Development of the method of accuracy measuring of precision spindle/Patobulintas metodas precizinio suklio sukimosi paklaidoms ivertinti.
Kasparaitis, A. ; Giniotis, V.
1. Introduction
The accuracy of the rotation of a spindle is evaluated by radial,
axial and angular errors [1, 2]. During the formation of the circular
raster scales and after that--during the calibration of angle
standards--circular scales of periodic or coded structure, one of the
most influential constituents on its uncertainty are radial errors of
the spindle rotation, on which the disc for scale formation or
calibration is placed in the plane of the circular scale [3, 4]. An
objective point for the determination of accuracy uncertainty of this
rotation has a great influence for minimization of these errors or its
correction by calculated compensation of the systematic error or during
the correction of the production process and rotary tables and angle
standards as well.
Here we present an intention to assess disadvantages of the
evaluation of these errors according to roundness reference measure
(template) and the proposals for elimination of these disadvantages.
2. Subjectivity of assessment of radial rotation errors
Assessment of radial error of rotation in respect of fixed
unmovable basis. Applying this method, the reference measure of
roundness is fixed to the spindle to be calibrated by means of the
centring adjustable device. During this operation, movements of the
centre are measured by two pick-ups of small linear displacement. Errors
in radial direction are evaluated according to the value of displacement
of the centre of the roundness measure in two perpendiculars to each
other and to the axis of rotation directions or by assessing of the
Lissajouis figures developed by vectorial sum of the displacements
mentioned above [5]. During the calibration of precision spindles a
glass or of other material made spherical (usually, semispherical) or
cylindrical body (artefact) is used. The deviations of the cross-section
of the artefact from roundness not exceed 0.01-0.02 [micro]m. The
pick-ups of small displacement are fixed to the unmovable body of the
spindle.
During the measurement of the rotation the error in one dimensional
direction is assessed by sum of harmonic constituents of all the
movements of the centre of a spherical body. During the measurement of
rotation error in the plane, the radial error usually is assessed by the
displacement of the centre of the sphere in the plane by the width of
the ring of trajectory. The result of measurement is evaluated according
to trajectory's declinations including constituents of
spindle's displacements in the plane, eccentricity of the roundness
measurement standard and its cross-section declinations from the
roundness in the plane.
For accuracy improvement of the calibration, some means are taken
to eliminate deviations from roundness of the standard measure although
there are no efforts made to eliminate an influence of the eccentricity
of roundness standard to the axis of spindle rotation [6]. The influence
of this parameter on the results of calibration is demonstrated further.
Displacement of the centre [O.sub.2] of the roundness standard in
the fixed coordinate system XOY according to the scheme in Fig. 1 is
expressed by the equation
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (1)
where [e.sub.1] is the radius of trajectory of the spindle centre
[O.sub.1] in the plane of measurement, [e.sub.2] is the eccentricity of
the roundness standard in the measuring plane according to the spindle
axis, [[beta].sub.0] is the angle between positive value of axis X and
radius [e.sub.1] at the initial position of the spindle, [[tau].sub.0]
is the angle between positive value of axis [X.sub.1] and eccentricity
[e.sub.2], [[omega].sub.1] and [[omega].sub.2] are angular velocity of
the vector [e.sub.1] and of the spindle, t is time.
[FIGURE 1 OMITTED]
XOY is fixed coordinate system, the initial point O of which
coincides with the hole of the spindle axis rotation;
[X.sub.1][O.sub.1][Y.sub.1] is movable coordinate system an initial
point [O.sub.1] of which coincides with the axis of spindle;
[beta]--angle of rotation of radius [e.sub.1]; [tau] is angle of
declination of the movable coordinate system
[X.sub.1][O.sub.1][Y.sub.1], angle of rotation of the spindle; 1 x and 1
y are directions of the measurement of radial displacement of the
roundness standard; [O.sub.2] is centre of the roundness standard in the
measuring plane.
The radius e of the trajectory of centre [O.sub.2] of roundness
measure and polar angle [alpha] in polar coordinate system are described
by the equations
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
where [[omega].sub.0] = [[tau].sub.0]-[[beta].sub.0] is angle
between the radii [e.sub.1] and [e.sub.2] at the initial position of the
spindle.
Aerostatic and hydrodynamic bearings as well as roll bearings of
special construction are mainly used in precision measuring and
technological equipment [7, 8]. The trajectory of the axis of such
bearings in the measuring plane can be described by Fourier series with
adequate accuracy
[e.sub.1] = [e.sub.10] + [n.summation over (i=1)] [A.sub.1] sin i
[[omega].sub.2] t + [[zeta].sub.0i], (3)
where [e.sub.10] is mean value of [e.sub.1,] [A.sub.i] is the
amplitude of vector [e.sub.1] by change of frequency i[[omega].sub.2],
[[zeta].sub.0i] is initial phase value of i-th harmonic of [e.sub.1], i
is harmonic's number.
It is the feature of aerostatic spindles an irregular trajectory of
the axis rotation. By assumption hat the trajectory has an elliptic
pattern, it can be strictly described by the Eq. (3) in case of i = 2
and [[omega].sub.1] = [[omega].sub.2]. Then the radius of rotation
standard centre [O.sub.2] and polar angle [alpha] in polar coordinate
system in the plane of measurement will be described by the Eq. (4).
Analysis of these equations shows that the centre trajectory of the
rotation standard in the measuring plane depends on eccentricity
[e.sub.2] and angle [[psi].sub.0]. During their variation, essential
changes of its form occur as well as orientation and according to its
ring's width an radial rotation error can be determined.
This can be illustrated by the graphs of radial error of aerostatic
spindles in the measuring plane in case when eccentricity of the
roundness measure according to the rotation error of the spindle differs
(Fig. 2).
Radial error assessed by the ring width of the trajectory at
different centring in the plane differs by 0.24 [micro]m to 0.44
[micro]m.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (4)
[FIGURE 2 OMITTED]
Characteristic feature of hydrodynamic bearings is trajectory of
the spindle approximately near to circular, its angular velocity being
twice smaller than velocity of the spindle itself. It can be expressed
as [e.sub.1] = [e.sub.10], [[omega].sub.1] = 0.5 [[omega].sub.2].
In this case the form and orientation of the centre trajectory of
the roundness standard depends essentially on the value of eccentricity
[e.sub.2] and its orientation (angle [[psi].sub.0]). Also, the diagram
of trajectory repeats every two revolutions of the spindle. If
[[omega].sub.1] [not equal to] 0,5 [[omega].sub.2], or is approximately
equal, then the trajectory will rotate around the centre of the spindle
and will not repeat at every two revolutions. Despite of small errors
due to not coinciding of the measurement direction with the required and
of the influence of the roundness standard's displacements in the
directions of axis movement to the displacements into the other
directions, the readings [D.sub.x] and [D.sub.y] in the direction of
ordinate axis X and Y are expressed by the equations
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (5)
where [k.sub.x], [k.sub.y] are coefficients of amplification of
measuring signals for x and y respectively, [delta]x, [[delta].sub.y]
are roundness deviations of the cross-section of the roundness standard
in the measuring plane in X and Y axis respectively.
By inserting the values x and y from the Eq. (1) into the Eq. (5) a
member consisting from two harmonic oscillations appears. Frequency of
the one is of the other (i+1). Amplitudes of both oscillations are equal
to [A.sub.i]/2. This value of method's error except of harmonic
constituent equal to the frequency of revolution depends on
[[beta].sub.0] and [[zeta].sub.0i].
For example, in case of aerostatic bearing, when i = 2 and
[[omega].sub.1] = [[omega].sub.2] = const, frequency of the one
oscillation is equal to the frequency of spindle rotation
[[omega].sub.2], and of the other is three times more. Amplitudes of
both frequencies are equal to [A.sub.2]/2. The frequency [[omega].sub.2]
is eliminated from the results of measurement as coinciding with the
eccentricity. The next frequency will be assessed as radial error of the
spindle rotation having the frequency [[omega].sub.3] that does not
exist as it is an error of the method.
Method, when a pick-up of small displacements is fixed to the
spindle to be calibrated. By using this method the tip of the pick-up
contacts the surface of the roundness standard that is mounted to the
unmovable body via centring device. Relative radial displacements of the
surface of the roundness standard and the spindle axis trajectory are
measured in the measuring plane. The radial errors of rotation are
assessed according to the readings of these measurements.
[FIGURE 3 OMITTED]
As in the case of using the first method, this time also is
impossible an ideal centring and always remains an eccentricity between
the spindle axis of rotation and the roundness standard of unknown value
and direction in the measuring plane.
According to the measuring diagram according this method shown in
Fig. 3, applying several simplifications and mathematical rearrangement,
displacement of the measuring tip of the pick-up in the perpendicular
direction to the axis of the spindle will be expressed by the equation
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (6)
where [[gamma].sub.0] is angle between the positive coordinate axis
X and the direction of measurement at initial position of the spindle;
[[epsilon].sub.0] is angle between the positive coordinate axis X and
the eccentricity [[epsilon].sub.3] of the roundness standard at initial
position of the spindle. Other designations are the same as in Fig. 1.
In this case of measurement of radial error, its phase and
amplitude of the graph completed by the readings of the measurement
depend on the angle between the radius [e.sub.1] and measuring direction
at initial position of the spindle.
Recording the results of measurement in polar coordinate system
occur additional errors of eccentricity of the graph that depend on mean
radius of the graph, eccentricity of the roundness standard, angles
[[beta].sub.0], [[gamma].sub.0], [[epsilon].sub.0].
3. Assessment of radial error of rotation by centrodes
Objective assessment of radial errors requires elimination of the
uncontrollable parameters that make influence on the results of
measurement. Centrodes can be used for this purpose as they
unambiguously determine a movement of flat figure.
The displacement of the centre of cross-section of the roundness
standard in the measuring plane perpendicular to the axis rotation
[X.sub.O1] of the spindle, without evaluation of the influence of small
axial displacements of the spindle, can be determined by rotation of
mobile centrode along the fixed centrode and rigidly connected to the
spindle.
Coordinates of the moment centre P of velocities in nonmobile plane
are described by the equations
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (7)
where [x.sub.O1], [y.sub.O1 are coordinates of centre [O.sub.1],
[[omega].sub.2] are angular velocity of rotation of flat figure.
XOY is not mobile coordinate system the beginning of which O
coincides with the centre of the body of the spindle; X'O,Y'
is mobile coordinate system the beginning of which [O.sub.1] coincides
with the centre of the first roundness standard. Coordinate axis
[X.sub.1] is directed across the centre of the second roundness standard
[O.sub.2]; P is moment velocity centre; [[phi].sub.0] is angle between
the not mobile X and mobile X', coordinate axis at the initial
time; 1x, 1y and 2x are the directions of measurement of radial
displacement of the roundness standard.
As angular velocity of the figure is undetermined, there are three
unknown variables [x.sub.p], [y.sub.p] and [[omega].sub.2] in two Eq.
(7). For solving the third equation with the same variables is needed.
The third equation can be formed by measuring the movement of one
more point [O.sub.2] connected with the spindle (Fig. 4)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (8)
where [x.sub.O2], [y.sub.O2] are coordinates of centre [O.sub.2] in
the system of not mobile coordinate system.
[FIGURE 4 OMITTED]
During flat displacement of the figure, velocities of its two
points [O.sub.1] and [O.sub.2] are connected by the dependence
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (9)
where [e.sub.4] = [O.sub.1][O.sub.2].
Then projection of the velocities into the axis Y can be determined
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (10)
where [MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] is angle
of rotation of the spindle, mobile coordinate system's angle of
rotation; [[phi].sub.0] is angle between the non mobile X and mobile
X', coordinate axis at initial moment.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII]
By assessing Eq. (10) from (7) and (8) Eqs., the system of three
equation can be formed with three variables
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (11)
By solving this equation the coordinates of non-mobile centrode are
determined in the non-mobile coordinate system and variable angular
velocity of the spindle
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (12)
Coordinates of instantaneous velocities centre P and nonmobile
centrode graph are not dependant on the selection of points [O.sub.1]
and [O.sub.2] and also from their position according to the axis of the
spindle. They unambiguously determine the displacement of flat figure in
respect of non-mobile elements of the spindle.
The position of the point under measurement in accordance to the
spindle is determined by using mobile centrode that determines geometric
position of instantaneous centres of velocity in the moving body. Its
coordinates in the mobile system of coordinates X'[O.sub.1] Y'
can be written
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (13)
The graph of mobile centrode also depends only on the displacement
of flat figure and does not depend on chosen centres [O.sub.1] and
[O.sub.2]. If exact distance between the centres [O.sub.1] and [O.sub.2]
angle [[phi].sub.0] between the axis X and line [O.sub.1] [O.sub.2] by a
single measurement the data is received for the calculation of nonmobile
coordinates [x.sub.P], [y.sub.P] of centrode and mobile coordinates of
centrode [x'.sub.p], [y'.sub.P] and for angular velocity
[[omega].sub.2] of the spindle. When this is known, unambiguous
determination of the coordinates of every point P in the non-mobile
coordinate system
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (14)
The method proposed can be accomplished by using the roundness
standard with three reference cylindrical surfaces.
Two cylindrical reference surfaces are concentric and the surface
in the middle is concentric to those (Fig. 5). The value of
eccentricities [O.sub.1] [O.sub.2] is determined by measurements. Such
standard of roundness is fixed to the spindle to be calibrated via the
centring devise. Displacements in the coordinate directions X and Y of
the middle cylindrical surface are measured by two measuring systems
mounted on sturdy pedestal on two perpendicular directions 1x ir 1y.
Using the third measuring system 2x the displacement of other two
cylindrical surfaces are measured in the direction of X axis.
Capacitance transducers with the cylindrical surface are used for
measurement of the displacement of reference cylindrical surfaces. Such
transducers eliminate the influence of form errors of the roundness
standard on the measurement result. Three surfaces are used for the
purpose of elimination of calibration errors occurring by angular biases
of the spindle during its rotation.
[FIGURE 5 OMITTED]
4. Conclusions
1. Various methods of measurement of radial errors of the precision
spindles using the roundness standard give different results of
measurement of the same measurement due to uncontrollable values.
2. The trajectory of the centre of roundness standard used for the
measurement of radial errors of the spindle depends on radial error of
the spindle's axis trajectory in the measuring plane and on its
value and direction of eccentricity in respect of the spindle axis.
3. Function and value of radial error measurement depend on the
uncontrollable errors of centring and on the direction of measurement
during the calibration.
4. The trajectory of the spindle is evaluated unambiguously
according to the centrodes.
5. The centrodes can be calculated in the measuring plane according
to the displacement of two eccentrically situated roundness standards in
the same plane.
6. The trajectory of every point connected with the spindle can be
determined unambiguously and the metrological or technological errors
according to the analysis of measuring results can be determined using
centrodes for the calculation.
Acknowledgments
Publication is prepared based on information received by
implementing project "Creation of the absolute, high resolution,
precision angular encoder with capabilities of self diagnostics"
which is supported by EU structural funds and Republic of Lithuania.
(project Nr. VP2-1.3-UM-02-K-03-025).
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Received April 05, 2011
Accepted June 29, 2012
A. Kasparaitis, Vilnius Gediminas Technical University, Sauletekio
al. 11, 10223 Vilnius, Lithuania,
E-mail: a.kasparaitist@precizika.lt
V. Giniotis, Vilnius Gediminas Technical University, Sauletekio al.
11, 10223 Vilnius, Lithuania
cross ref http://dx.doi.org/10.5755/j01.mech.18.4.2335