Vibratory manipulation of elastically unconstrained part on a horizontal plane.
Baksys, B. ; Ramanauskyte, K. ; Povilionis, A.B. 等
VIBRATORY MANIPULATION OF ELASTICALLY UNCONSTRAINED PART ON A
HORIZONTAL PLANE
Summary
Theoretical and experimental investigation of the part motion on an
excited in two perpendicular directions horizontal plane is analyzed in
presented paper. The mathematical models of vibratory displacement, as
plane moves along circular or elliptical trajectories, were made. By the
simulation and experiments, motion trajectories of the parts during
positioning and search were investigated. The dependencies of the part
displacement, from the initial point towards the centre of steady
search, on the parameters of the systems and excitation were defined.
The part is positioned during the transient motion regime, while the
search occurs during the steady motion regime. It was verified
experimentally, that the part on the circularly or elliptically vibrating plane may be directed to predefined point and later is able to
perform search motion by circular or elliptical trajectory.
NESUVARZYTOS DETALES VIBRACINIS MANIPULIAVIMAS ANT HORIZONTALIOSIOS
PLOKSTUMOS
Reziume
Straipsnyje teoriskai ir eksperimentiskai nagrinejamas detales
judejimas ant horizontaliai dviem statmenomis kryptimis zadinamos
plokstumos. Sudaryti vibracinio slinkimo matematiniai modeliai, kai
plokstuma juda apskritimu ir elipse. Modeliuojant istirtos detales
judesio trajektorijos pozicionavimo ir paieskos metu, nustatytos detales
poslinkio nuo pradines padeties iki nusistovejusios trajektorijos centro
priklausomybes nuo sistemos ir zadinimo parametrii. Detale
pozicionuojama esant pereinamajam judesio rezimui, o paieskai budingas
nusistovejes judesio rezimas. Eksperimentiskai patvirtinta, kad ant
apskritimu ar elipse judancios plokstumos detale galima nukreipti i
nustatyta taska, o paskui apie si taska ji gali atlikti apskritimines ar
elipsines trajektorijos paieskos judesi.
B. Baksys, K. Ramanauskyte, A. B. Povilionis
[TEXT NOT REPRODUCIBLE IN ASCII.]
1. Introduction
Assembling is a final stage of manufacturing instruments, machines
and other more complex products, which takes from 25 to 50% of product
manufacturing time, and its expenditure is up to 50% of the product
price. With an increase in the batches of small products and in their
variety, the scope of assembly processes and manipulating operations
related to them also increase. For this reason more flexible manufacture
and assembly systems are needed. For smooth matching, the parts have to
be oriented and their connective surfaces have to be matched, thus
determining the effectiveness of automated mechanisms. Different
scientific papers analyze the processes of the parts manipulation by
means of various manipulators and robots whose operation is mostly based
on the active methods of matching connective surfaces of the parts.
These methods include the use of various sensors, vision systems,
control algorithms, feedback systems. All of these devices are expensive
and complex.
For assembly automation it is necessary to accomplish operations of
parts feeding into assembly position, orienting and positioning,
matching, joining and removing assembled units from the working area.
Matching of connective surfaces is the main stage of automated assembly
during which the parts are matched in the way they can be assembled
without difficulties. In recent years the manipulation of the parts and
assembly automation are performed using vibrations. The method of
vibratory search can be used for connective surfaces matching of the
parts. During the search one part must move along certain trajectories
in respect to the other part by the plane, which is perpendicular to the
connection axis. The centre of the connective part must fall into the
zone of allowable error, which is defined by the clearance between the
assembled parts, the size of the chamfers and the axial tilt angle.
The horizontal motion of parts on the horizontally excited plane
was experimentally investigated by D.S. Reznik [1,2], W.Y.Du [3]. The
basic problem is to compute a suitable closed motion of the plane, which
creates desirable frictional forces under each part. An important
contribution was to show that a sequence of plane rotations about a know
set of centres is the desired closed motion. Sensorless manipulations of
parts on the vertically vibrating plane were analyzed by Bohringer K.-F.
[4], and the parts on the horizontally and vertically excited and
segmented plane were examined by Frei P [5,6]. A. Federavicius [7, 8]
investigated transportation of a body on a vibrating plane when the
effective friction coefficient is controlled. Paper [9] shows, those
parts can be manipulated on a plane, witch is excited in two
perpendicular directions.
Vibratory transportation of the parts occurs when the plane is
excited along the transportation direction. For assembly automation it
is necessary to feed the parts into predetermined position and then
match the connective surfaces of the parts. During the positioning, the
slip motion of the parts should be pointed along the various directions.
It can be done by exciting the plane in two directions by equal
frequencies under the particular initial phase of the excitation signal.
Connective surfaces of the parts are matched when being positioned part
accomplishes the search motion near the positioning point. Therefore, it
is important to investigate part's motion regimes during the
positioning and search, aiming to identify the excitation parameters
that ensure the most effective matching of connective surfaces.
In this study the motion of a cylindrical part on a horizontally
vibrating plane has been theoretically and experimentally investigated
taking into account dynamic processes, and in addition the motion
regimes most suitable to manipulation of the parts being automatically
assembled have been determined.
2. Equations of part movement
The plane is excited in two perpendicular directions. By changing
the excitation amplitude, frequency and phase of the excitation signals,
the part can be easily and quickly redirected and provided with search
motion of different trajectories, and this way the matching of
connective surfaces is possible.
Investigated here is the manipulation of a body on a vibrating
plane. Let us assume that [xi][O.sub.[eta]] is an immovable coordinate
system located in a horizontal plane (Fig. 1). In the same plane a
coordinate system [xi][O.sub.LV] related to the vibrating plane is
located. The coordinate axes x and y are parallel to the axes [xi] and
[eta] respectively. Let us suppose that the plane motion in
[xi][O.sub.[eta]] coordinate system is uniform and runs in such a way
that every point traces a circle of radius [R.sub.e]. Thus motion of any
point of the plane is determined by the equations:
[xi] = [[xi].sub.0] + [R.sub.e]cos[omega]t; [eta] = [[eta].sub.0] +
Resin[omega]t (1)
where [omega] is the frequency of harmonic motion, t is time.
The body on a vibrating plane is presented as material particle of
mass m, influenced by the inertial force and constant friction force F =
[micro]mg, which has the direction opposite to the relative velocity.
Differential equations of the part motion on a vibrating plane are
ma[xi] = [F.sub.[xi], [ma.sub.n]=[F.sub.n] (2)
where [a.sub.[xi] and [a.sub.eta] are the projections of absolute
acceleration of the part onto the [xi] and [eta] axes.
[FIGURE 1 OMITTED]
When the body slides with respect to the plane x=x(t), y=y(t) and
acceleration projections of gravity center of the part are expressed by
two components
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.]
The first component determines relative acceleration of the part,
and the second component -acceleration of translation.
Friction force depends on the angle between the relative velocity
of the part and projections of the velocity onto the x and y axes.
Projections of the relative velocity of the part are denoted by [??] and
[??]. Then the projections of friction force onto [xi] and [eta] axes
(also onto the x, y axes) are
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.] (4)
where [micro] is coefficient of dry friction between the surfaces
of the body and the plane.
Substituting the expressions (3) and (4) into the body motion
equations (2) the following is obtained
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.] (5)
These equations are valid as the body slides on the plane, i.e. as
[x.sup.2] + [y.sup.2] [not equal to] 0.
It is necessary to determine such a trajectory of the body motion,
which results the connective surfaces search time to be the smallest.
3. Simulation of the part motion on the circularly vibrating plane
To solve Equations of motion (5), MATLAB software was applied and
the calculation code was written. By the results of mathematical
simulation it was determined that the part moving from the initial point
towards the positioning point has characteristic transient and steady
regimes of motion (Fig. 2). The character of the trajectory for
transient regime depends both on the excitation amplitude and frequency
as well as on the coefficient of friction and initial velocity. The part
can move to a predetermined position along a circular looping
trajectory, or along a curvilinear or linear trajectory. Such a
transient motion of the part may be used to accomplish part positioning
towards the other mating part. As the plane vibrates by a circular
trajectory, the trajectory of steady motion of the part is also
circular. The examples of part's center motion trajectories along x
and y directions are shown in Fig. 3.
It is possible to control the direction of motion by changing the
initial phase of excitation signals [8]. Steady motion of the part may
be used in search of the connective surfaces of the parts.
Under a significant positioning error of the connective surfaces,
i.e. when axial misalignment between the axes of the peg and the bushing
is larger than the diameter of the circular search trajectory, it is
necessary to position the surfaces prior to matching. Having known the
misalignment between the assembling parts, it is necessary to choose
magnitudes of the parameters so, that predefined positioning of the
parts to is ensured. As it is seen in Fig. 4, increasing the friction
coefficient [micro] the displacement K of the part from the initial
point to the centre of search motion rapidly decreases, and when
friction coefficient exceeds 0.1, the displacement decreases more
slowly. Increasing both the excitation frequency co and amplitude
[R.sub.e], part's displacement K increases (Fig. 5).
[FIGURE 2 OMITTED]
[FIGURE 3 OMITTED]
[FIGURE 4 OMITTED]
[FIGURE 5 OMITTED]
4. Simulation of motion of a part on a plane vibrating along
elliptical trajectory
As excitation of the plane in one direction has higher amplitude
than in the other direction, in the system of coordinates'
[xi][O.sub.[eta] every point of the plane traces an ellipse. Then the
motion of any point of the plane is determined by the equations
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.] (6)
where [A.sub.e] is the length of major axis of the ellipse,
[B.sub.e] is the length of minor axis of the ellipse
Motion of the part on the plane vibrating along elliptical
trajectory is expressed by the equations:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.] (7)
As the plane is subjected to elliptical vibrations, the trajectory
of the steady state motion regime of the part is also elliptical (Fig.
6). The character of the transient motion regime, which describes
movement of the part, while the plane moves along elliptical or circular
trajectory, practically does not differ.
The performed investigation showed, that under the same friction
coefficient and excitation frequency, as the plane is excited by the
elliptic trajectory, the displacement of the part from the initial point
to the centre of the steady search motion is bigger than that under
circular excitation of the plane. As the part is moving along steady
elliptic trajectory, the conditions for matching of connective surfaces
are more advantageous. If the axis of the part will cross the zone of
the allowable error, depends on the position of the trajectory centre
relative to the mentioned zone, the radius of the circle or on the
length of the ellipsis axes. When the minor axis of the ellipse is
smaller than the diameter of allowable error zone, the center of the
part will cross the mentioned zone.
[FIGURE 6 OMITTED]
[FIGURE 7 OMITTED]
It is possible to control movement direction of the part the same
way as if the plane is excided circularly [8], i.e. by varying the
initial phase of the excitation signals (Fig. 7). Under the same initial
phase of the excitation signal, but with different excitation amplitudes
along the x and y directions, the results change both in direction angle
of the part motion and in covered distance towards the centre of the
steady trajectory.
The direction angle y of the part movement on the plane follows a
complex law, which is represented as a sum of the sine curve and linear
function (dashed line) (Fig. 8). The larger is the difference between
the amplitudes [A.sub.e] and [B.sub.e]. of the plane excitation, the
larger is amplitude of the sine. The sine graph of the direction angle
change, when the amplitude of excitation along the x direction is
smaller than that along the y direction ([A.sub.e] < [B.sub.e]), it
is shifted by a half period of the sine.
[FIGURE 8 OMITTED]
5. Experimental investigation of unconstrained part motion on the
vibrating plane
Experimental setup and the method investigation. To verify the
results of theoretical the experiments of the unconstrained part motion
on vibrating plate analysis were carried out. The experimental setup was
designed and made (Fig. 9). Vibrating plate 1 is mounted on four elastic
rods 2. To the bottom surface of the plate DC motor 3 with eccentric
mass 4 is attached. The base 5 of the setup is immovably fixed to the
floor. DC motor 3 is connected to the voltage adjuster 6, which provides
the possibility to change the frequency of rotation. Eccentric mass 4
was used to control vibration amplitude of the plate 1. Elastic rods 2
were used to ensure horizontal motion of the plate relative to the base.
Part 7 was placed on the vibrating plate 1. Immovably fixed to the plate
reflective spheral marker 8 was used to capture motion of the plate,
while motion of the part on the vibrating plate was tracked by means of
the reflective marker 9, attached to the part. Four ProReflex MCU 500Hz
cameras were used to track motion of the part. 3D Qualisys Track Manager
(QTM) system was used for motion analysis.
Infrared (IR) light diodes, mounted around the cameras' lens,
emit the IR light, pointed towards the markers. IR light hits the
reflective markers and goes back to the camera lens, and so motion
trajectories of the markers are fixed. The center point of the spherical
marker is calculated in real time by sub-pixel interpolation algorithm.
The obtained data is momentarily transferred to computer, where QTM
system processes the data from all four cameras and performs automated
recognition of the markers. Then computer monitor reproduces 3D real
time trace of each marker. Besides, it is possible to make the 3D or
motion along the x, y and z axes graphs of each marker. Obtained by QTM
system data is stored in text file. By means of Microsoft Excel software
motion trajectories of the plate and the part along the x-y plane were
made.
[FIGURE 9 OMITTED]
Results of the experiments. It was determined during the
experiment, that providing small amplitude [A.sub.e]=0.012 m and
frequency [omega]=30 [s.sup.-1] excitation to the plane, it moves along
the circular trajectory (Fig. 10, a). The part placed on the aluminium
alloy plate, starts transient motion, in the direction, which depends on
the part placement moment in respect of the vibration period of the
plane, later motion trajectory gets steady (Fig. 10, b). Obtained during
the experiments, motion trajectories of the part positioning and search
are very similar to those obtained during the simulation (Fig. 3). It
was determined, that because of irregular roughness of different parts
of the plate, the loops of the transitional motion of the parts are of
different magnitudes and steady motion is not quite exactly circular.
The performed experiment showed, that under existing surface contact
(except of the point contact) of the part and the plate, because of
acting friction forces, the part also performs rotation along its own
axis, which was neglected during the simulation.
[FIGURE 10 OMITTED]
Exciting the plane by higher amplitude [A.sub.e]=0.012 m and
frequency co=30 [s.sub.-1], due to unequal rigidity of the rods along
the x and y directions and varying centrifugal inertia force, the
elliptic trajectory of the plane is obtained (Fig. 11, a), as at each
rotation an ellipse is drawn not exactly around the same point. As the
plate moves along the elliptic trajectory, the obtained steady motion
trajectory of the part is also elliptic (Fig. 11, b), which was also
defined during the simulation (Fig. 6). Furthermore, steady motion of
the part is not quite stable, i.e. the centre of the steady motion is
slightly varying. This is because of non-ideal conditions of the plate
excitation during the experiment and due to irregular roughness of the
plate surface.
[FIGURE 11 OMITTED]
[FIGURE 12 OMITTED]
[FIGURE 13 OMITTED]
Motion trajectories of the parts, made of the different materials,
consequently under different friction coefficients between the plane and
the part, are written. One of the parts is made of plastic, the other -
of steel. The parts were placed on the plane vibrating by the elliptical
trajectory (Fig. 12). The obtained motion trajectories of the parts are
shown in Figs. 13-14. It was determined during the experiments that as
friction coefficient between the steel part and the plane is bigger, the
displacement of the part from initial point is smaller. This verifies
the correctness of the simulation results.
[FIGURE 14 OMITTED]
Performing the experiments, it was observed, that close to the edge
of the plane small amplitude vibrations along the vertical direction are
excited. Therefore, close to the edge of the plane, the part changes
motion direction. To avoid such change in direction, it is necessary to
increase the rigidity of the plane.
6. Conclusions
1. Research was carried out considering the unconstraint part
motion on a plane, which is horizontally excited in two perpendicular
directions. It was determined that the part on the plane can be
positioned to a predefined point and provided with a search motion along
circular and elliptic trajectories.
2. Displacement of the part from the initial position to the centre
of search trajectory mainly depends on friction coefficient [micro] and
decreases increasing the friction, whereas increasing the excitation
frequency [omega] and the amplitude [R.sub.e], displacement increases.
3. Experimental results showed that motion trajectories of the part
positioning and search are very similar to simulation results. It was
determined, that because of irregular roughness of the different parts
of the plate, part's transitional motion loops are of different
magnitude and steady-motion is not quite exactly circular or elliptic.
Received November 15, 2008
References
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Accepted January 22, 2009
B. Baksys *, K. Ramanauskyte **, A. B. Povilionis ***
* Kaunas University of Technology, Kqstucio 27, 44312 Kaunas,
Lithuania, E-mail: Bronius.Baksys@ktu.lt ** Kaunas University of
Technology, Kqstucio 27, 44312 Kaunas, Lithuania, E-mail:
Kristina.Ramanauskyte@ktu.lt *** Kaunas University of Technology,
Kqstucio 27, 44312 Kaunas, Lithuania, E-mail: Algis.Povilionis@ktu.lt