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Lehigh UniversityLehigh Preserve
Theses and Dissertations
1984
A study of fluid flow in screen process printingShiaw-Min ChenLehigh University
Follow this and additional works at: https://preserve.lehigh.edu/etd
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Recommended CitationChen, Shiaw-Min, "A study of fluid flow in screen process printing" (1984). Theses and Dissertations. 5163.https://preserve.lehigh.edu/etd/5163
A STUDY OF FLUID FLOW
IN SCREEN PROCESS PRINTING
by
Shi aw-Min Chen·
A Thesis
Present in Partial Fulfillment
of the Requirement for the Degree of
Master of Science
in
Chemical Engineering
Lehigh University
1984
ACKNOWLEDGEMENT
The author expresses his sincere appreciation to Professor
A. C. Zettlemoyer for his many helpful criticisms and inspiring dis
cussions on the research project. Many thanks are due· to Professor
F. J. Micale for suggesting this project and for his many contribu
tions as supervisor of this research.
Most of all, the author wishes to ·thank the M. Lowenstein Corp.
for their financial support this study, without which this work
would not have ·been possible.
Also, the author would like to thank the Lehigh University Com
puting Center for their facilities and helps.
Acknowledgements are also given to Dr. K. Chaing, Dr. J •. L. Lin
and Dr. S. Kiatkamjornwong who offerred a number of very helpful
suggestions.
The author also wishes to express his appreciation to Ms.
J. Lavelle for her help in -this study.
Finally, the greatest appreciation must be given to my parents,
Mr. and Mrs. J. N. Chen, for their constant enc~uragement at all
times.
11
CERTIFICATE OF APPROVAL
This thesis is accepted and approved in partial fulfillment of
the requirements for the degree of Master of Science in Chemical En-
gineering.
Date
~t;r~ Professor in Charge
/f_.c.~~ Dr~.Tz:ttl~er
Professor in Charge
r#£? c. c/~ Dr. J. C. Chen
Chairman Department of Chemical ·Engineering
iii
/ \
\
Table or Contents
ACKNOWLEDGF.MENT Abstract
CHAPTER· I Introduction 1.1 Approach to the problem
CHAPTER II Mathematical modelling 2. 1 Introduction 2.2 Region !--flow pattern in the ink bank 2.3 Region II --Flow in the screen holes 2.4 Summary of Region I and Region II 2.5 Limitation
2.5.1 Limitation in Region I "_2.s.1.1 The creeping flow
2 -~ 5 .1 • 2 The singular poi~ t 2.5.2 -Limitation in Region II
2.5.2.1 A long tube 2.5.2.2 Steady state
CHAPTER III Rheology or the ink 3.1 Viscosity of test inks 3.2 Rheology of test inks
CHAPTER IV Results and discussion 4.1 Criteria for calculations 4.2 Rate of deformation
4.2.1 Rate of shear 4.2.2 Rate of normal strain
4.3 Pressure drop build up by ink flow in region I 4.4 The flow rate through the screen 4.5 Volume ·of ink delivered
CHAPTER V Conclusions and future work 5.1 conclutions 5.2 Future research references Appendex A Appendex B
iv
ii
1
2 3 4 4 5
15 16 18 18 18 19 20 20 21 22 22 31 39 39 40 41 41 46 59 55 63 63 64 65 67
71
Figure 2-1: Figure 2-2: Figure 2-3:
Figure 2-4:
Figure 3-1:
Figure 3-2:
Figure 3-3:
Figure 3-4:
Figure 3-5:
Figure 3-6:
Figure 3-'.7:
Figure 3-8: Figure 3-9: Figure 4-1:
Figure 4-2:.
Figure 4-3:
Figure 4~4:
Figure 4-5:
Figure 4-6 :_
Figure 4-7:
Figure 4-8:
List or Figures
Schematic model of rotary screen printer. 4 Simplified model of the ink bank. 6
Schematic or blade and screen where the fluid 9 may move from the ink bank through the holes of the moving screen. Flow in a long cylindrical tube where R is the 15 radius of the tube, Lis the length of the tube.
Apparent viscosity as a function of RPM for six 24 test inks on the Brookfield Viscometer.
Pseudo-stress as a function of RPM for six test 25 inks on the Brookfield Viscometer.
Apparent viscosity as a function of shear rate 26 for six test inks on the Band Viscometer. Shear stress as a function of shear rate for six 27
test inks on the Band Viscometer. Apparent viscosity as a function of shear rate 28
for inks and clears on the Weissenburg Viscometer.
shear stress as a function of shear rate for 29 inks and clears on the Weissenburg Viscometer.
Log viscosity as a function of· log shear rate 32 (replot from Fig. 3-5) A fully developed fluid flow in a circul~ tube. 35 Shear stress distribution in the circular tube. 36
a, b, c Shear rate as a function of r, 80
and U, 42 calculated from eq.2-17(c). a, b and c., Rate of normal strain as a function 44
of r, 80 and U, calculated from. eq. 2-17(b). a, b, c, d and e, The pressure drop build up in ~7;
the ink bank acting on the screen as a function of m, n, r, 8~ and U.
a and b, The pressure drop exerting a lifting 51 force on the squeegee as a function of 8
0 and U;
a, b, c; d and e, The flow rate through a single 52 hole in the screen as a function· of R, n, 8
0, r
and u. · a, b and c, Volume ot ink delivered as a function· 56 of R, n, and 8
0•
Volume of ink delivered as a function of upper 61 limit of integration, RU. Volume of ink delivered as a function of lower 62 limit of integration, RL.
V
Table 3-1: Table 3-2:
List of Tables
Formulation of the test inks Constant m and n calculated from Figure 3-7
........
vi
23 33
I.
Abstr:-act
A mathematical model of screen process printing to predict the
hydraulic pressure and the volume of ink delivered through the
screen was developed. The model deals with both fluid dynamics of
the screen process and the rheological properties of the printing
inks.
Calculations from this mathematical model agre~ qualitatively
with the published experimental data in terms · of hydraulic pressure
build-up and volume of ink transferred with respect to squeegee
angle and speed of the moving screen.
..
CHAPTER I
Introduction
The screen process printing, for a variety of applications,
date! bapk many years and is ·older than conventional printing .it-
self. Since the advent of the screen process printing, which
brought forth the capability of producing large volumes of printe~
material at relatively low cost, screen process printing had been
used primarily for low volume, high cost application. It is only in
more rece.nt times that screen process printing has been used for
commercial. operations, and usually on irregular shaped or fll
defined surfaces such as textiles.(1,2]
The challenge for screen process printing in textiles is two
fold: first, to increase the printing speed, and second, to increase
the quality of the printing. The invention of the rotary screen
printer was a major breakthrough for increasing printing speed and . . '
rendering this technique economically feasible for many prin~~g ap-
plications. Work has also progres~ed on the materials used for· the
screen and on method~ for preparing the holes for imaging. Toe
results of these advances for textile printing applications have
been improved image quality and line definition, and reduced costs
which have led to an expaned volume of screen printing.(3,4,5,6,7]
Al though many advances have been made in terms of the mechanics
2
of rotary screen printing and _quality of the screen, very little
work has been accomplished in terms of refining the process vari
ables from knowledge of the mechanisms involved in the process. [ 8]
So, the objective .of this work is to study a model of the screen
process printing.
1.1 Approach to the problem
The fundamental mechanism of screen process printing is that a
stencil bearing an image or. a design is attached to a screen. When
stock is placed directly und.er the screen, process ink is forced
through the open mesh the image area of the screen, with a squeegee
allowing, thus, the ink penetrates through to the stock. In other
words, screen process printing involves the principle of actually
printing through a plate.[1l
Based on this fundamental mechanism, a mathematical model is
presented in Chapter 2, and the results of this mathematical model
are presented in Chapter 4, along with a comparism of the.model with
wxperimental results published in 11 terature.
Chapter 3 includes a preliminary study of the rheologiqal
properties of the process inks, which is necessary in order to es
tablish the relationship among the printing variables as establis_hed
in the modelling.
3
\
2. 1 Introduction
CHAPTER II
Mathematical modelling
A schematic presentat~on of the rotary screen printer is shown
in Figure 2-1.
Roller Bar
Textile
Figure 2-1: Schematic model of rotary screen printer
Some applications utilize a blade in place of the roller bar. The
pressure of the roller bar, or blade, on the screen cylinder is con
trolled by an electro-magnetic bar under the substrate.
The flow pattern in this process contains three different
regions which are Region I, U~e ink bank contained between the
roller bar and the screen cylinder; Region II, the ink "flow through
the holes on the screen cylinder; Region III, the ink absorbed by
4
the substrate. The Reg~on III is being eliminated from this modell
ing because of the complexity of the forces involved in the
mechanism of absorption on the substrate. The model will be based
on Region I and Region II only. Assuming that no fprce exists
beyond Region II, which means that once the ink passes through the
screen cylinder, there are no effects due to surface tension, capil
lary force or graviational force.
2.2 Region !--flow pattern in the ink bank
Region I, represented in Figure 2-2, has been ~implified due to
the complicated nature of the mathematics. Figure 2-2 illustrates
the stationary blade, represented as the roller bar, and the moving
plate, represented as the screen cylinder without holes, which moves
with the· velocity of U in the direction opposite to th~ direction. of
r.
The· ink bank is further assumed to be· infini tly long in the Z
direction, i.e. there is no edge effect, which reduces this system
into a two dimensional problem. Also, it is assumed that the ink is
a newtonian, incompressible fluid. A c_or.rection f~r a generalized
newtonian fluid will be discussed later. Therefore, ~e problem
fits the criteria for the stream function as expressed .in Equation
(2.1).(9,.10]
:-. 1 ~('\/21/J)+-ch r
a<I/J , '\J 2"')
<Y( r, OJ
5
( 2.1)
where
plate
r is the distance from the point of contact of the blade with the plate.
80 is the angle.of the blade with the plate.
9 is the angle measured from the plate.
Figure 2-2: Simplified model of the ink bank.
where 1/1 is the stream function defined by F.quation, (.2 .2) and
(2.3).
(2.2)
and
6
and
'v 2 is Laplace oper~ tor
v is kinematic viscosity, and
t is time.
Vr, v8 are velocity in r, 80
direction, respectively.
ac "', 'v 2
1/1 >
fY ( r, 8 ) is the Jacob operator.
(2.3)
The first term on the left hand side in Eq~ation (2.1) represents
the time d·ependency of the stream ·runction. And, the second term on
the leftr.hand side represents. the inertia force of the fluid.
For further simpUfication, the following assumptions are made:
1. steady st·ate, and
2. creeping flow.
If a steady state is assumed, the first term in Equation
( 2 .1) cancels. If creeping flow is assumed, the second term
represents the· inertia force whic.h becomes very small. Therefore,
F.quation (2.1) is reduced to Equation (2.4).(11]
7·
'v 4 t/J'= 0.
The boundary conditions are:
Vr(r,8=0) = - u
V8(r,8:0) = 0
Vr(r,9:80
) = 0
v8(r,8=80 ) = 0
By solving Equations (2.2), (2.3) and (2.4) (see appendex A) we
get the stream funoUon and the velocity profile in the ink bank can
be expressed by Equations (2.5), (2.6) and (2.7), respectively.
"' =
(2.5)
where A is an integration constant.
u Vr = - 2 2 . ·[ ( sin( 90 ) cos( 80 ) - 80 80- sin (80 )
+ 9 sin2(80 )) sin(9) + ( 9~ ~ sin2(80 } + sin(80
) cos(90
)
+ sin{ 80 ) cos( 80 ) - 8 80 ) cos( 9)], (2.6)
8
u v9 = [ 00
2 sin(9) - e sin2(e0
) cos(e) 92
- sin2 (8) 0 0
(2. 7)
In the next step, replace the plate in Figure 2-2 with a screen
plate as shown in Figure 2-3.
Figure 2-3:.
Schematic of blade and screen
where the fluid may move from the ink bank
through the holes of the moving screen.
Once the holes in the screen are parti.ally depleted as the ink
is printed, the layer of ink immediately above the plate flows in a
9
r
manner to refill the holes. Consequently, the velocity .of this ink
layer is no longer the same as the velocity of the plate. Then, the
boundary conditions change to:
' Vr(r,8:0) = - kU
' . v8(r,8:0) = - 0
' Vr(r,8=80 ) = O
' v8(r ,8=80 ) = 0
Again, solving ·Equations (2.2), (2.3) and (2.4) by using these new
boundary condi .tions yields the new stream function, 1/1' , velocity
profile, v; and V~ , as in Equations (2.8), (2.9) and (2.10).
k r U ,/,
1 = [( a
02 + 8 sin(8
0) cos(8
0)
'¥ 8~ - sin2(80
)
( 2. 8)
k u 2 2 · [( sin(9
0) cos(8
0) - 9
0 8 - sin ( 8 ) 0 0
(2. 9)
10
' Vg = k u
2 2 I 8~ sin(8) - 9·sin2(80
) cos(8) 80 - sin (8
0)
(2.10)
In reality, the flow rate of the ink through a single hole on
the screen is very small so that 'the proportionality constant, k, is
very close to one. Therefore, Equ~tion (2.8), (2.9) and (2.10) ar.e
approxima.tely equal to Equatiqns (2.5), (2.6) and (2.7), respec
tively.
The most. interesting parameter in Regi~n I is the normal pres
sure distribution along the plate, which is generated by the ink
flow in the ink bank.
The total stress tensor, or pressure tensor, is defined in
Equation (2.11) ~[ 12]
!J = ! + 6 p =· (2.11)
where
!J is total stress tensor , or pressure tensor.
T is stress tensor. =·
d is unit tensor.
P is the surrounding pressure.
11
If one considers the ink bank, the only surrounding fore~. ac
ting on the system is the atmospheric pressure. Therefore, Equation
( 2. 11) can be simplified to Equa ~ion ( 2. 12) •
fl"=T+6P, = = = a
where Pa.is atmospheric pressure.
The stress built up by the flow, 1. e. the pressure drop, or dif
ference between surrounding pressure and the pressure in the system
in Region I can be discribed by Equation (2.13),
n= T • ( 2. 13)
The· stress tensor is def_ined in Equation ( 2 .14). [ 13]
! = T/a y • (2.14)
where
~a is apparent viscosity.
Y is rate of deformation tensor. =
The rate of strain tensor is defined in Equation ( 2 .15) •
12
(2.15)
where
is "del" c;,pera tor .•
is velocity vector.
is transpose of ('\7 V).
The rate of strain tensor can be ~xpressed by Equation ( 2. 16) ,
(2.17) and (2.18).
Yrr ryVr
= 2-' ~r
Yee 1 ave vr
) , = 2-(-+-r as r
'Yre . ~ ( ~.) 1 avr
= Yer= r °a + -·--. r r r a 9
where
Yrr· is the normal rate of strain in r direction.
Yee is the normal rate of strain in 9 direction.
'Yre is the shear ra.te.
(2.16)
(2.17)
(2.18)
By substituting for Vr and v8 in Equation (2.16) to·(.2.18), Equation
(2.19), (2.20) and (2.21) is obtained.
Yrr = a, (2.19)
(2.20)
13
• Vg Yre = - -;- (2.21)
The. stress tensor built up by Region I is defined by Equation
( 2 • 2 2) , ( 2 • 2 3) and ( 2 ~ 2 4 ) •
flee= ( 2 ( ave + V )) a r ae r
llre = a< V9 f c3Vr -+--) r r ae
where
flrr
flee
is the normal stress in r direction.
is the normal stress in 9 direction, also called Pr in this case.
fl re is the shear stress.
(2.22)
(2.23)
(2.24)
The only pressure which is exerted normally to the ~creen plate
is .D.Pr and is expressed by Equation (2.25).
where .D.P1 is the pressure drop which is exerted normal to the screen plate and which is generated by the flow in the Region.I.
14
(2.25)
2.3 Region II --Flow in the screen boles
Consider a single screen hole as a cylindrical tube as shown in
Figure 2-4.
·I
L R
I I
I
f
Figure 2-4: Flow· in a long cylindrical tube
where· R is the radius of the tube,
Lis the length of the tube.
Assuma.._1h~ink in the tube is a newtoniari fluid, and the ink
flow is well developed, so there is no edge effect. Then, by Hagen
Poiseuille law, the volume flow rate is expressed by Equation
(2.26) and (2.27).(14]
. 4 ~PIIR
Q = ----8 L T/ a
,. (2.26)
15
\/
where
Q is the volume flow rate.
~P11 is the pressure/'reqUired to produce flow at a flow rate of Qin this tube.
A is the internal area of the tube.
2.4 Summary of Region I and Region II
(2.27)
Because effects of. Region Ill are not been considered, so,
there is no additional _force applied to this system. Therefore, the
pressure. drop /Uired in Region II to produce ink flow must be
equal to the pressure drop created in Region I, as expressed by
Equation (.2.28).
Therefore ·the .6PII term in Equati (2.26) is replaced by ~PI" as
defined in Equation (2.25), then the ow rate in the tube is dis-
cribed by Equation (2.29). \
A2 2 oV8 Q = - ( C - + vr )) , 8 L r O 8
(2.29)
16
Aocording to Equation (2.29) the flow rate in the tube is not a
function of the viscosity of the. ink. The equatj.on is applicable,
if the ink is a newtonian fluid, but, in most cases, the ink is a
non-newtonian fluid .• [7, 15] Therefore, the effective visco~ity for a
particular ink will vary from Region I to Region II because rate of
shear applied in each region· is differe~t. To compensate for this,
two terms designated as rJ aI and T?arI are inserted in Equations
(2.29) to yiel~ Equation (2.30).
A2 T/ar 2 (YV9 . Q=--(-(-+V))
8 L T] a II r (Y 9 r (2.30)
(
The volume of the ink transferred through a single hole can be
expressed ~Y Eq ua ti on ( 2. 31) •
V = J Q dt
where
V is the volume. of ink transfer.red through a single hole.
t is the 'time a single hole travels during. ink transfer through the hole.
Substituting dr/U for dt in Equation (2.31) yields Equation
(2.32) which discribes the volume of ink transfer.
17
The calculation can be d.one at this point, that once the
rheological properties of the ink and the operating parameters of
the syst-em are provided, then, th.e volume of ink transferred as well
as the flow rate in a single hole and the hydrodynamic pressure drop
can be calculated· by Equations (2.25}, (2.30) and (2.32).
(_-) -"
2.5 Limitation
2.5.1 Limitation in Region I
2.5.1.1 The creeping flow
In Region I, the assumption. of creeping flow was made for the
purpose of simplification. However, this assumptiom restricts the
application of this model to a small region. )
Since the flow is creeping flow, then, the Reynold's number
must be very small. [ H, 12] By defirii tion, Reynold's number is ex
pressed by Equation ~2.33).
pr U R = - ' e 7/a
(2.33)
where
18
Re is the Reynold's number.
Consequently, in order for Re to remain very small, the limitation
for r in F.quation (2.33) is expressed in (2.34).
r « V -u (2.34)
where is kinematic viscosity.
In conclusion, this model is valid only when r .is much smaller
then the ratio of the kinematic viscosity to the screen velocity.
2.s.1.2 The singular point
If one considers the extreme case that if r approaches zero in
Region I, it is very obvious that there are two different boundary
conditions which apply to this single point such as:
Vr(r=8, 8=0) = - U,
and
Obviously, in the neighborh9od of r equal to zero, this model is
divergent.
19
2.5.2 Limitation in Region II
2.s.2.1 A long tube
The Hagen-Poiseuille law applies only if the edge effect is
negligible which is accomplished by assuming that the ink is. new
tonian and ink flow is well developed.
An energy loss due to the edge effect can be caused by a sudden
contraction at a entrance to a pipe line. This energy loss is less
for a laminar flow than for turbulent flow.[16)
Actually, an entrance length of a tube must be in the order of
where Le is entrance.length.[16)
in order to produce the characteristic parabolic velocity profiles.
Eisenstadt and Kline et.aL, suggested that in order to main
tain Poiseuille-flow the dimension must be:
L --> 1
In addition, for a rounded entrance and for laminar flow, the
entrance loss is negligible.
20
2.5.2.2 Steady state
The Hagen-Poiseuille .law is based on steady state flow However,
examination of Equation (2.30), reveals that the flow rate of the
ink varies with a change in r. This means that during a s.ingle pass
of the .holes through the ink bank, the flow rate of ink through the
screen is not constant, and therefore, it is not steady state.
J
..
21
\
,,.---
CHAPTER III
Rheology of the ink
Al though, it was assumed in the theoretical approac~, that the
ink is a newtonian fluid in reality, most inks exhibit non-newtonian
behavior. [ 7, 15]
3. 1 Viscosity of test inks
As shown in Table 3-1, a series of test inks were formulated
for investigation as ·model inks where, in one set., the pig~ent
remained constant and the binder system was systematically changed,
to produce inks 1, 3, 5 and .6. In another set, the pigment was sys
tematically changed, while attempting to maintain the same shade of
blue, and the binder remained constant producing inks 1, 2· and 4.
The viscosity of the test inks were measured on the Brookfield
Model LV Viscometer with a 114 spindle, Band Viscometer, and the
Weissenburg Viscometer witn a cone and plate configuration. The
results on the Brookfield Viscometer are presented in Figures 3-i in
which apparent viscosity is plotted as a function of spindle speed
and in 3-2 illustrating apparent viscosity times RPM, i.e. a pseudo
stress, as a function of RPM, approximating the classical plot of
stress versus rate of shear.
Figures 3-3 and 3-4 repr·"sent the results from the Band Vis
cometer illustrating apparent vi~cosi ty· and shear stress, respec-
22
Table 3-1:
Formulation of the test inks
1 2 3 4 5 . 6 Blue 3G 80.0 54.0 80.0 82.5 80.0 80.0 Valet 4BN 50.0 50.0 50.0 50.0
9.0 4.0 9 .. 0 5.0 9·.0 9.0 27.0
Orange C
Scarlet FDLN 24.0. 282C Clear 661.0 715.0 688.~
200.0 200.0 200.0 200.0
661.0 70-SE Clear 661.0 Binder TP989 200."0 200.0
661.0
tively, as a function of the shear rate.
The results from Weissenburg Viscometer are shown in Figures
3-5 and 3-6 in which apparent viscosity and shear stress, respec
tively, are plotted as a function of shear rate for six .inks and
clears, i.e. the unpigmented portion of the ink.
Comparison of these results indicate that the Brookfield Vis
cometer is measuring the viscosity only at low rates of shear as
evidenced by th~ very slow spindle speeds and the corresponding high
23
40
,..., 32 Cl)
1/)
0 a. ._,
(\J
0 24 .-X
>--+'
1/)
0 l 6 (.)
1/)
>
8
0 0 3 6
RPM
Figure 3-1:
9 12
Apparent viscosity as a function of RPM
for six test inks on the Brookfield Viscometer.
24
0
0
I::,.
'iJ
<> lS1
l.NK 1
1 N-K 2 1NK 3 1NK 4 1NK 5 ]NK 6
so
'""' 40 :r: CL
0:: 'lJ
1/)
0
0. 30 ....,
(\J
0 .-
X
L 20 0... a:::
X
(.)
1/)
1 0 >
0
••' ·~'' '~---'Y", . .-,,~·• - • ,.._.r•, ..... ....,- -_,.• __ .• ·••·• -··-. ~ ,
0 3 6
RPM·
Figure 3-2:
9
Pseudo-stress as a function of RPM
1 2
for six test inks on the Brookfield Viscometer.
25
D INK 1 0 INK 2 6 INK 3 \J· lNK 4 O· lNK S lSI ·1 NK 6
1 0
D INK 8 0 INK
.!J. INK 'v INK ·O lNK
6 1SI 1NK
4
2
0 0 2500 soon 7500 10000
Shear Rate (sec- 1).
Figure 3-3:
Apparent viscosity as a function of shear r:-ate for six test inks
on the Band Viscometer.
26
1
2
3
4 5
6
,-...
(\J
E l)
' C >,
-0 ._,
If)
(/)
V
'--+'
U)
'-(0
\)
..c U)
8600
7200
5800
4400
3000 0 2500 5000 ?500
Sh c a r Ra t e ( s e ·c - l )
Figure 3-4:
0
0
6
V
<> 1S1
10000
Shear stress as a function of shear rate for six test inks
on the Ba.nd Viscometer.
27
lNK 1
1NK 2 1NK 3 1NK 4 1 NK .5 lNK 6
. ,-..,
Cl.)
IJ)
0 a..
-.J
>-......
IJ)
0 (.)
IJ)
>
so
40
30
20
10
0 0
0 1NK 1 0 lNK 2 ~ INK 3 "v lNK 4 0 1NK 5 ISl JNK 6 Q) NT4A ~ 282C w 70SE1
250 500 750
Sh e a r Ra t e ( s e c - l ) ·/
Figure 3-5:
1000
Apparent viscosity as a function of shear rate for
inks and clears on the.Weissenburg Viscometer.
28
7500
6000
........ (\J
E c..)
'-C 4500 ;:,,,.
-0 ......, If)
If)
V
'--+"' 3000 U)
'-(0
V
...c U)
1500
0 0 1500 3000 4500 6000
Shear Rate (s·ec- 1) ,·
Figure 3-6:
shear stress as a function of shear rate for
inks and· clears. on the Weissenburg Viscometer.'
29
D lNK 1 0 INK 2 ~ lNK 3
'7 INK 4 () INK s ISi INK 6 Q) NT4A & 282C w 7 OS"E 1
apparent viscosity values, Th.e Band Viscometer is capable of
measuring viscosity only at relatively high rates of shear.
However, the Weissenburg Viscometer is capable of taking measure
ments over both lower and higher rates of .shear range.
There is a lack of agreement in the results from the Band Vis
cometer and Weissenburg Viscometer which may be related to the in
complete wetting of the mylar film on the Band Viscometer by these
essentially water based inks~ These results suggest that the .Band
Viscometer is not the best instrument for measuring these test inks
which vary as to their ability to wet the mylar film which fn turn
would significantly effect the rheological measurements.
The results from the Brookfield Viscosity are inadequate for
complete rheologi~al charaterizat1011 of the inks because the rate of
shear is not well defined. However, this instrument is very easy to
operate and is capable of differentiating the inks based on their
relative apparent viscosity in -terms of RPM.
These results indicate that the _most c~mprehensive and reliable
viscosity measurement are obtained with the Weissenburg Viscometer.
It should be mentioned, however, that the measurements are t.i,me con
suming particularly at.lower rates of shear.
J.
30
3,2 Rheology ot test inks
Plotting the apparent viscosity data from the Weissenburg Vis
cometer on a log-log scale. as shown in Figure 3-7 illustrates that
the apparent viscosity of the inks decreases linearly as the shear
rate is increased. This relationship ~uggests that the rheological
properties of the inks can be described by the Ostwald-deWaele power
law which is defined by equation (3.1) .[ 17]
where
T is the shear stress.
t is the shear rate.
The constant m, with dimension of N sn
M2 constant n are characteristic of each fluid.
(3.1)
and the dimensionless
While n equal to one,
then, mis apparent viscosity and is newtonian fluid.
Since a generalized newtonian fluid is defined by equation
(3.2).
T : "a 'Y ,_
where "a is apparent viscosity.
So, the apparent viscosity for the power law defined in equation
31
D lNK 1 0 1NK 2
1 02 ~ lNK 3
,....._ 'v 1NK 4 (l.l
0 lNK 5 11)
0 ISi 1 NK. 6 a.
(D NT4A .....,
>- l O 1 £ 282C -t-'
11) w 70SE1 0 (.)
11)
>
1 OO
1 0 - l ----.............. -~~...u.----..J..--+~UJ.:IJ-J.-.J..-1...J..UJJ.I
10° 10 1 1 o3 10 4
Shear Rate (sec-1).
Figure 3-7:
Log viscosity as a function of log she~r rate (replot from Fig. 3-5)
32
(3.1) is:
· n-1 '1a = m >' , (3.3)
or
log 17 a = log m + ( n-1) log >' (3.4)
Thus, the constant (n-1) and ( log m) represent as slope and inter
cept, respectively,in equation (3.4).
The constant m and n are calculated from Figure 3-7 and i.s
shown in Table 3-2.
Table 3-2:
Constant m and n calculated from Figure 3-7
Sample No
rn
n
Inks
1 2 3 4 5 6
379 513 423 402 247 151
0;2a4 0.23a 0~311 o.306 0.301 o;3aa
Clears
282C NT4A 70-:-SE
92 186 214
· 0. 384 0. 381 0. 302
Substitute equation (3.3) and (2.21) into equation (2.25),
then, the pressure .drop build up in region I is calculated by equa
tion (3.5).
33
V 1 av n-1 2· av = m (- ...:.i + - ---!'.:..) (- (---.i. + V ))
r r <Y e r .a e r (3.5)
Also, by the same substitution to equation (2.JO), the flow
rate in region II may be calculated by equation (3.6).
A2 1 V 1 oV n-1 Q = - - (- ~ + - ---!'.:..)
8 L TJ all r r () 8
( ~ ( ()V9 + V )) ,. r CY 9 r
( 3. 6)
But, in equation (3.6), the viscosity in region II, >'n , is still
not known because the shear rate.in region II has not been defined.
In order to determine the shear _rate in region II, consider a
circular tube as shown in· Figure 3-8.
A momentum balance over this tube is described by equation
(3.7).
d 'r'z dr'
where
~p = (-) L .
r I ,
, r, z i_s shear stress.
~P is pressure drop over the tube.
34
( 3. 7)
where
L
I
J.
r' and z are cylindrical coordinates.
R is the radius of the tube.
Lis the length of the tube.
Figure 3-8:
A fully. developed fluid flow in a circular tube.
solving the differential eqation (3.7) for shear stress yields equa
tion (3.8).
T r'z 6P
= (-) 2 L
r' . , (3". 8)
According to this equation, the shear stress distribution in
this tube can be described by Figure 3-9.
Because the radius of the holes in the screen is very small the
shear stress at any point along the radius may assumed to be a
constant, r 8, as described _by equation (3.9).
35
where
R
T 1 (r' = 0) = Q r z
L__ T ( r' = R) = ...----- r' z
TR is the shear stress at r' equal to R.
Figure 3-9:
Shear stress distribution in t~e circular tube.
T: T r'z
8P = TR = (- ) R ,
2L ( 3.9)
Then, substitute the pressure drop in equation (3~9) by equation
(2.27) and solve for the shear rate in the tube as described in
(3.10).
4Q ?' II =-;jp
where >' II is the rate of shear in region II •.
(3,10)
In equation (3,6), express the value of 7JaII in terms of the
shear rate as ex;pressed in equations (3,3) and (3.10) to obtain the
flow rate defined by equation (3.11).
36
[ 1 A2 ( ave ) Q = --- ae + vr 4 ,rr L
1
(- ..!§ + ~ avr n-1 n
) l r r ae (3. U)
. .
. 4
~
It is noted in equation (3. 11) that the flow rate, Q, is not a
function of the rheological parameter m.
In the next step, consider the values for the. velocity
profiles, Vr and v8 , described in equations (2.6) and (2.7). Ex
tract the the screen velocity ter·m,: U, from the equations and ex
press the remainder a·s fr( 8 ,80
} and f 8( 8 ,80
) which are functions of.
8 and 80 only, as represented in equation (3.12) and (3.13).
(3.12)
(3.13)
Replacing the V r and V 8 in equation ( 3. 11 ) with their cor
responding terms as given iri equation (3.12) and (3.13) yields equa-
tion (3.14) describing the flow rate ·or ink.
37
·~
..
Q = u
1
(
- ~ + -.1 ~ ) n-1 l r r ae . 4
~
n
(3.14)
If in equation (2.32) the Q term is replaced by the description
of Q given in equation (3.14), the volume of ink transferred through
the screen can be expressed by equation (3.15).
V = J [ 1
dr , (3.15)
According to equation (3.15), the volume of ink transf~rred
through the screen is not a function of the speed of the screen.
38
CHAPTER IV
Results and discussion
4.1 Criteria for calculations
In order to test the validity of the ma thema ti.cal model, values
for the pressure drop , .6P, ink flow rate , Q, and volume of ink
transferred through ·the screen , V, were calculated by computer for
comparison with corresponding values reported in the literature.
The independent variables carefully selected for these calculations
are:
r 10-6 to 1.0 cm.
80 5° to 25°.
u 25 to 125 cm/sec.
m 100 to 500 N(s)n/M2.
n 0.2 to LO.
L 0.01 cm.
R 0.002 to 0.01 cm.
The lower limit for distance, r, is arbi trari.ly chosen t.o be
cm. According to the limitations discussed in sectlon 2 .5 .1.2
when r approaches zero this model approaches a singular point. This
means that as r approaches zero all the dependent variables will ap-
proaoh infinity. The lower limit, therefore, cannot be zero. The
upper limit is obtained by setting the · maximum Reynold's number
39
equal to one in Equation 2-26 in section 2.5.1.1, where the cal
culated maximum distance, rmax• is equal to:
V rmax =-
u
According to calculations based on a newtonian ink, r varies · max
from 1 • O cm to 20 cm, and 1 • O cm is assigned as the upper limit. 90
and U are arbitrarily chosen to vary from s0 to 25° and from 25 to
125 cm/s, respectively. Rheological parameters, m and n, are
selected based on the values- obtained from the test inks. Screen
parameters, L and R, are assigned values which meet th~ specifica
tions discussed in section 2.5.2.1. If the Reynold's number is set
equal to one, then .according to Eisenstadt's Equation, the ratio of
L to R must be greater than or equal to one.
4.2 Rate of deformation
The rate of deformation, which is a function of the rate of
shear and the rate of normal strain, is very important in this math-
ematical modelling. The fluid to which the model applies is assumed
to be non-Newtonian or shear thinning, and its effective vfscosi ty
would depend on the rate of shear applied. In addition, the pres-
sure build up in the ink bank, the ink flow rate, and the amount of
ink transfer through the screen are dependent on the rate of nor.ma!
strain.
40
4.2.1 Rate or shear
The rate of shear chosen for the calculations was calculated
based on Equation. 2-17(0), and the data are shown in Figure 4-1.
Figures 4-1 (a) ano (b), which: represents shear rate as a func
tion of r and 80 , respectively, indicates that r and 80
have a
similar relationship to shear rate. As the d~stance, r, or squeegee
angle, 90 , i_ncreases,. the shear rate initially decreases rapidly,
and then gradually starts to level off. Figure 4~1 (c), shows that
the shear rate increases linearly with an increase in screen speed.
It should be noted in Figure 4-1 (a) that the shear rate increases
to very high values for small values of r.
4.2.2 Rate of normal strain
The rate of normal strain is the strain which is operation nor
mally to the moving surface, i.e. screen, and which is responsible
for the pressure normal to that surface. Figure 4-2 represents the
relationship between rate of normal strain and screen process print
ing parameters r, 90 and Figures 4-2(a) and (b), show that the rate
of normal strain decreases with increasing r or 90
•. Ffgure 4-2 (c)
shows that the normal strain decreases linearly with increasing
printing speed u.
41
106
:'105 I 0 Q) a)
U=75cm/s e =5°
0
I I
103 -ti----+-, -------J,......_ __ ....,;._+,---~1
0 0.3 0~6 0.9 1.2
12 t('\ I 0 ..... >< ,....._
"'j 8 0 Q) a) .._,
Q)
+> Ill ~
~ QJ
..c: U)
0
r (cm) (a) Shear rate as a function of distance r.
U=.75cm/s i i
r=1 .Ocm I
I I I
--------2 10 18 26 34
00
(degree) (b) Shear rate as a function of squeegee angle 90.
Figure 4-1: a, b, C
Shear rate as a function of r, 80
and U,
calculated frora eq.2-17(c).
42
10
"' I 0 ... >< 7
-... I 0 4) rn ....... 4) .µ a, 4 s.. s.. a, (1l
..c: en
0
9 •5° 0
r=1 • 'Jcm
1.5 U (cm/sec) X 1 o'"'
15
( c) Shear ·rate as a func ·ti on of scr e.en speed U.
Figure 4-1, continued.
43
0
~ -300 I
() Q) O')
Q) .µ al S..
S--4 -600 al Q)
.r:: Cl) . z
-900
+1
-3
-.... I () Q) O')
....... Q) .µ
-7 al S--4
S--4 al Q)
.r:: Cl)
• z -11
(b)
0 0.6 r (cm)
·u=75cm/s 9 =5°
0
0.9 1.2
(a) Rate of normal strain as a function of distance r.
2
Rate or 10 '( 18 ) 9 degree
U=75cm/s
r=1 .Ocm
26 34 0 . . ..
normal strain as a function of squeegee angle 90
,
Figure 4-2: a, b and c,
Rate of normal strain as a runctioh of r, 90
and U,
calculated from cq. 2-17(b).
44
0
-- -4 I C) Q) r1l
Q) .µ al S..
S.. -8 al Q)
..c: U)
• z
-12 0 75
U ( cm/sec )
9o=5o
r=1 .Qc~
I !
·' i I I
l I
150
( c) Rate of normal strain as a function of screen spead U.
Figure 4-2, continued
45
4.3 Pressure drop build up by ink tlow in region I
The pressure drop which results from ink flow in region I is a
significant driving force regulating both the ink flow through the
screen holes and, ev.enturally, the printing of the ink on the sub
strate. It is also possible from the proposed model to calculate
the lifting force, i.e., the force acting on the squeegee blade,
which would be required actually to lift the squeegee blad·e from the
screen. Figur·es 4-3 a, b, c, d and e 111 us tra te as a result of the
computer calculation based on the proposed model how the pressure
drop in region ·I of the system is affected by systematic changes in
one of the independent variables, m, n, r, 80
or U.
It is evident from the results presented in Figure 4-3 (a) and
(b) that the pressure drop is greater when the rheological
properties of the ink on the press are characterized by large m and
n values. The increase in ~P is linear with respect to m and ex
ponential with respect to n. The advantage of this enhanced pressure
drop is the fact that more ink will be delivered through the holes
of the screen. As anticipated, the pressure drop decreases as the
value of r increases, i.e. as the distance from the "blade-screen nip
gets larger, as shown in Figure 4-3(c).
When the squeegee angle is increased from 5° to 25°, the pres
sure drop in the system decreases significantly as represented in
Figure 4-3(d). This trend in· pressure drop by varing 80
is similar
46
14
-N
Us75cm/s
eo=50
r=1 .Ocm
n=0.3
e ~ 10 ~ 'tj
........
2 100 200 300
m 400
i
I
I I I i j I
! I I
I I I
500
(a) Pressure drop on the screen as a function of m. 104
U=75cm/s
g- ,02
r=1 .Ocm
9 =5° 0 M 'tj
Q) M ::s [1)
~ 10 M
p...
m=300
0 0.8 1.2 1 • 6 n
(b) Pressure drop on the screen as a function of n.
Figure 4-3: a, b, c, d and e,
The pres-sure drop build up in the ink bank acting on
the screen as a functioh of n, n, r, 80
and U.
47
45 ·-·-··- ·-·-.. - ---·-·-·--·
U=75cm/s I
I 9o=5o
i I - ! N I e m=300 I
30 I C, I
I ....... i c:: n=o.3 >,
'O ........ p. 0 s...
'O
(I) 15 s... ·, ::s a,
"----------a, (I) S... p..
0 n 0 0.3 0.6 0.9 1.2
r (cm) (c) Pressure drop on the screen as a function of r.
90
30
U=75cm/s
r-=1.0cm
m=300
n=0."5
2 JO 18 26 34 e (degree)
(d) Pressure drop on \he screen as a function of 80
•
Fi;tire 4-3, c and d, continued.
48
'
-N e t.)
9
'= 6 >, 'O .....,
0 0
··--- .. ·--... -.. ,-·-------·--····-1 I
7.5
9 =5° 0
r=1 .Ocm
m=300
n=0.3
U (cm/sec} X 10~1
i
15
(e) Pressure drop on the scr~en as a function of U.
Figure 4-3, e, continued.
49
r
to that reported by G. Boycigiller and L •. w. c. Miles.[8, 18] The
model also predicts, as shown in Figure 4-3(e), that as the screen
velocity is increased, the corresponding pressure dr·op increases in
a nonlinear mode. G. Boycigiller and L. W. c. Miles also reported a
similar relationship between .6 P and U. [ 8, 18] The ·validity of the
mathematical model is substant;f.ated by its ability to predict the
results obtained experfmentally as reported in literature.
In addi ti.on to the force exerted normal to the screen by the
build up of the pressure drop in the. ink bank, an opposite force is
also exerted which tends to lift the squeegee from the screen. A's
shown in Figure 4-4(a) and (b), this upward lifting force is very
large when the squeegee angle is small but decreases rapidly as the
angle is increased. [81 An ·increase in the velocity of the screen
will also produce an increase lifting force on the squeegee.(8]
4.4 The flow rate through the screen
The ink flow rate through a single hole in the screen is cal
culated using Equation 3-9 as a function of systematic changes in
the independent variables R, n, 90
, r and U, as ·Shown in Figure
4-5 a, b, o, d and e, respectively.
As shown in Figure 4-5(a), an increase in the radius of the
holes in the screen will cause .a logarithmic type increase in the
flow rate of ink t~rough the screen. This behavior is .logical, and
50
(I)
"Cl a,
,-1
.tJ
c:-(J\J
e p. C)
0 ........ s... C:
"Cl >, "Cl
9 ...-----·- -· - .... ' ...
7
--·-·------------- ---
U=75cm/s
r=1 .Ocm
m=300
n"'0,3
f ._ 5 ::s rn rn (I) s...
p..
(I) 'Cl a,
9
'.ri,,..... 6 ~ o e
C) p. ........ 0 C: r,.. >,
'Cl 'Cl
0
3-r------1----+-----l------J 2 10 18
9 (degree) 0
26
(a) Pressure drop as a function of squeegee
0
9 =5° 0
r=1 0cm
m=300
n=o.3
.~
------------
75 U ( cm/sec )
54
angle, 80
•
I I
150
(b) Pressure drop as a function of screen velocity, U.
Figure 4-4: a and b,
The pressur~ drop exertinc a lifting force on the squeegee as
a function of 80
and U.
51
10-12 ";!!--·-- --·-~ ..... --· .. --· ..... _ --·---
U•75cm/s
r•1 .Ocm
9 =5° 0
n=0.3
I
I 10-l:,,...-"--:~-----i-------+------+,-----J
0
0
0~004 0.008 0.012 0.016 R {cm)
Flow rate as a function of hole size, R.
0.4 0.8 n
U=75cm/s
r=1 .Ocm Q =50·
0
R=0.004cm
1.2
(b) Flow rate as a function of n.
Figure 4-5: a, b, c, d and e,
l I
I I
I i
i I I
!
1 • 6
The flow rate ·throubh a. sinGle hole in the screen as a function
of R, n, 80
, rand U.
52
12
... 0 ... >< 8 -() G) 0) ......
I"\ E! ()
0
·-·-· --· -- ·-··- -·-···-.. ---·--·-------........ -·--1 U•75cm/s
-r=1 .Ocm
R=0.004cm
n=0,3
I I ! I
I ! '
2 10 18 26 34 9
0 (degree)
(c) Flow rate a~ a function of squeegee angle, 99
. 10
,q-.....
0 ->< -() G) rn ......
I"\ E! ()
.........
G) ... ct! ~
) 0
r-i rz.
6.7
3.3
0 0 0.3 0.6
r(cm)
U=75cm/s
R=0,004cm
e =s0 0
n=0.3
0.9
(d) Flow rate as a function of distance, r.
Figure 4-5 c and d, continued.
I I I
I I I
1.2
10 .. ---·--··---· R•0.004cm
I.O r=1 .Ocm / .... 0 8 =5° I .... 0 ;
>< ,.
6.7 n=0.'3 . ,-.. . _: f t) : .... (I) . - . .. II)
......... I"\
E! t) .._,,
QJ 3.3 +> ~ ~
:a 0
,-l
rs..
0+------+------+------4------1 0 75 150
U (cm/sec)
(e) Flow.rate as a function of screen velocity, U.
Figure 4-5 e, continue.
54
a fast flow of inlc would be expected through a "loose" screen with
large openings because it offers little resistance to fluid . .flow.
An increase in the n value which characterizing the degree of
non-Hewtonian behavior of the ink, results in a large increase in
ink flow, as shown in Figure 4-5(b). Conversely, an increase in e . 0
or r would tend to dec~ease the ink flow rate through the screen ac
cording to Figure 4-5(c) and (d), respectively. Finally, an in
crease in the screen velocity will produce a corresponding linear
increase in the ink flow rate as shown in Figure l~-5(e).
4.5 Volume of ink delivered
To the printer, the most irnportant advantage of the mathemati
cal model would be its ability to predict how the volume of ink
delivered to the substrate would be effected· by changing the ink
and/or the press conditions! Equation 3-14, was used to calculate
the volume of ink delivered per hole as a function or· the independ
ent variables R, n and 80
, as shown in Figure 4-6a, band c, ~espec
tively.
Figure 4-6( a) and (b) show· that an increase in R or n results
in a logarithir.ic trpe increase in tho volu1.1e- of ink delivered which
is consistent with the results obtained for the flow rate, Q, varil.!s
in the same manner. The prediction that the volu1.1t, of ink deliv·ered
would decreases as the squeegee angle, 00
, is incr~ased, as shown in
55
,-...
-1~ 10
t"\ -15 e 10 0
(I)
8 ;j
,-t
0 >
10-17
I
.... ···---------------~.
n=0,3
8 12 16
R (cm) x103
(a) Volur.1e of inl: dclive:red as a function of hollJ zize, R.
Figure 4-6: a, band c,
Voluwo of ink delivered as a function of H, n, and 80
•
56
-t"'I e ()
10-18
1 o-20-r------ir------+------+-------J 0 0.4 0.8 1.2 1.6
n
(b) Vol~me of ink delivered as a function of n.
Figure 4-6(b) continued.
57
10
8
U'\
0 6 R=0.004cm ->< ,..... n=0.3
t<"\ e C) ..._,,
Q) 4 e ::, ~ 0 >
2
0 2 10 18 26 34
80
(degree)
(c) Volume of ink delivered as a function of squeegee angle.
Figure 4-6(c) continued.
Figure 4-6(c), agrees with the trend reported by B. F. Dowds and by
N. Hiro.[ 15 ,19] Appendix B pres~nts the numerical values for the
volume of ink delivered over a wide range of independent- variable
values.
The theoretical model also predicts that the volume of ink
delivered is independent of the screen velocity as is evident from
inspection of Equation 3-14. The initial results of rotary screen
printing trial experiments, which were carried out by the
M. Lowenstein Corporation in the printing speed range of 7 to 45
yards per minute, confirm the ·theoretical predictions by showing
that the volume of ink delivered was independent of printing
speed.[20]
The limits of intergration along the·. screen, i.e. the upper c3:nd
lower limits of the r values, for the theoretical predi tions
presented in figure 4;;.6 (a), (b), and (c), were arbitrarily set at
10-6 to 1 cm. The lower limit of intergration is especially impor
tant because the flow rate, normal pressure, and rate of shear all
increase dramatically as r becomes smaller and smaller. It is not
possible, furthermore, to set the lower limit of integration at r
equals to zero because all three quantites approach infinit~ as r
approaches zero, and hence they are not mathematically defined at
the singular point of r equals zero. The rationale for establishing
1 o-6 cm as the lower limit is that this size represents the smallest
59
pigment particle which can be present in the bank.
Calculations. of ink volume delivered were carried out in Figure
4-7 and 4-8 as a function of the variable upper and lower limits of
integration, respectively .Figure 4-7, which for all practical pur
poses shows that the effect of increasing the size of the .ink bank,
shows that the vol~e of ink delivered increases rapidly up to about
one cm followed by a gradual increase with increasing r. Figure
4-8 shows the effect of volume of ink delivered when the bank s'ize
is fixed at one cm and the lower limit of integration is varied for
smaller and smaller va.iues. It is obvious from ~hese calculated
results that the bulk of the ink flow ·occurs at small values of r.
60 ·
10-16 ------·-----··
9 8
9 =5° 7 0
6 R=0,004cm
5 n=0,3
4 ,-...
r,"\ e () .......
3 a, s ::,
9 =50 ,-f 0 0 >
2 R=0,004cm
n=0,3
10-17 -t-----t----+-------l------l 0
Figure 4-7:
0,4 0,8 1.2 1.6
RU (cm)
Volume of ink delivered as a function of upper limit
of integration, RU.
61
10-16 ------·- --·-·· -- ·----------·---·---~-----·-----,
-17 10
R=0.004cm
n==(). J ,..._ t('\
e 0
10-18 ',,J
(1)
e ::, rl 0 >
10-19
10-20
10-5 10-3 1 Q-.1 10 O
RL ( cm)
Figure 4-8: Volume of ink delivered as a function of louer lir.1it
of integration, nL.
62
CHAPTER V
Conclusions and future work
5 .1 conclutions
The limitions of the mathematical model must be reconized for a
proper interpretation of theoretical results and conclusions based
on those resuJ_ts. The mathematical model considers two regions of a
rotary screen printing process, where region one considers the
forces corperative in the bank. of ink above the screen and region
two considers the flow of ink in the hole of the screen. The sub
strate, i.e. the textile, is not taken into consider~tion ·with the
result that there is no pos~tive or negative pressures developed as
ink passes through_ the hole. The hydrostatic head of ink in the
bank is also not taken into consideration. Al though all of these
factors are considered to be potentially significa·nt, their inclu
sion in the theoretical model. are proposed for future work and ex
pansion of the theoretical model as presented in this ·report.
Based on computer calculation using the mathematical model
describing the hydrodynamic flow in region I and II on the press,
the following conclusions can be drawn:
1. The volume of ink .transferred through the screen is inde
pendent o( the screen velocity.
63
,.
2, The ink flow rate and the volU111e of ink transfered
through the screen increases with increasing val ue_s of n.,
which characterize the non-newtonian nature of the ink,
but is independent of the m value, which is th~ apparent
viscosity at a rate of shear of 1 sec·1 ..
3, The volume -of ink transferred through the screen in
creases with decreasing squeegee angle.
4. Although, the volume of ink delivered is increased by in
creasing the size of the ink bank, the majority of ink
flow takes place at small values of r which is a measure-. . . .
ment of the distance from the point of contact of the
squeegee blade with the screen.
5, 2 F.uture research
The mathematical model must -be extended to include region III
and the effects of the substrate on irµc transfer during screen
process printing, The pressure normal to the screen which is in
duced by the hydrostatic head of the bank must also· be added to the
present model. Both of these factors will increase ~he degree of
sophistication of the model presented in this report and can have
the effect of both increasing the magnitude of flow through the
screen and can alter the rela tfonship which have been predicted by
the present model,
references
1. A.Kosloff, Screen Process Printing, Times Pub. co., Ohio,{1950)2.
2. B.Zahn, Screen Process Methods of Reproduction, Drake, Ill., { i950) 13.
3. B.Miller and D.B.Clark, Textile Research, 3(1978)150.
4. B.Miller and D.B.Clark, Textile Research, 5(1978)256.
5. L.S.Penn, C.K.Nitta and L.Rebenfeld, Textile Research, 12(1981)324.
6. A.M.Schwartz and C.A.Rader, Chem., Phys. and Appl. Surf. Active Substances, Vol.12, edited by J._Th.G.Overback, N.Y.(1967)383.
7. R.L.Derry and R.S.Higginbotham, J. of the Society of Dyers and Colorists, ·59( 1953)569.
8. G.Boyacigiller, A Study of The Flow of Printing Pastes in Screen Pr~nting, Ph.D. Thesis,· (197.0)Victoria U. of Manchester.
9. H.Schlichting, Boundary Layer Theory, 7th ed., McGraw-Hill, N • Y , ( 1 97 9 )7 3 •
10. R.B.Bird, W.E.Stewart and E.N.Lightfoot, Transport Phenomena, John Wiley & Sons, N.Y.(1960)1-30.
11. H.Schlichting, Boundary Layer Theory, 7th ed~, McGraw-~ill, N.Y.(1979)112.
12. R.B.Bird, R.C.Armstrong and O.Hassager, ·Dynamics of Polymeric Liquids, John Wiley & Sons, N.Y.(1977)7.
13, R.B.Bird, W.E.Stewart and E.N~Lightfoot, Transport Phenomena, John Wiley & Sons, N.Y.{1960)102.
14. S.Middleman, Fun~~entals of polymer Processing, McGraw-HU!, N. Y, { 1977) 87,
15. B.F.Dowds, J, of '.!'he Society of Dyers and Coloists, 12(1970)512.
16. R.H.Perry and C.H.Chilton, Ch. E. Handbook, 5th ed·. McGraw-Hill, N.Y.{1973)5-33,
17. R.B.Bird, R.C.Armstrong and O.Hassager, Dynamics of Polymeric Liquids, John Wiley & Sons, N.Y.(1977)208.
18. L. W. C.Miles, Tex~ile Printing, Merrow, England( 1971) 25,
19. K.Teraji and N.Hiro, Sen-I-Gakkaishi (Japanese), 33, Vol. 2(.1977) 102.
20. Private communication with W. J. Kennedy at M. Lowenstein Corporation.
66
I
Appendex A
Solution for streat:i function,
From the Havier-Stokes equation 2-1, the equation for the
stream function, , is reduced to equation 2-4:
where ljJ is defined as
V = r
1 ~ r ae
And boundary conditions arc:
V (r,8=0) r
= - u
v8
(r,8=0) = 0
v (r,O=O ) r o
= 0
67
A-1
A-2
A-3
The reduced ?Javier-Stokes equation A-1 and the boundary c_on
di tions n:ieet the criteria for homogeneous constant coefficient
fourth-order partial differential equation.
Since "for all values of r, at 9 = O; equation A-2 becoraes:
V = r
- .!.£!_ r ae - - u
So, by solv_ing e_quati_on A-4, 1/1 beco:iles:
1/1 = - UrG(8) + F(r)
A-4
A-5
where G( 9 ) is defined as a function of 9 only; t( r) is defined
as a function of r only.
Substituting in .equation A-3 the function for i.µ as described
in equation A-5 yields:
V = ~ = 0 e ar = -UG(8) + dF(r)
dr
Since g( 9) is function of only 9 ~nd F( r ) is function of only r 1
then for all values of r at 9 = 0:
68
dF(r)
ar - 0
indicating that
F(r) = C 0
where C0
is a constant.
Substitutin~ equation A~B in A-5 yields:
$ = - UrG(B) + C = rH(B) + C 0 0
where H( e ) ~ - U G( e)
Substituting equation A-9 in A-1 produces:
4 2 .,
~ H(B) + 2 ~ H(B) + H(.B) = 0
dB dB
Solvin~ equation A-10 for B( 9) yields:
69
A-7
A-8
A-9
A-10
H ( 8) = c1cos(8) + c2sin(8) + C 8cos(8) + C 8sin(8) . 3 4 A-11
Substituting for H( 9 ) in equation A-9, the strear:i function be-
co1:ies:
Ey substituting equation A-12 into A-2 and A-3, the constant C0
will disappear and the constants c1, c2, c3 and c4 can be solved by
using the boundary conditions.
Appendex·B
Numerical results of volume of ink delivered.
90 n R V
degree cm cm3
5.000 .200 .002 .239002E-22 5.000 .200 .004 .611846E-20 5 .ooo. .200 .006 .156809E-18 5;000 .200 .008 • 1 56 6 3 3E-17 5.000 .200 .010 .933603E-17 5.000 .300 .002 .434793E-16 '5. 000 .300 • 0014 ,350595E-14 5.000 .JOO .006 .457142E-13 5.000 .300 .008 .282702E-12 5.000 .300 .010 . 11 6 1 7 0 E- 11 5.000 .400 .• 002 .586440E-13 5.000 .400 .004 .265392E-11 5 . "'' • "j' '
t, ·,I/", . 21Hi82.S:-'.-10 ,·.
.. oo ·; .: co .008 .12010::(-09 5. }~/ . '(0 ;010 .409787E-09 5.000 .700 .002 .620058E-09 5.000 • 700 .004 .133526E-07 5.000 • 700 .006 .804263E-07 5.000 .100 .008 .287540E-06 5.000 .100 .010 • 772451E-06 5.000 1.000 .002 .252416E-07 5.·000 1. 000 .004 .403865E-06 5.000 1.000 .006 .20lJ457E-05 5.000 1.000 .008 .646184E-05 5.000 1. 000 .010 • 157760E-04
10.000 .200 .002 .11870~E-22 10.000 .200 .004 • 303880E-20 10 •. 000 .200 .006 .778811E-19 10.000 .200 .008 .777933E-18 10.000 .200 .010 • 46 3684E-17 10.000 .300 .002 .216868E-16 10.000 ,300 .004 .174871E-14 10·.000 ,300 .006 .228015E-13 10.000 .300 .008 .141007E-12 10.000 .300 .010 .579436E-12
71
10.000 .400 .002 .293131E-13 10.000 .400 .004 • 132656E-11 10.000 .400 .006 .123376E-10 lO. 000 .400 .008 .600333E-10 10.000 .400 .010 .204832E-09 10.000 .700 .002 .310786E-09 10.000 ·.100 .004 .669260E-08 10 .ooo .700 .006 .403114E-07 10.000 .700 .008 .144121E-06 10.000 .700 .010 .387169E-06 10.000 1.000 .002 .126655E-07 10.000 1.000 .004 .202648E-06 10.000 1.000 .006 • 102590E-05 10.000 1.000 .008 .324236E-05 10.000 1.000 .010 .791593E-05 15.000 .200 .002 .787989E-23 15.000 .200 .004 .201725E-20 15.000 .200 .006 .516999E-19 15.000 .200 .0.08 .516416E-18 15.000 .200 .0·10 .307808E-17 15.000 .300 .002 .144169E-16 1-5. 000 .300 .004 .116250E-14 15.000 .300 .006· .151579E-13 15.000 .300 .008 .937384E-13 15.000 .300 .010 ,385195E-12 i5.000 .400 .002 • 195005E-13 15.000 .400 .004 .882493E-12 15.000 .400. .006 .820755E-11 15.000 .400 .008 . 399371 E-10 15.000 .400 .010 • 136264E-09 15.000 .700 .002 .206940E-09 15.000 .700 .0"04 .445632E-08 15.000 .700 .006 .268416E-07 15.000 •. 700 .008 ,959642E-07 15.000 .700 .010 .257800£-06 15.000 1.000 .002 .843650E-08 15.000 1.000 .004 • 134 984E-06 15 .·ooo 1.000 .006 .683357E-06 15.000 .1 • 000 .008 .215974E-05 15.000 1.000 .010 .527281E-05 20.000 .200 .002 .588376E-23 20.000 .200 .004 .150624E-20 20 •. 000 .200 .006 .386033E-19 20.000 .200 .ooa .385598E-18 20.000 .200 .010 .229834E-17
72
20.000 .300 .002 .107725E-16 20.000 .300 .004 .868643E-15 20.000 .300 .006 .113262E-13 20.000 .300 .008 .700430E-13 20.000 .300 .010 .287825E-12 20.000 .400 .002 .145764E-13 20.000 .400 .004 .659651E-12 20.000 .400 .006 .613502E-11 20.000 .400 .008 .298524E-10 20.000 .400 .010 .101855E-09 20.000 .700 .002 .154756E-09 20.000 .700 .004 .333258E-08 20.000 .700 .006 • 2007 30E-07 20.000 .700 .008 .717650E-07 20.000 .700 .010 .192791E-06 20.000 1.000 .002 .631025E-08 20.000 1.000 .004 .100964E-06 20.000 1.000 .006 .511130E-06 20.000 1.000 .008 .161542E-05 20.000 1.000 .010 .394390E-05 25.000 .200 .002 .468292E-23 25.000 .200 .004 • 119883E-20 25.000 .200 .-006 .307246E-19 25.000 .200 .008 • 306900E-18 25.000 .200 .010 .162926E-17 25.000 .300 .002 .857768E-17 25.000 .300 .004. .691661E-15 25.000 .300 .006 .901857E-14 25.000 .300 .008 .557720E-13 25.000 .300 .010 •· 229182E-12 25.000 .400 .002 .116091E-13 25.000 .400 .004 .525366E-12 25.000 .400 .006 .488611E-11 25.000 .400 .008 .237753E-10 25.000 .400 .010 .811207E-10 25.000 .100 .002 • 123'287E-09 25.000 .100 ;oo4 .265491E-08 25.000 .700 .006 .159913E-07 25.000 .100 .008 • 571719E-07 25.000 ,700 .010 • 153587E-06 25.000 1.000 .002 .502765E-08 25.000 1.000 .004 .804424E-07 25.000 1.000 .006 .407240E-06 25.000 1.000 .008 • 128708E-05 25.000 1.000 .010 ,314228E-05
73