Journal of Materials Processing Technology, 24 (1990) 225-233
225
Elsevier
ROTARY SPLITTING
-
A NOVEL SHEET METAL FORMING TECHNIQUE
BAUER Institut of P r o d u c t i o n E n g i n e e r i n g , U n i v e r s i t y P.O. Box 101240, D 5900 Siegen (FRG)
D.
Siegen,
SUMMARY A first attempt is given to analyse and describe Skinner's rotary splitting technique theoretically. It is found that this technique is of high kinematical compiexity and quite sensitive to changes in process parameters. Negiecting eiasticai deformation effects a piastomechanical theory is presented to predict the deformation force, depending on tooi geometry, workpiece properties, feed rate and mandrel speed. Results achieved by this theory are compared to those obtained by experimental work. A large difference between experimentei and theoretical values is found and attributed to neglecting eiastical effects. Therefore, in the next step of investigation the author intends to improve his theory and compietes it by these effects. Additionally friction and work hardening effects shali be considered in future, too. INTRODUCTION In 1963 W.J. Skinner has been taken out a patent for a combination of transverse facturing
roliing and metai spinning technology
V-beit puiiey and simiiar components
with round profile~
Skinner cailed this novei chipless forming technique ting
(ref.
I). In the meantime
sucessfully
in automotive
Skinner's
industry
(refs. 2-3).
patent has been appiied
But the theoreticai
metai working process is aimost compieteiy any resuit of research, has been pubiished
Skinner'a rotary spIitting of our investigations
process.
background
of
of this
forming technique
Therefore,
and theoretical
econo-
optimisation
unknown because not
dealing with Skinner's
up to the present.
we started experimental
Rotary Split-
ieading to considerabie
mic benefits with weight savings and structurai V-belt puliey
manu-
two years ago,
investigations
analysing
In this paper first results
wiil be presented.
FORMING PROCESS The principle machinery
of the forming process is shown in Fig. I. The
employed
is simiiar to that used for metal spinning
(ref. 4). Starting workpiece may be a blank of 3 - 6 mm thickness
0924-0136/90/$03.50
© 1990---Elsevier Science Publishers B.V.
226
Forming Railer
Blank
Fig. 1. Principle of Skinner's rotary splitting technique using a driving blank as workpiece and a driven forming roller as tool
227
or a similar workpiece
pre-form
machine.
Forming tool
suitable
material
(ref.
with a central
is centered
5). This
and clamped involved
and shape.
forming
cular to the axle of mandrel. contact too,
Simultaneously
perpendicular mation zone,
of friction
This
appearing
splitting
of
rolling
roller
comes
between tool
is starting
and work-
because the
tool forces
of the w o r k p i e c e - d i a m e t e r
into
it begins rotating,
plastic
defor-
RWS in the contact
2.
localized
plastic
deformation
in radial
and circumferential
workpiece
with an annular
Fig.
workpiece
feed rate of the rotating
and reduction Fig.
rotary
roller
This
of the
along a path perpendi-
When the forming
forces
flange.
mandrel
to transverse
is powered
with the rim of the rotating
by means
piece.
is a free running
Similar
roller
hub and circular
on the rotating
is continuoualy
direction
groove
delivering,
of V-ehape
processing
finally,
a
at its periphery,
1.
DEFORMATION MECHANISM The mechanism o f t h e d e f o r m a t i o n p r o c e s s i s up t o t h e p r e s e n t no a n a l y s i s e x i s t s point
of our i n v e s t i g a t i o n
analysis of the relevant
v e r y complex and
dealing with it,
has been t h e r e f o r e ,
Starting
a kinematical
process parameters e f f e c t i n g
t h e depth
o f p e n e t r a t i o n T and t h e c o n t a c t area o f t h e f o r m i n g t o o l causing p l a s t i c Assuming t h a t following
AK
deformation in the workpiece. elastical
s p r i n g b a c k can be n e g l e c t e d t h e
e x p r e s s i o n s can be d e r i v e d a c c o r d i n g t o
Fig.
2:
BK AK = 2 K2 f 0
(K1 eA + K2 s i n
Where K1 = RWZ - K2; BK = a r c s i n
(1)
a A) d B
K2 = RR; K3 = ( ~ - y ) / 2 ;
a A = K3 B/8 K
(2)
(b/Rwz)
(3)
a + c = RWS + RWZ a
2
+
b2
2 = RWZ
(4) (5)
b 2 + c 2 = (Rws + s) 2
Where B K : a n g l e o f ferential
c o n t a c t between r o l l e r
direction:
and w o r k p i e c e i n
a A = a n g l e o f c o n t a c t between r o l l e r
circumand
228
×
z~Y
Fig. 2. Kinematical process parameters determing the amount of contact area between tool and workpiece.
229 workpiece
in axial direction;
RWS = radius
forming roller; V-groove;
R o = original radius of workpiece;
of deepest point of V-groove; R R = radius
RWZ = outer radius of
of roller edge;
y = shoulder angle of
and s = feed rate of forming roller.
Notice that eqn.
(I) is a t r a n s c e n d e n t a l
one and can, therefore,
be solved only iteratively. The integration matical
of eqn.
expression
(I) is delivering,
finally,
a mathe-
in order to predict the amount of the contact
area A K at the interface
between tool and workpiece.
study of this expression
has been revealed that at constant values
of T the amount of A K is increasing y and s are increasing, that at constant
too.
DEFORMATION
if the values of Ro, RWZ,
R R,
On the other hand it has been found
values of Ro, RWZ,
decreases with increasing
A parameter
RR, y and s the amount of A K
vaiues of penetration
depth T.
FORCE
In the second part of our i n v e s t i g a t i o n s find a p i a s t o m e c h a n i c a i theory
we have been tried to
predicting the deformation
force
F z, Achieving this aim we fitted to our problem a proposai of M.W. S t o r o s c h e w and E.A.
Popow
(ref. 6). These research workers
for the normal stress distribution
o n produced
force on the contact area the foiiowing on = kf Where
(1 + ~A -
choosed
by the deformation
simplification,
Fig. 3.:
~)
(6)
kf is denoting the effective s t r e s s - s t r a i n
curve of work-
piece materiai. MultipIying this stress distribution, ponding
contact area, BK
F
Z
= 2 ~
(I), we get,
eqn.
(6),
by the corres-
finaliy:
~A kf
cos
8 ~
O
[(1+~ A -
~)
cos
e •
0
K 2 (K 1 + K 2 c o s
Eqn.
eqn.
(7) ~)]
d ~ d B
(7) can be soived by the assumption that
kf = kfm = constant.
This means that work hardening of workpiece material wiIi not be taken
into account.
A parameter study of this soiution
vering the following t h e o r e t i c a l results:
Choosing
is deii-
constant
for kfm ; Ro; RWZ ; RR; X and s the amount of the deformation
values force
230
!
--~X
o.
'/
0n=2,27
Fig. 3. A s s u m p t i o n a c c o r d i n g to (ref.
F z decreases regarding,
with
on the
F z is g r o w i n g
of stress 6).
increasing other
distribution
values
hand,
up at i n c r e a s i n g
on c o n t a c t
of p e n e t r a t i o n
constant values
values of kfm,
area
depth
T;
and
of T the
amount
of
R o,
R R and
s.
RWZ,
231
1600
I/,00
J
_J
1200
IOO0 rt
800
u~ o
600
U..
400
/0
200
0
5
15
10
25
20
Depth (mm)
Fig.
4.
Comparison
of e x p e r i m e n t a l
(a)
and t h e o r e t i c a l
(b)
forces.
RESULTS In the and
following
experimental
carbon micro
steel
roller
was
was
Lubricant tions
we
are
results
submitted.
Sheet
material
yield
stress
150 HV 0,05).
were
s = 0,03
employed observed
of our t h e o r e t i c a l
(4 mm t h i c k n e s s ;
R ° = 65 mm.
involved
choosed
work
Stw 24
hardness
deformed
first
RWZ mm/U
was
The
The
initial
geometrical
= 65 mm
and
Kooher
y = 34 ° at m a x i m u m
speed F i00
depth
used
RpO,2
of the
dimensions
R R = 0,3
at a m a n d r e l
of t y p e
radius
computations
mm.
was
blank
of the
The
low
= 290 MPa,
feed
forming rate
U = 180/minute. E. U n d e r
T = 25 mm.
these
condi-
232
E -i
160--i 150
Fig. 5, L i n e s steel S t w 24 1 5 0 HV 0 . 0 5 .
of constant a n d T = 25
microhardness mm. H a r d n e s s
of
HV 0 , 0 5 a t undeformed
low carbon material
233
The resuits
of the force measurement
the theoretical
results
F z was measured
by means
penetration
in Fig.
of high sensitive
depth T by an inductive
The theoreticai
vaiues
But in order to integrate Thus,
we measured
of the workpiece one.
The results
Looking
at Fig.
are presented
deformed
strain
dispiacement
have been computed this equation
the hardness
of our measurement
are presented
piace in the deformation kfm = 1,55
CONCLUDING
to eqn.
are showing
in Fig. hardening
zone.
5. of about
Regarding
this
• Rpo,2 = 450 MPa for the compu(7).
4 the results
not yed good agreement
The Iarge difference of deformation fore,
(7).
REMARKS
As can be seen from Fig.
friction,
eqn
in the cross section
155 % has been taken
of F z according
and the
it with that of the starting
we choosed, tation
gauges
we needed the vaiue of kfm.
distribution
and compared
force
transducer.
by soiving
5 it can be seen that a materiai
finally,
aiong with
4. Where the deformation
with those
between theoreticai
force Fz, couid possibiy
workhardening
computed
and eiastical
we intend to improve
by experiment.
and experimental
attributed
deformation
and compiete
by our theory
our theory
values
to negiecting effects.
There-
by these effects
in the next step of our investigations. REFERENCES I 2
3 4
5
6
C. Packham, Manufacture of one piece sheet metal V-belt pulleys with up to three grooves, Sheet Metal Industries, 55 (4) (1978) 441-445. D.H. Poiitt, The Practice and Potentiai of Flow Forming Processes, in: Proc. Ist. Int. Conference on Rotary Metai Working Processes, London, November 20-22, 1979, IFS-Pubiications, Kempston, pp. 21-32. R. Noppen, Neue Werkstoffanwendungen in der Fahrzeugtechnik, in: Proc. Fertigungstechnisches Koiioquium FKT 85, Stuttgart, October 10-11, 1985, Springer, Beriin, 1989, pp. 67-72. C. Maiiana, H.N. Nagarajan and M.E. Visveswaran, Process Parameters in Flow Forming and how they affect the End Product, in: Proc. Ist. Int. Conference on Rotary Metal Working Processes, London, November 20-22, 1979, IFS-Publication, Kempston, 1979, pp. 2 3 1 - 2 4 2 . G. Thompson and J . B . H a w k y a r d , Crack F o r m a t i o n i n T r a n s v e r s e Rolling, in: Proc. 1st. Int. Conference on Rotary Metai Working Processes, London, November 20-22, 1979, IFS-Publication, Kempston, 1979, pp. 171-184. M.W. Storoschew and E.A. Popow, Grundlagen der Umformtechnik, 1st edn., VEB Verlag Technik, Berlin, 1968.