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Procedia Manufacturing 50 (2020) 79–85
2351-9789 © 2020 The Authors. Published by Elsevier B.V.
This is an open access article under the CC BY-NC-ND license ( http://creativecommons.org/licenses/by-nc-nd/4.0/ )
Peer-review under responsibility of the scientific committee of the 18th International Conference Metal Forming 2020
10.1016/j.promfg.2020.08.015
10.1016/j.promfg.2020.08.015 2351-9789
© 2020 The Authors. Published by Elsevier B.V .
This is an open access article under the CC BY -NC-ND license ( http://creativecommons.org/licenses/by-nc-nd/4.0/ )
Peer -review under responsibility of the scientific committee of the 18th International Conference Metal Forming 2020
Avail abl e on lin e at www.scie n c edir e ct.com
ScienceDirect 
Pr ocedia Manuf actur ing 00 ( 201 9) 000–00 0
ww w.elsevier .c om/locate/procedia

2351- 9 7 8 9 © 202 0 T h e Autho r s. Published by E l s evier B. V.
This is an open acc ess article under the CC BY-NC-ND license (http://cre a tivecom m ons.org/l icenses/by-nc-nd/4 . 0/)
Peer-review under responsibility of th e scie ntific comm it tee of the 18th Inte rnati onal Conference Met a l Form ing 2020 Project.
18th International Conference Metal Forming 2020 Project
Numeric al and experi mental evalu ati on of a n a lternative mec hanism for
wall thickness variations of hollo w prof il es applying a por thole die
Maik Ne genda nk a, *, V i dal Sanabr ia a , Walter Reimers b , Soeren Mueller a
a Extrusion Research and Development Center TU Be rlin , Gustav-Meyer -Al l ee 25, 13355 Berlin, Germany
b Chair Metallic Materials TU Berlin, Erns t-Reuter-Plat z 1, 10587 Berlin, Germany
* Cor r e spondin g author . T e l. : +49- 303- 147- 25 1- 6; f a x: +49- 303- 14 7- 250- 3. E - mai l address: m a ik. n egendank@ str a ngpr essen. ber lin
Ab s tract
The cross sectio ns of conven tion a lly extrud ed pr ofiles r e main co nstant along the length o f th e ex trudates du e to application of static, rigid dies .
The profile cross section is dimen s ioned ac cording to the expected loads applied duri ng techn i ca l appl ica tion. Most ly , t h e loa d s ar e not distributed
homogen eously upon th e length of a product . Th us , lo cally ov er- d imensioned pro f ile ar eas are the result. In order to optimize t he p rofile design
and th erefor e o b tain ligh t er pro ducts, load adap ted tailored pr of ile s sh o uld be manufa ctured . I n t his p a per a me ch anism for w al l thickn ess
variations of lig htweight hollow profiles wa s inv e s tigat ed by fin i t e el emen t an alys i s (F EA) and ex perim e nta l extru s ion trials . The principl e for
manufa c turing wall th ickness v a ria tions is ba sed on application of bending elements whic h work as bear ing ch annel at the por t h o le di e. The i r
defle c t ion in dir ecti on of the die b ear ing would le ad to wall th ick ness reductions. An increase of the wall th ickn esses should be achieved by a
defle c tion of the bending ele m ent s back into d i re ct ion of thei r in iti a l position due to the nor mal press u re of the flowin g alu m i n u m b i l l e t m a t e r i a l .
FEA of the mater i al f l ow during extrusion was con ducted in ord e r t o inves tig ate th e principl e f eas ibi l ity of the mech an ism. Th e for ce r e quirements
for wall th icknes s varia tions wer e also g a in ed fro m th e num eri c simulations on the one hand . The fo rce n e cessary for the def l ec tion of the bend ing
elements was als o deter mined in an exper imen t al test setup . T he extrusion t ryouts a pplying th e dev e loped mech anis m r evealed t ha t t h e f o r c e o f
the hyd r aulic drive w as successf ully tr ansmitted ont o th e moveab le seg m ents inside of the portho l e die. Although subsequent to th e ex trusion
experiments variations of th e hollow profil e wall thicknesses wer e observ e d, it w a s f ound ou t that th ey w e re not induced by the develop e d
mech anis m as in tended . Ins tead , aluminu m bil let mat e ria l f ill ed even smallest vo ids and gaps inside of th e mechanism causing de flec tion and
failur e of diff erent co mponents that effected th e d evelop m ent of the wall thic kn ess.

© 2020 Th e Authors. Published by Elsev i er B.V.
This is an op en a cces s a r ti cle und er th e CC BY-NC-ND license (h ttp:/ /cr eat iveco m m ons.org/l icense s/by-nc-nd/4.0 / )
Peer-revi ew und er responsibi lity of the sc i e ntif ic commi ttee of th e 18th In tern ation a l C o n f e r e n c e M e t a l F o r m i n g 2 0 2 0 P r o j e c t .
Keywords: alum in um ; extr usion; hollow pr of ile; var i able wall thickness; p o r t hole die

1. Introduction
In today’s extrusion ind ustry the cross section of profiles is
defined b y rigid tool s such as extrusio n dies and mand rels.
Convent ionally, o nly profile s with co nstant cross sections can
be produced. Dur ing the use of extrud ed products in techn ical
applicati ons the l oads usuall y are not distribute d
homoge neously upon the lengt h of a pr oduct. Thus, l ocally over
dimensioned profile areas are the result. In order to avoid these
and hence re duce the profile weig ht, extrusion dies need to be
developed to offer more flexibility regarding th e achievable
profile cr oss sections. It woul d then be possi ble to manufact ure
profiles with (tailored) cross sections that are lo cally adapted to
the acting load s. Due to weight reduction th ese innovative
profiles c ould contri bute to a red uction of f uel consumptio n as
well as emissi ons of com bustion gases when being a pplied for
vehicles with combustion engine s. Furthermore, the range of
vehicles with electric driv e could be exten ded by substitu tion
of conv entionally ex truded co mponents with th ese innovative
load adapted tailo red profiles. In order to develop the
producti on of such extruded, mo difications rega rding the
extrusion process and the di e technology have been
investigated , yet mostly for research purposes only.
Avail abl e on lin e at www.scie n c edir e ct.com
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Pr ocedia Manuf actur ing 00 ( 201 9) 000–00 0
ww w.elsevier .c om/locate/procedia

2351- 9 7 8 9 © 202 0 T h e Autho r s. Published by E l s evier B. V.
This is an open acc ess article under the CC BY-NC-ND license (http://cre a tivecom m ons.org/l icenses/by-nc-nd/4 . 0/)
Peer-review under responsibility of th e scie ntific comm it tee of the 18th Inte rnati onal Conference Met a l Form ing 2020 Project.
18th International Conference Metal Forming 2020 Project
Numeric al and experi mental evalu ati on of a n a lternative mec hanism for
wall thickness variations of hollo w prof il es applying a por thole die
Maik Ne genda nk a, *, V i dal Sanabr ia a , Walter Reimers b , Soeren Mueller a
a Extrusion Research and Development Center TU Be rlin , Gustav-Meyer -Al l ee 25, 13355 Berlin, Germany
b Chair Metallic Materials TU Berlin, Erns t-Reuter-Plat z 1, 10587 Berlin, Germany
* Cor r e spondin g author . T e l. : +49- 303- 147- 25 1- 6; f a x: +49- 303- 14 7- 250- 3. E - mai l address: m a ik. n egendank@ str a ngpr essen. ber lin
Ab s tract
The cross sectio ns of conven tion a lly extrud ed pr ofiles r e main co nstant along the length o f th e ex trudates du e to application of static, rigid dies .
The profile cross section is dimen s ioned ac cording to the expected loads applied duri ng techn i ca l appl ica tion. Most ly , t h e loa d s ar e not distributed
homogen eously upon th e length of a product . Th us , lo cally ov er- d imensioned pro f ile ar eas are the result. In order to optimize t he p rofile design
and th erefor e o b tain ligh t er pro ducts, load adap ted tailored pr of ile s sh o uld be manufa ctured . I n t his p a per a me ch anism for w al l thickn ess
variations of lig htweight hollow profiles wa s inv e s tigat ed by fin i t e el emen t an alys i s (F EA) and ex perim e nta l extru s ion trials . The principl e for
manufa c turing wall th ickness v a ria tions is ba sed on application of bending elements whic h work as bear ing ch annel at the por t h o le di e. The i r
defle c t ion in dir ecti on of the die b ear ing would le ad to wall th ick ness reductions. An increase of the wall th ickn esses should be achieved by a
defle c tion of the bending ele m ent s back into d i re ct ion of thei r in iti a l position due to the nor mal press u re of the flowin g alu m i n u m b i l l e t m a t e r i a l .
FEA of the mater i al f l ow during extrusion was con ducted in ord e r t o inves tig ate th e principl e f eas ibi l ity of the mech an ism. Th e for ce r e quirements
for wall th icknes s varia tions wer e also g a in ed fro m th e num eri c simulations on the one hand . The fo rce n e cessary for the def l ec tion of the bend ing
elements was als o deter mined in an exper imen t al test setup . T he extrusion t ryouts a pplying th e dev e loped mech anis m r evealed t ha t t h e f o r c e o f
the hyd r aulic drive w as successf ully tr ansmitted ont o th e moveab le seg m ents inside of the portho l e die. Although subsequent to th e ex trusion
experiments variations of th e hollow profil e wall thicknesses wer e observ e d, it w a s f ound ou t that th ey w e re not induced by the develop e d
mech anis m as in tended . Ins tead , aluminu m bil let mat e ria l f ill ed even smallest vo ids and gaps inside of th e mechanism causing de flec tion and
failur e of diff erent co mponents that effected th e d evelop m ent of the wall thic kn ess.

© 2020 Th e Authors. Published by Elsev i er B.V.
This is an op en a cces s a r ti cle und er th e CC BY-NC-ND license (h ttp:/ /cr eat iveco m m ons.org/l icense s/by-nc-nd/4.0 / )
Peer-revi ew und er responsibi lity of the sc i e ntif ic commi ttee of th e 18th In tern ation a l C o n f e r e n c e M e t a l F o r m i n g 2 0 2 0 P r o j e c t .

Keywords: aluminum; extrusion; hollow profile; variable wall thickness; porthole die

1. Intr oduc tion
I n t o d a y ’ s e x t r u s i o n i n d u s t r y t h e c r o s s s e c t io n o f p r o f i l e s i s
defi ned b y ri g i d t o ol s suc h as ext r usi o n d i es and ma nd r e l s .
C o n v e n t i o n a l l y , o n l y p r o f i l e s w i t h c o n s t a n t c r o s s s e c t i o n s c a n
b e pr odu ced. D ur i ng th e u s e of ex trud ed p r o du c ts in techn i cal
a p p l i c a t i o n s t h e l o a d s u s u a l l y a re n o t d i s t r i b u t e d
ho mo ge neo u sl y u p o n t h e l e n g t h of a p r od uct . T hus , l o cal l y o v er
dimensioned profile areas are the resu lt. In ord e r to avo id these
and he nce re d u ce t h e p r o f i l e wei g ht , ext r usi on di es need t o be
d e v e l o p e d t o o f fer more flex ib ility reg a rdin g th e ach ievab le
pr ofi l e cr oss se ct i ons. It w oul d t h e n be p o ssi bl e t o ma n u fac t ure
p r o f iles with (t ailo red) cro ss sectio n s t h at are lo cally ad ap ted t o
th e actin g l o ad s. D u e t o weig h t r e du ction th ese i n novativ e
pr ofi l e s c o ul d cont ri b u t e t o a red u ct i o n of f u el con s u m pt i o n as
wel l as emi ssi ons of c o m b us t i on gases w h e n b ei n g a p p l i e d f o r
vehicles with combustion engine s. Fu r t h e rmor e, t h e r a nge of
v e h icles with electric d r iv e co u l d b e ex ten d ed by sub s titu tio n
o f co nv en tion a lly ex tru d e d co mp on en ts wit h th ese inno v a tiv e
lo ad ad ap ted tailo red p r ofiles. In ord e r to d e v e l o p th e
pr o duct i o n of suc h e x t ru d e d , mo di fi cat i o ns rega rdi n g t h e
ext r usi o n p r o cess a n d t h e di e t ech n o l o gy hav e been
in v e stig ated , yet mo stly fo r research purpo ses on ly.

Avail abl e on lin e at www.scie n c edir e ct.com
ScienceDirect 
Pr ocedia Manuf actur ing 00 ( 201 9) 000–00 0
ww w.elsevier .c om/locate/procedia

2351- 9 7 8 9 © 202 0 T h e Autho r s. Published by E l s evier B. V.
This is an open acc ess article under the CC BY-NC-ND license (http://cre a tivecom m ons.org/l icenses/by-nc-nd/4 . 0/)
Peer-review under responsibility of th e scie ntific comm it tee of the 18th Inte rnati onal Conference Met a l Form ing 2020 Project.
18th International Conference Metal Forming 2020 Project

Numerical and experimental evaluati on of an alternative mechanism for
wall thickness variations of hollo w profiles applying a porthole die
Maik Negendank a, *, Vidal Sanabr ia a , Walter Reimers b , Soeren Mueller a
a Extrusion Research and Development Center TU Berlin , Gustav-Meyer-Allee 25, 13355 Berlin, Germany
b Chair Metallic Materials TU Berlin, Ernst-Reuter-Platz 1, 10587 Berlin, Germany
* Corresponding author . Tel.: +49-303-147-251-6; f ax: +49-303-147-250-3. E-mail address: maik.negendank@strangpressen. berlin
Abstract
The cross sections of conven tionally extruded profiles remain constant along the length o f the extrudates due to application of static, rigid dies.
The profile cross section is dimens ioned ac cording to the expected loads applied duri ng technica l application. Mostly, the load s ar e not distributed
homogeneously upon th e length of a product. Thus , lo cally over-dimensioned pro file areas are the result. In order to optimize t he profile design
and therefore o btain lighter products, load adapted tailored pr of iles should be manufactured. In this p aper a mechanism for wal l thickn ess
variations of lightweight hollow profiles wa s investigated by fin ite element analys is (FEA) and experimental extrusion trials . The principle for
manufacturing wall th ickness variations is ba sed on application of bending elements whic h work as bearing channel at the portho le die. Their
deflection in direction of the die bearing would lead to wall th ick ness reductions. An increase of the wall thicknesses should be achieved by a
deflection of the bending elements back into direction of thei r in itial position due to the normal pressure of the flowing alu m inum billet material.
FEA of the material flow during extrusion was conducted in order to investig ate the principle f eas ibility of the mechan ism. The force requirements
for wall thicknes s variations were also gain ed from the numeric simulations on the one hand . The force necessary for the deflec tion of the bending
elements was also determined in an exper imental test setup. The extrusion tryouts a pplying the dev eloped mechanism revealed tha t the force of
the hydraulic drive was successfully transmitted onto the moveable seg ments inside of the porthole die. Although subsequent to the extrusion
experiments variations of th e hollow profil e wall thicknesses were observed, it was f ound out that they were not induced by the developed
mechanism as intended. Ins tead, aluminum bil let material f illed even smallest voids and gaps inside of the mechanism causing de flection and
failure of different co mponents that effected the develop ment of the wall thickness.

© 2020 Th e Authors. Published by Elsev i er B.V.
This is an op en a cces s a r ti cle und er th e CC BY-NC-ND license (h ttp:/ /cr eat iveco m m ons.org/l icense s/by-nc-nd/4.0 / )
Peer-revi ew und er responsibi lity of the sc i e ntif ic commi ttee of th e 18th In tern ation a l C o n f e r e n c e M e t a l F o r m i n g 2 0 2 0 P r o j e c t .
Keywords: alum in um ; extr usion; hollow pr of ile; var i able wall thickness; p o r t hole die

1. Intr oduc tion
I n t o d a y ’ s e x t r u s i o n i n d u s t r y t h e c r o s s s e c t io n o f p r o f i l e s i s
defi ned b y ri g i d t o ol s suc h as ext r usi o n d i es and ma nd r e l s .
C o n v e n t i o n a l l y , o n l y p r o f i l e s w i t h c o n s t a n t c r o s s s e c t i o n s c a n
b e pr odu ced. D ur i ng th e u s e of ex trud ed p r o du c ts in techn i cal
a p p l i c a t i o n s t h e l o a d s u s u a l l y a re n o t d i s t r i b u t e d
ho mo ge neo u sl y u p o n t h e l e n g t h of a p r od uct . T hus , l o cal l y o v er
dimensioned profile areas are the resu lt. In ord e r to avo id these
and he nce re d u ce t h e p r o f i l e wei g ht , ext r usi on di es need t o be
d e v e l o p e d t o o f fer more flex ib ility reg a rdin g th e ach ievab le
pr ofi l e cr oss se ct i ons. It w oul d t h e n be p o ssi bl e t o ma n u fac t ure
p r o f iles with (t ailo red) cro ss sectio n s t h at are lo cally ad ap ted t o
th e actin g l o ad s. D u e t o weig h t r e du ction th ese i n novativ e
pr ofi l e s c o ul d cont ri b u t e t o a red u ct i o n of f u el con s u m pt i o n as
wel l as emi ssi ons of c o m b us t i on gases w h e n b ei n g a p p l i e d f o r
vehicles with combustion engine s. Fu r t h e rmor e, t h e r a nge of
v e h icles with electric d r iv e co u l d b e ex ten d ed by sub s titu tio n
o f co nv en tion a lly ex tru d e d co mp on en ts wit h th ese inno v a tiv e
lo ad ad ap ted tailo red p r ofiles. In ord e r to d e v e l o p th e
pr o duct i o n of suc h e x t ru d e d , mo di fi cat i o ns rega rdi n g t h e
ext r usi o n p r o cess a n d t h e di e t ech n o l o gy hav e been
in v e stig ated , yet mo stly fo r research purpo ses on ly.

18th International Conference Metal Forming 2020

80 Maik Negendank et al. / Pr ocedia Manufacturing 50 (2020) 79–85
2 M. Negendank et al. / P rocedia Manu facturing 00 ( 2 0 1 9 ) 000–00 0

E.g. Makiyam a and Murata [1] varied the cross sectio n of
full pr ofiles ( not hollo w) by appl ying a prototype CNC vari able
vertical section extrusion machine th at allowed the extrusion of
profiles with axial v ariable height along their length. Ju n et al.
[2] appli ed two dies, one fix ed and one moveable in order to
achieve variable cross secti ons on full profiles, as one side
remained a constant shape while the contour of the ot her side
was varied thro ughout th e extrusion pro cess.
Murata et al. [3] applied a ta pered mandrel and varied the
mandrel position and thus the mandrel cross section inside the
die durin g the extrusion proc ess and were able to manufacture
tubes with axial variable wall thicknesses. A similar approach
was investigated by Negendank et al. with the difference that
instead of a tap ered mandrel a stepped ma ndrel was applied [4].
The author s were able to extrude tailored seamless aluminum
alloy tubes with very abrup t as well as with graded wall
thickness t ransitions. The microstructural development al ong
the hollow profiles’ leng ths in regions with different wall
thicknesses was evaluated in [5] and the mechan ical properties
in [6]. Based on a similar appr oach the company Otto Fuchs KG
developed t he manufacture of seamless al uminum tubes/pipes
with axial variable wall thicknesses for drilling applications
(Aludrill™) [7]. Rott [8] also applied an axial moveable
stepped man drel but the t ransition of t he mandrel cross section
was designed with multip le steps. This lead to a better
dimensional stability of the outer tube diameter in the wall
thickness transitio n regions.
For the extrusio n of profile s with mo re complex cross
sections or with multiple hollow pro file chambers a porthole die
needs to be applied. Hence, a wall thickness variation
mechanism fo r a porthole die needed to be developed .
Selvaggio et al. [9, 10] a pplied a mechani sm with move able
bearings for the variation of the outer profile heigh t along the
hollow profile len gth. The gen eral feasibility was shown
successfully since a wall thickne ss variation of up to 0.7mm
was achieved over a profile lengt h of 3m. Negendank et al. also
developed a m echanism for the axial variation of the h ollow
profile wall thickness. In contrast to Selvaggio et al. their
mechanism aimed on the wal l thickness variation base d on
varying t he inner profi le height a nd keep the oute r profil e
dimensio ns const ant. The mechanism ba sed on moveable
segments attached to the mandrel of the porthol e die, that coul d
be move d in vertical di rection to c hange the inne r profile hei ght
and thus the wall thick ness. A maximal wall thickn ess variation
of 1.2mm fo r alumin um alloy EN AW-60 60 (AA6063) [11] and
1.0mm for the magnesium alloy AZ31 [12] was achieved in
experime ntal extrusion t ryouts. But the described de velopment
lacked reliability and reproducibility since billet material flew
into small gaps between the m ov eable segments of the wall
thickne ss variation mecha nism.
For that reason, an alternati ve mechanism was developed.
Numerical investigation s of the material flow and th e required
forces to achieve wall thickness variations were carried out.
First result s are described in this paper.
2. Experimental
Based on the observations of the previo usly developed
mechanism [11 , 12] for wall th ickness variation du ring
extrusion by application o f a porthole die, an alternative
mechanism wa s designed (Fig. 1) . It is mainly based on wedges
with an inclination angle of 10 ° that are positioned beneath
sheet-like bending elements. The we dges are mounted to an
inner mandrel that can be a xially moved in as well as against
the extrusi on direction (E D). The movement is generated b y an
external dri ve consisting of two h ydraulic cylinde rs positioned
beside the porthole die and that transfer their stroke
synchron ously onto a cros s bar. The inner ma ndrel on the ot her
hand is connec ted to the cross bar . Thus, when the cross bar
and hence the wedges are mov ed by the hydraulic cylind ers in
direction oppo site to ED, the bend ing elements will be
deflected towards the die bearing. Subseque ntly, with
increasing displacement of the wedges the deflection of the
bending elements also increases leading to a reduction of the
profile wall thickne ss. On the other hand , when the cro ss bar is
moved in ED, the normal pressure of the billet material in the
die bearing sh ould deflect the be nding elements towards the
mandrel and hen ce increase th e profile wall thickn ess.
Fig. 1. Schematic setup of the wa ll thickness variation mechanism, ED  .

Fig. 2. Geometric model for FEM simulations, ED  .
In order to investigate if th e describe d mechanism would b e
able to achieve th e desired wall thickness variation in ax ial
profile di rection during the extrusion process, an analysi s of the
metal flo w was conducte d using the FE M software code
DEFORM 3D. Du e to process sy mmetry only a 90 ° model was
applied f or the probl em in order t o save solving t ime and disc
space (Fig. 2). The lagra ngian method with a shear friction
factor of m=1 and a heat tra n sfer coefficient of h=11000W/m 2 K
were applied. The billet material w as aluminum alloy EN AW-
6060 and th e material model for flow stress calculation was
contai ner
billet
upper die lower die
ram cross bar
mandrel nose
inner mandrel wedg
e

bending
element
profile
Mo vem ent
extrusion direction �
1.Mandrel  of  upper  die
2.Lower  die
3.W edg e
4.Inner  mandrel
5.Bending  ele ment
6.Outer  bearing  channel
7.Mandrel  nose

Maik Negendank et al. / Pr ocedia Manufacturing 50 (2020) 79–85 81
M. Negendank et al. / P rocedia Manu facturing 00 ( 2 0 1 9 ) 000–00 0 3

applied from an earlier pro ject [1 3]. Fig. 3 displays the t hick-
walled and the thin-walled cross sections th at should be
manufactured within the same extruded profile. It becomes
clear that the wall thickness will only be varied on the upper
and lower p rofile side. Another ai m of the FEM analysis wa s
to estimate the force requiremen ts necessary for the deflection
of the b ending element s during t he extrusio n process and the
additional force required to deform the flowing aluminum billet
material. The bending elements shou ld be manu factured fr om
H13 hot working steel bu t in a non-harden ed condition . In the
hardened state the pressure of the billet material in the die
bearing co uld not be high eno ugh to achieve a deflect ion of the
bending elemen ts into direction of th e initial position . As
material model “H13 machining” was selected from the
DEFORM 3D database and the material be havior was def ined
as elasto-plastic. All compo nents were set to 500°C and the ram
speed was 3mm/s.

In order t o verify the forces gained from the FE M
simulations a simplified test setu p was designed that could be
positioned in th e universal tensio n/compression testing
machine MTS 810. Fig. 4 sh ows the experiment al setup where
the width of bending eleme nts and wedges i s only hal f those
that woul d be appli ed in the extr usion expe riments. The t ests
were conduct ed at T=420°C. At the beginn ing of the test the
wedges were mo ved towards the bendi ng elements with a
velocity of 1mm/min for a maxi mum stroke of 5mm. T he force
(F d ) necessary to deflect the be nding elements was measured.
Afterwards the stroke was reset to 0mm and th e wedges were
pulled out (r emoved) beneath the wedges. The there fore needed
force (F r ) was measured.

Fig. 3. Schematic representation of the two desir ed profile cross sections.

Fig. 4. Test setup for expe rimental determination of required forces for bending
element deflection (a) side view with out furnace (b) front view during testing
at T=420°C.
Finally, afte r all necessary c omponents were manufactu red
extrusion e xperiments were c arried out in o rder to investigat e
the feasibility of axial wall thickness variations with the
developed c oncept. The compone nts of the inner mec hanism
(inside the porthole die) are gi ven in Fig. 5 .
Fig. 5. Inner mechanism for wall thickness variation, ED  .

Fig. 6. Outer mechanism/drive without heating jacket.
The external mech anism is displayed in Fig. 6 and the setup
for the e xtrusion e xperiments i n Fig. 7. T he porthole die was
preheated to 520°C a nd subs equently put into the die holder of
the 8MN extrusion press at t he extrusio n R&D Center at TU
Berlin. Since the die holder did not feature a die heati ng system
the porth ole die was c overed by a heating jacked (T=5 10°C) in
order to redu ce significant die cooling during the installatio n
and connecti on phase of the external dri ve. The EN AW-6060
billets with diameter of 122mm were heated to 500°C in an
induction furn ace. After the extr usion experiments were carried
out, the manufactured profiles were cut and the wall
thicknesses were measured to reveal th eir development in ax ial
profile direction. Th e extrusion ratio for th e thick-walled
(t=4.5m m) profile sect ions was 14:1 an d 23:1 for the cros s
section with red uced wall thick ness (t=2.0mm).

wed ge
wedge
bending
element
mandrel of
porthole die
inner mandrel
mandrel
nose
bending
element

82 Maik Negendank et al. / Pr ocedia Manufacturing 50 (2020) 79–85
4 M. Negendank et al. / P rocedia Manu facturing 00 ( 2 0 1 9 ) 000–00 0

Fig. 7. Experimental extrusion setup, ED  .
3. Results and discussion
The results of the FEM material flow analysis are give n in
Fig. 8 for different stages d uring the process. Fi g. 8a shows the
situation after a pro cessing time of 1.5s w hen the inner mandrel
starts to move in d irection opposite to ED. The b eginning of the
extrude d profile ha d just exited t he die bear ing. In Fig. 8b the
inner mandrel reache d its maximal stroke at a processing time
of 6.0s a nd thus, the wedge forced the bending eleme nt to its
maximal deflection. Hereby the wall thickn ess of the hollow
profile was reduced s uccessfully. In Fig. 8c t he inner mandrel
was moved to its initia l position. It can be noticed that the
bending elemen t was also deflected close to its initial shape
only due to the normal pressure a pplied by t he flowing
aluminum in the region of the die bearing cha nnel.
Subsequently, th e wall thickn ess of the ho llow profile was
successfully decreased and hence a full wall thickness variation
cycle achieved. Thus, the re sults of the FEM material flow
analysis su ggest that the deve loped mechanism sh ould be able
to manufacture hollow profile segments with different wall
thicknesses along the axial pro file direction.
Fig. 8. Results of FEM analysis of material flow, ED  .
The axial force nece ssary to achieve the ma ximal deflection
of the bendi ng element with th e “H13 machining” material
model provide d by the DEFORM 3D material data base was
determined to up to F d =3.4kN in the 90° simulatio n model,
when no aluminum billet material was present. Hence, this
value co rresponds t o F d =13.6k N in a full 360° mod el. On the
other hand, when the flowing billet material is presen t the
necessary force to de flect the bending elem ents and to reduce
the wall thickness of the hollow profile increased to about
F d =55kN (Fig. 9 )
An experime ntal test setup (Fig. 4) was a pplied in order to
measure the necessary force to deflect the be nding elements
(F d ) and thus to verify the force det ermined by FEA. I n a
subsequent second ex periment the necessary force (F r ) to pull
out the wedges beneath the bendi ng elements was mea sured. A
deflection of the bending elemen ts into their initial po sition was
not possible with the simplified test setup. Fig. 10 displays the
load vs. stroke diagram of t he experiments. It was revealed that
a force of up t o F d =11kN was necessary to fu lly deflect the
bending elemen ts (H11 hot work ing steel, not harden ed). This
is comparable to the F d =13.6kN dete rmined by FEA. Up to
F r =3kN were needed i n the expe riment to pull the wedges out
beneath the bending elements . The fluctuations i n the displayed
graph (Fig . 10) are caused by stick- slipping cond itions.
Fig. 9. Force necessary to deflect bending elements and reduce hollow profile
wall thickness during extrusion determined by FEA.
Fig. 10. Load vs. stroke diagram for deflection of bending elements (F d ) and
for removing the wedges beneath the bending elements (F r ).
The extrusio n experiments were carried out in t wo
campaigns. In the first campaign (I) the general feasibility of
the developed mechan ism as well as the influence of the
applied pressure for th e external drive (hydraulic cy linders) on
the maximum deflection o f the be nding elements should be
investigated . The pressure of the two hydraulic cylind ers as
well as the resulting forces of each of the hydraulic cylinders
are given in table 1. Six EN AW-6060 billets were ex truded
during the first campaign. The first billet was extrud ed in order
‐ 11
‐ 10
‐ 9
‐ 8
‐ 7
‐ 6
‐ 5
‐ 4
‐ 3
‐ 2
‐ 1
0
1
2
3
‐ 5 ‐ 4 ‐ 3 ‐ 2 ‐ 1 0123
F_b F_r
strok e [mm]
load [kN]
0
10
20
30
40
50
60
70
80
0123456789
F_inn er_m andrel_ED  [k N]
pr oces s  ti me  [s]
ram
containe r
portho le die  with
heating jacket
hy draulic lines

Maik Negendank et al. / Pr ocedia Manufacturing 50 (2020) 79–85 83
M. Negendank et al. / P rocedia Manu facturing 00 ( 2 0 1 9 ) 000–00 0 5

to fill the porthole die and no wall thickness variation was
attempted. During extrusion of each of the following five
billets the hydrau lic cylinders were driven in extrusion
direction (ED) as well as in direction opposite to ED mu ltiple
times. Fig. 11 shows that the stroke of the hydraulic cylinders
had an in fluence on the ext rusion force . The extrusion force
slightly increased as th e cylinders push ed the crossb ar in
opposite ED aiming on a wall thickn ess reduction and the force
decreased when the cy linders were driven in ED attempting to
increase the wall thickn ess of the hollo w profile. The
development of the wall thickness al ong the length o f the
hollow profile was analyzed on the upper and lower profile s ide
and the results are displayed in Fig. 12.

Table 1. Pressure settings and resulti ng forces for each of the two hydraulic
cylinders.
b

illet no. pressure compression force tension force
[MPa] [kN] [kN]
I.1 0 0 0
I.2 10 15.7 9.3
I.3 16 25.1 14.8
I.4 16 25.1 14.8
I.5 22 35.6 20.4
I.6 25 39.2 23.2

Fig. 11. Extrusion force vs. processing time for extrusio n of billet I.4.

Fig. 12. Axial development of hollow profile wall thicknesses on upper and
lower side of the hollow profile (extrusion cam paign I).

Accordin g to Fig. 12 at the beginning of the profil e (I.1) the
wall thic knesses on the u pper and lower side of the profil e
remained const ant at t=3. 3mm over the pr ofile length si nce no
variation was attempted. During extrusion o f billet I.2 the
external drive was activated multiple times us ing a pressure of
10MPa ( 100bar) for eac h of the two hydraulic cyli nders. The
wall thick ness was found to be incr eased gradua lly to t=3.5mm
in axial profile direction. A wall thickness reduction was no t
observed. For the section of pro file I.3 the wall th ickness on the
upper pr ofile side was fou nd to be increased signif icantly up to
t=5.4mm (Fig.12). On the other hand, the wall th ickness on the
lower profile side slightly decr eased t o t=2.9mm. A section of
profile I.3 with macro scopically visible wall th ickness
variations is given in Fig . 13. In the dis played profi le area, the
wall thickness was first reduced from t=3.3mm to t=2.9mm.
After that reduction the bending element was ripped o ut of its
bearings an d got stuck i n the profil e. Obviousl y, the bulged
profile surface was a result of th at process. Behind the ripped
out bending element th e profile wall thickness increased to
t=4.4mm ( ∆ t=1. 1mm) on the u pper side of t he profile b ut
decreased f rom t=3.3m m to t=2. 9mm ( ∆ t=0.4mm) on the lower
profile si de.

Fig. 13. Wall thickness transition area of on upper side of profile I.3 with
displaced bending element, ED  .

The analysis of the upper die (of the porthole die) re vealed
the reason for the described observations. The alu minum billet
material flew into the opening s between the mandrel nose and
the mandrel and finally lead to plastic deformation of the
mandrel nose (Fig. 14). Due to this deformation the b ending
element on the upper profile side was ripped out of its bearing
and got stuck in th e hollow profile. The deformation oc curred
into direction of the lower profile side, leading to the observed
wall thickn ess reduction on the lower side of the profile and th e
increased wall thickness on the upper side (Fig. 12).
Subsequent parts of the hollow profile (after billet I.3) were
extruded under unspecified condition s, where the material flow
in the die bearing area could have led to local wall thickness
variations wi thout that the aut hors could give a reasonable
explanati on.

Based on the observatio ns of the first extrusion campaign
several modifi cations were appli ed for the second ca mpaign
(II) of extrusion trials. Firstly, the sid e gaps on a newly
manufactured mandr el nose were closed by inserting hardened
(48 HRC) H11 steel plates in order to prevent billet material
from filling these gaps (Fig. 14). In contrast to campaign I the
3,0
3,5
4,0
4,5
5,0
5,5
0,0 2,0 4,0 6,0 8,0 10,0 12,0 14,0 16,0
w al l  th ickn ess  t  [mm]
len gt h  of  hol low  p rofile  [m]
t  up per  pro file  s id e t  low er  pro fil e  s id e
billet  I . 1 bill e t  I.2 billet  I.3 bille t  I. 4 billet  I . 5 billet  I.6
5,05
5,10
5,15
5,20
5,25
5,30
5,35
0 100 200 300 400 500 600 700 800
F  [M N]
ti me  [s]
bend ing ele ment
bulged surf ace
t=3.3mm t=2.9mm t=4.4mm
10mm

84 Maik Negendank et al. / Pr ocedia Manufacturing 50 (2020) 79–85
6 M. Negendank et al. / P rocedia Manu facturing 00 ( 2 0 1 9 ) 000–00 0

experime nts of the second camp aign were conducted with a
hydraulic cy linder pressu re of 25MPa (250bar) . Additiona lly,
two diffe rent geometries of bending elements were
manufactured. The first set of bending elements feature d a
reduced cross section of 0 .5mm instead of 2.0mm as appli ed in
campaign I. T he lower cross s ection was suppos ed to improve
the bendability o f the bending elements, esp ecially when th ey
need to be deflected into d irection of the initial position for
manufacture of a n increased wa ll thickness. During ex trusion
of billet II.1 it was ob served that the bend ing elements broke
right at the start and got stuck in front of the prof ile.
Fig. 14. Deformed bending element and deformed mandrel nose also filled with
aluminum after initial etching for die cleaning with NaOH.
Fig. 15. Adjustments of the inner mechanism for the second extrusion
campaign.

For the billets II.2 to II.4 bending elements with the initial
thickne ss of 2.0mm were a pplied again, but in contras t to
campaign I thei r edges towards the mandrel were rounded a bit
as indicated in Fig. 15. The rounded edges were applied in
order to achieve the wall thickness variatio ns not only b y
plastic de formation of the be nding element s but partly through
their slight ro tation as illustrated in Fig. 15. Fig. The results of
the second campaign regarding the develo pment of the wall
thickne sses in axial profil e direction are gi ven in Fig. 16 .
Accordingly, the wall thicknesse s were successfully reduced
during extru sion of billet II.2 from t=3.8mm to t=3.27mm on
the upper profile side and fro m t=3.6mm to t=2.9mm on the
lower side of the hollow profile. Although the hydrau lic
cylinders were driven ba ck and forth multiple time d uring
extrusion of billet II.2 no reduction of the wall thicknesses was
observed. Instead the seam welds on b oth sides of the hollow
profile we re found to be separate d starting at a profil e length of
0.5m to 2.5m and t he profile surfaces were extremely wa ved in
this profile section. The reason for the profile separations was
found at t he end of the separations since the H11 plates stuck
in the side walls cutting the pro file open.
Fig. 16. Axial development of hollow profile wall thicknesses on upper and
lower side of the hollow profile (extrusion cam paign II), ED  .

Obviously, aluminum billet material was able to first
dislocate the H11 plates so that they sliced th e profile sides
open. The n the H11 plates we re squeezed out. Afterwards the
profile seams on the si des were welded correctly again. At the
end of the extrus ion of billet II.2 the wall thicknesses
drastically in creased from t=3.3 mm to t=6.0m m on the upp er
profile side and from t=2. 9mm to t= 4.9mm on the lower side
(Fig. 16) . Subsequent observat ions of the pr ofile in that sect ion
found t hat both bendin g elements were rippe d out of thei r
bearings in this region (Fig . 17). Additionally, as previously
observed for profile I.3 (F ig.13) bulges formed again on the
profile su rfaces where the bending eleme nts got stuc k. Fig. 18
visualizes the development of profile wall t hicknesses in this
specific profile section between billets II.2 and II.3 more
closely. The wall thickn ess on the lower profile side first
decreased from t=3.1mm to t=2.4mm at a prof ile length of
about 2.5m. Th is hints to the conc lusion that the profile wall
thickness was varie d successfully by the develope d mechanism
in this case. Afterwards, an in crease to t=4.2mm was observed.
But at a profile length of abou t 2.6m the lower bending element
was ripped out of its bearings. The increased wall thickness of
up to t=4.7mm seemed to correspond ing with that. Until the
end of the extrusion the wall thickness then remained constant.
On the upper side of the profile the wall thickn ess increased
significantly from t=3.2mm to t=5.6mm a t a profile length of
2.49m (Fi g. 18). Later it further increased up to t=6.0mm This
increase was found to correspond with the loss o f the upper
bending elemen t. The displayed d ecrease in wall thickness at a
profile length of 2.63m took place as the bending element on
the lower side of the profile was displaced. Hence, these later
wall thickne ss variations were induced by the lo ss of the
bending elem ents as well as subsequent va riations of t he
material flow and not due to the activation of the developed
wall thickness variation mechanism.

aluminum
filled ga p
inner m andrel
without wedges
mandrel of porth ole die
bendi ng elemen t
defor med
mandrel nose
2,0
2,5
3,0
3,5
4,0
4,5
5,0
5,5
6,0
0,0 1,0 2,0 3,0 4,0 5,0 6,0 7,0
wal l  thickn ess  t  [mm]
pr of ile  lengt h  [m]
t  u ppe r  pro fi l e  s ide t  lowe r  pr of i le  side
b illet  II.2 b i llet  II.3 b ill et  II.4
mandrel nose
H11 ‐ plate 
(48HRC)
bendin g element
mandrel of por thole di e
rounded edge
wedge inserted
rot ation of
bending elem ent

Maik Negendank et al. / Pr ocedia Manufacturing 50 (2020) 79–85 85
M. Negendank et al. / P rocedia Manu facturing 00 ( 2 0 1 9 ) 000–00 0 7

Fig. 17. Section of transition area between billet II.2 an d II.3 with visible wall
thickness variation and displaced bending elements, ED  .
Fig. 18. Axial development of hollow profile wall thicknesses in transition
area between billets II.2 and II.3, ED  .
Conclusions
A mechanism for the wall thick ness variation of lightweight
hollow profiles by ap plying moveabl e segments in a porthole
die was de veloped. Wall thickness variations s hould be
achieved throug h bending elements integrated into the porthole
die. FEA of material flow indicated the principle feasibility of
the mechanism. Experime ntal extrusion trials p roved the
functionality o f the extern al wall thickness variation
mechanism, meaning that the force of the two hydraulic
cylinders was successfully transf erred via a cross bar to an
inner mand rel. The functionali ty of the inner mecha nism which
consiste d of wedge pl ates that were mounted ont o the inner
mandrel and s hould induce the strain of the bending ele ment
could not yet be proven on a reliable and reproduceable basis.
In the e xperimental t ryouts alumi num bill et material wa s
squeezed into even the s mallest gaps of the inner mechanism
leading to the displacement of bending elements an d other
components.
Future develop ments will focus on improving th e support
and the bearings of the bending elements as well as on a
constructive solution th at does not feature any voids o r gaps
where the billet material could flow in and block or destroy the
wall thickness variation mechanism or its components.
References
[1] Makiyama T, Murata M. A technical note on the development of prototype
CNC variable vertical section extr usion machine. J Mat Proc Tech
2005;159:139- 44.
[2] Jun L , Xiangsheng X, Quiang C. An investigation of the variable cross-
section extrusion process. I nt J Adv Manuf Tech 2017;91:45 3-61.
[3] M akiyama T, Murata M. Controlling inside diameter of circular tube by
extrusion. Mat Sci Forum 2002;396- 402:513-20.
[4] Negendank M, Mueller S, Reim ers W. Extrusion of aluminum tubes with
axially graded wall thickness and mechanical characterization. Procedia
CIRP 2014;18:3-8.
[5] Negendank M, Taparli UA, Mueller S, Reime rs W. Microstructural
evolution of indirectly extruded se amless 6xxx aluminum tubes with axial
variable wall thickness. J Ma t Proc Tech 2016;230:187-97.
[6] Negendank M, Taparli UA, Mueller S, Reimers W. Extrusion of tailore d
seamless aluminum tubes with axial variable wall thickness and
characterization of mechanical properties. Proceedings of the 11 th
International aluminum extrusi on technology seminar 2016;1:801-10.
[7] Fuchs O, Tailored aluminum tubes – extruded tubes with vari able wall
thicknesses. Int Aluminium J 2013;8 9(10):35-6.
[8] Rott A. Aluminium seamless pipe e xtrusion with variable wall thickness.
In: Tekkaya AE, Jäger A, editor s. ICEB-International Conference on
Extrusion and Benchmar k Conference Proceedings Advances in hot
extrusion and simulation and 5 th extrusion benchmar k; 2013. p. 104-107.
[9] Selvaggio A, Chatti S., Khalifa NB, Tekkaya AE. New developments in
extrusion of profi les with variable curvatures and cross-sections. In:
Proceedings of the 11 th International aluminum extrusion technology
seminar 2012;1:505- 12.
[10] Selvaggio A., Haase M, Khalifa NB, Tekkaya AE. Extrusion of prof iles
with variable wall thickness. Procedia CIRP 2014;18:15-20.
[11] Negendank M, Mueller S. Strangpressen von Aluminiumhohlpr ofilen mit
axial variabler Wandstärke. In: Kraly A, Chimani CM, Uggowitzer PJ,
editors. Hochleistungsmetalle und Proze sse für den Leichtbau der Zukunft,
ISBN-13: 978-3- 902092-10-6; 2018. p. 62-73.
[12] Negendank M, Sanabria V, Muel ler S, Reim ers W. Extrusion of
magnesium alloy hollow profiles with axial variable wall thickness. AIP
Conference Proceedings 2019;2 113:030002.
[13] Sanabria V, Mueller S, Reim er s W. Friction modelling in long bearing
channels during multi-hole extrusion of aluminium alloy. Mate rials Today
2015;2:4820- 8.

2,0
2,5
3,0
3,5
4,0
4,5
5,0
5,5
6,0
2,45 2,50 2,55 2,60 2,65 2,70 2,75
wal l  th i ckn ess  t[mm ]
pr of ile  l en gth  [m]
t  u ppe r  pro fi l e  s ide t  lowe r  pr of i le  side
b illet  II. 2 b illet  II.3
bending eleme nt
bending eleme nt
lower profile side
upper profile side
5cm
increase of
wal l  thickness
decrease of
wall  thickness
1 st  increase of
wal l  thick ness
2nd  increase of
wall  thickness

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