mass of the coupler m3=0.21kg, mass of the slider m4=0.14kg, moment of inertia of crank I2=0.00001kg.m2 and moment of inertia of coupler I3=0.00025kg.m2. In addition all the links are assumed to be uniform such that their centers of gravity are at their geometric centers. The following are other parameters used for the different contact models: Nominal bearing diameter d=10mm, Length of the cylindrical contact between the journal and the bearing L=20mm, Coefficient of restitution ce=0.9, Young's modulus E=207MPa, Poisson's ratio υ=0.3 and reporting time step is 0.000001s. The dynamic response of the slider-crank mechanism is presented by plotting the variations with time of the slider velocity, slider acceleration and torque required to maintain constant speed of the crank. The behavior of the revolute clearance joints is also illustrated by using the slider velocity and the slider acceleration to plot the phase portraits at different test scenarios. 3.2 Influence of the Clearance Size 11
  • 6. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 In this subsection, the influence of the clearance size at c-cr joint and also at s-cr joint on the dynamic behavior of the slider-crank mechanism is investigated and comparisons presented. The range of the clearances used at each joint is 0.01mm, 0.1mm, 0.3mm and 0.5mm, and the crank rotates uniformly at 5000rev/min. Figures 4 and 6 show that increasing the clearance size of a revolute joint, the mechanism experiences increased peaks of the slider acceleration. This implies that at higher joint clearances, higher impacts followed by rebounds take place, instead of continuous or permanent contact between the journal and the bearing walls. When the clearance is small, the system response tends to be closer to the ideal response as evident in Figures 4(a) and 6(a). This implies that at smaller clearance, the journal and the bearing of the joint experience a smaller number of impacts and the journal follows the bearing wall. This is also evident in the phase portraits presented in Figures 5 for c-cr from which it is clearly observed that increasing the radial clearance of this joint from 0.01mm to 0.5mm, the behavior of the system changes from periodic to quasi-periodic. This quasi-periodic behavior is evident in the phase portrait diagram because at large clearance sizes (0.3mm and 0.5mm), cycles of the mechanism fill up the diagram in a fully predictable manner. When the clearance is small (0.01mm and 0.1mm), the behavior of the system tends to be periodic since the cycles of the mechanism follow the same path in the phase portrait diagram. However, increasing the clearance size beyond 0.5mm the behavior of the system changed from quasi-periodic to chaotic. At large clearance sizes such as 0.3mm and 0.5mm, the three types of journal motion inside the bearing are clearly observed, namely, the free-flight motion, the impact mode and the permanent or continuous contact mode. However, as seen in Figure 7 increasing the radial clearance of the s-cr joint from 0.01mm to 0.5mm, the behavior of the system changes from periodic to quasi-periodic, and then to chaotic. The chaotic behavior is evident in Figure 7(d) since at a joint clearance of 0.5mm, different cycles of the mechanism lead to different curves in the phase portrait diagram in an unpredictable manner. These observations are consistent with those made by (Flores et al. 2010b, Flores et al. 2007) who investigated the effect of clearance size of a gudgeon joint (s-cr joint) on the behavior of a slider-crank mechanism. This behavior is different from the one witnessed when only c-cr joint was modeled as a revolute clearance joint, in which at a clearance of 0.5mm the behavior of the system was still quasi-periodic. This shows that the dynamics of the revolute clearance s-cr joint in the slider-crank mechanism is more sensitive to the clearance size as compared to that of revolute clearance c-cr joint. This confirms the already made observation that, dynamic response peaks of the mechanism when s-cr joint is modeled as a real joint are higher than the peaks produced when c-cr joint is modeled as a real joint with the same radial clearances. Although, the clearances of different joints in a system show almost the same effects on the dynamic response of the system, it has been shown that the joints will have different sensitivities to the clearance size. Therefore in order to design effective controllers for eliminating fully the chaotic behaviors brought about by the non-linearities of joints with clearances, the dynamic effect of each joint on the system should be understood, that is, the effects of clearance sizes in one joint cannot be used as a general case in a mechanical system. 4. Conclusions From the numerical simulations presented in this work, it can be concluded that the dynamic response of a multi-body mechanical system with revolute clearance joint depends on the location of the joint and the clearance size of the joint. It is clear that the dynamics of the revolute clearance joint in a mechanical system is quite sensitive to the clearance size such that by slightly changing the value of the clearance size, the response of the system can shift from chaotic to periodic behavior. However, the degree of sensitivity to the clearance size varies from one joint to another. For instance in a slider-crank mechanism, the joint between the slider and connecting rod is more sensitive to the clearance size than the joint between the crank and the connecting rod. This explains why many researchers have emphasized on modeling the joint between the slider and connecting rod as a clearance joint. Therefore in order to design effective controllers for eliminating fully the chaotic behaviors brought about by the non-linearities of joints with clearances, the dynamic effect of each joint on the system should be understood. This is because the effects of the clearance sizes in one clearance joint cannot be used as a general case in a mechanical system. 12
  • 7. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 References Baumgarte, J. (1972), “Stabilization of constraints and integrals of motion in dynamical systems,” Journal of Computer Methods in Applied Mechanics and Engineering, vol. 1, pp. 1–16. Cheriyan, S. K. (2006), “Characterization of Mechanical Systems with Real Joints and Flexible Links”, PhD. Thesis, Wichita State University. Erkaya, S., & Uzmay, I. (2009), “Investigation on effect of joint clearance on dynamics of four-bar mechanism” Journal of Nonlinear Dynamics, vol. 58, pp. 179–198. Erkaya, S., & Uzmay, I. (2010) “Experimental investigation of joint clearance effects on the dynamics of a slider-crank mechanism” Journal of Multibody System Dynamics, vol. 24, pp. 81–102. Flores, P. (2004a), “Dynamic Analysis of Mechanical Systems with Imperfect Kinematic Joints”, PhD. Thesis, UNIVERSIDADE DO MINHO PARA. Flores, P., & Ambrosio, J. (2004b), “Revolute joints with clearance in multibody systems,” Journal of Computers and Structures, vol. 82, pp. 1359–1369. Flores, P., Ambrosio, J., Claro, J. C. P., Lankarani, H. M. & Koshy, C. S. (2006a), “A study on dynamics of mechanical systems including joints with clearance and lubrication”, Journal of Mechanism and Machine Theory, vol. 41, pp. 247-261. Flores, P., Ambrosio, J., Claro, J. C. P., & Lankarani, H. M. (2006b), “Influence of the contact-impact force model on the dynamic response of multi-body systems”, Journal of Multibody Dynamics, vol. 220, pp. 21-34. Flores, P., Ambrosio, J., Claro, J. C. P., & Lankarani, H. M. (2007), “Dynamic behavior of planar rigid multibody systems including revolute joints with clearance, Journal of Multibody Dynamics 161-174. Flores, P., (2010a), “A parametric study on the dynamic response of planar multibody systems with multiple clearance joints” Journal of Nonlinear Dynamics, vol. 4, pp. 633–653. Flores, P., Koshy, C., Lankarani, H., Ambrosio, J., & Claro, J. (2010b), “Numerical and experimental investigation on multibody systems with revolute clearance joints”, Journal of Nonlinear Dynamics. Lankarani, H. M., & Nikravesh, P. E. (1990), “A contact force model with hysteresis damping for impact analysis of multibody systems” Journal of Mechanical Design, vol. 112, pp. 369–376. Muvengei, O., Kihiu, J. and Ikua, B. (2011a) “Effects of input speed on the dynamic response of planar multi-body systems with differently located frictionless revolute clearance joints”. International Journal Mechanical and Materials Engineering, vol. 4, pp. 234-243. Muvengei, O. M. Kihiu, J. & Ikua, B. (2011b), “Dynamic Analysis of Multi-Body Mechanical Systems with Imperfect Kinematic Joints: A Literature Survey and Review”, Sustainable Research and Innovation Conference, JKUAT. Nikravesh, P.E. (1988), Computer-Aided Analysis of Mechanical Systems, Prentice Hall, Englewood Cliffs, New Jersey. Shabana, A. A. (1994), Computational Dynamics, John Wiley & Sons, New York. 13
  • 8. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Figure 1: Penetration depth due to impact between the bearing and the journal Figure 2: Transfer of impact forces to the center of masses of the bodies Figure 3: Slider-crank mechanism 14
  • 9. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Figure 4. Slider acceleration responses for different clearance sizes at c-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d) 0.5mm 15
  • 10. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Figure 5. Phase portraits for different clearance sizes at c-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d)0.5mm 16
  • 11. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Figure 6. Slider acceleration responses for different clearance sizes at s-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d) 0.5mm 17
  • 12. Journal of Energy Technologies and Policy www.iiste.org ISSN 2224-3232 (Paper) ISSN 2225-0573 (Online) Vol.2, No.3, 2012 Figure 7. Phase portraits for different clearance sizes at s-cr joint (a) 0.01mm (b) 0.1mm (c) 0.3mm (d)0.5mm 18
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