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Study of dynamic behaviour via Taylor anvil test and structure observation of M300 maraging steel fabricated by the selective laser melting method

Abstract

This paper deals with the M300 high strength maraging steel fabricated via selective laser melting method. Mechanical properties especially microhardness and compressive yield strength of maraging steel in as-printed state were observed. The acquired data was implemented in Johnson-Cook constitutive equation used for numeric simulation, which showed the satisfactory correlation with the observed experiment. Dynamic behaviour under high strain rate (impact velocity reached 185 m.s-1)- 1 ) was investigated via Taylor Anvil Test. The experiment revealed structure and geometrical changes accompanied with the creation of characteristic funnellike and cylindrical areas on the deformed sample. Impacted sample forehead featured the increase of micro- hardness (465 HV) accompanied with structure changes. The structure in the funnel-like area exhibited the decrease of average grain size, which reached the minimum (3.1 mu m) in the vicinity of the impacted forehead. Closer analysis revealed that the high strain rate caused the increase of high fraction high-angle grain boundaries (50,8 %) and higher geometrically necessary dislocation density (52.77 1.m-- 2 ) in the funnel-like area.

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Study of dynamic behaviour via Taylor anvil test and structure observation of M300 maraging steel fabricated by the selective laser melting method

Author: Kolomý, Štěpán; Jopek, Miroslav; Sedlák, Josef; Zouhar, Jan
Publisher: Elsevier
Year: 2024
DOI: 10.1016/j.jmapro.2024.07.057
Source: https://dspace.vut.cz/bitstreams/8ea92650-e929-4bb0-967a-69e1b462656d/download
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
A ailable online 20 July 2024
1526-6125/© 2024 The Au ho s. Published by Else ie L d on behal o The Socie y o Manu ac u ing Enginee s. This is an open access a icle unde he CC
BY-NC-ND license (h p://c ea i ecommons.o g/licenses/by-nc-nd/4.0/).
S udy o dynamic beha iou ia Taylo an il es and s uc u e obse a ion
o M300 ma aging s eel ab ica ed by he selec i e lase mel ing me hod
S epan Kolomy , Mi osla Jopek
*
, Jose Sedlak, Ma ek Benc, Jan Zouha
B no Uni e si y o Technology, Facul y o Mechanical Enginee ing, B no, Czech Republic
ARTICLE INFO
Keywo ds:
Ma aging s eel
Taylo an il es
Selec i e lase mel ing
Johnson–cook
High s ain a e
Mic oha dness
S uc u e
ABSTRACT
This pape deals wi h he M300 high s eng h ma aging s eel ab ica ed ia selec i e lase mel ing me hod.
Mechanical p ope ies especially mic oha dness and comp essi e yield s eng h o ma aging s eel in as-p in ed
s a e we e obse ed. The acqui ed da a was implemen ed in Johnson-Cook cons i u i e equa ion used o
nume ic simula ion, which showed he sa is ac o y co ela ion wi h he obse ed expe imen . Dynamic beha -
iou unde high s ain a e (impac eloci y eached 185 m.s
−1
) was in es iga ed ia Taylo An il Tes . The
expe imen e ealed s uc u e and geome ical changes accompanied wi h he c ea ion o cha ac e is ic unnel-
like and cylind ical a eas on he de o med sample. Impac ed sample o ehead ea u ed he inc ease o mic o-
ha dness (465 HV) accompanied wi h s uc u e changes. The s uc u e in he unnel-like a ea exhibi ed he
dec ease o a e age g ain size, which eached he minimum (3.1
μ
m) in he icini y o he impac ed o ehead.
Close analysis e ealed ha he high s ain a e caused he inc ease o high ac ion high-angle g ain bounda ies
(50,8 %) and highe geome ically necessa y disloca ion densi y (52.77 1.m
−2
) in he unnel-like a ea.
1. In oduc ion
Addi i e manu ac u ing (AM) is he p ocess o c ea ing a pa based
on a digi al model c ea ed ia Compu e Aided Design (CAD) so wa e.
In AM, ma e ial is g adually added (laye by laye ), while in machining,
ma e ial is g adually emo ed. The pa is inally o med by sin e ing
indi idual laye s o a de ined hickness, which a e s acked on op o each
o he [1]. This echnology enables p oduc ion o complex shapes ha
would no be possible o p oduce by con en ional me hods [2,3]. AM is
used and ep esen ed in se e al sec o s such as he au omo i e and
ae ospace indus ies. I could also ind i s applica ion in heal hca e and
ashion [4–6]. AM enables o manu ac u e a ious ypes o ma e ials,
such as ool s eel [7] s ainless s eel 15-5PH [8] and 316 L s eel [9–11],
Inconel 718 [12–14], Ni alloy [15], Ti alloy [16,17] o Al alloy [18,19],
whose s uc u e and mechanical p ope ies can di e depending on he
p in ing pa ame e s, s a egies, hea ea men , e c. [20,21].
Gene ally, he beha iou o mos ma e ials unde dynamic loading is
di e en han unde s a ic/quasi-s a ic loading [22,23]. Machine com-
ponen s such as gea boxes, c anksha s e c. a e subjec ed o dynamic
loading dec easing hei li e. The use o dynamic es s p o ides a ma-
e ial assessmen , which helps o design new componen s. Dynamic es s
will ob ain inpu s in o he ma e ial models, which can be used o
nume ic simula ion. The simula ion p o ides eal esul s, which can be
used in he design o machine componen s. The me hods, which can be
used o e alua e dynamic p ope ies o he ma e ial a e he Spli Hop-
kinson P essu e Ba (SHPB) me hod and he Taylo An il Tes (TAT)
o en pe o med o gain ha dening beha iou s o nume ous alloys a
ul a-high s ain [24]. TAT can also be used in e e se mode o e alua e
he esponse o he ma e ial o dynamic loading o can be used in bal-
lis ics es s [25]. Using he esul s o he dynamic p ope ies in p ac ice
could lead o a be e , mo e accu a e and as e design o a machine
componen [26].
Many s udies and a icles ocused on he in es iga ion o he dy-
namic p ope ies o ma e ials. Rua e al. [27] s udied composi es wi h
epoxy esin polyme ma ix. The mic os uc u e o he es samples we e
in es iga ed using scanning elec on mic oscopy. Dynamic es s o he
ma e ial we e pe o med using he SHPB es , which p o ided s ess-
s ain cu es o di e en s ain a es. Lu and Li [28] in es iga ed he
dynamic beha iou o polyme s a high s ain a es using he SHPB. The
expe imen ally measu ed dependence o s ess on s ain o di e en
s ain a es is subsequen ly implemen ed in o he dynamic cons i u i e
Johnson-Cook equa ion including he e ec o s ain a e and empe -
a u e. Gilbe son [29] in es iga ed he dynamic p ope ies o wood
using he SHPB. The de o ma ion o he sample was measu ed by s ain
* Co esponding au ho .
E-mail add ess: [email p o ec ed] (M. Jopek).
Con en s lis s a ailable a ScienceDi ec
Jou nal o Manu ac u ing P ocesses
jou nal homepage: www.else ie .com/loca e/manp o
h ps://doi.o g/10.1016/j.jmap o.2024.07.057
Recei ed 21 Ma ch 2023; Recei ed in e ised o m 15 Ap il 2024; Accep ed 10 July 2024
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
284
gauge and digi al image analysis. SHPB has been ound o be a use ul
ool o assessing he ma e ial p ope ies o wood subjec ed o high
s ain a es o sho loading imes. Chen e al. [30] in es iga ed he
dynamic p ope ies o specimens made om conc e e. Tes ing was
pe o med using The SHPB o di e en loading angles and di e en
impac eloci ies. Fo lowe impac eloci ies, he s ess-s ain cu e
ea u ed a simila cou se o quasi-s a ic loading, in which he ini ial
c ack occu s in he cen e o he specimen and p opaga es ou wa d.
Impac eloci y has a signi ican ole in e ms o local s ess dis ibu ion
in he sample. Kang e al. [31] compa ed he dynamic p ope ies o shale
and g ani e. Dynamic p ope ies we e e alua ed using SHPB. They
ound ha dynamic loading educed he impac s eng h. Renliang e al.
[32] in es iga ed he dynamic beha iou o sands one ia he SHPB. The
empe a u e o he samples was main ained a −15 ◦C du ing he
expe imen . The es esul s e ealed ha when he a e age s ain a e
was low, he sample s eng h changed g adually bu when i was high,
i s s eng h changed apidly. Li, Xu, Chen e al. [33] in es iga ed he
dynamic p ope ies o coal samples subjec ed o di e en impac e-
loci ies. They obse ed an ob ious s ain a e e ec on he dynamic
s eng h o specimens, which exhibi ed c acks unde de ined impac ed
angle, a ec ing s ess concen a ion in specimens and changed hei
dynamic beha iou .
High demands on he high-se ies p oduc ion o such componen s,
which a e ypically manu ac u ed om Fe ma e ial by au oma ic
sequen ial machines, which can p oduce componen s a s ain a es up
o 10
3
s
−1
. To ensu e success ul indus ial p oduc ion he mapping o
dynamic beha iou o he used ma e ial is c i ical. Liu e al. [34] used
SHPB o he in es iga ion o U71Mn s eel (used o ails) he dynamic
p ope ies o e a wide ange o s ain a es and empe a u es. Johnson-
Cook models we e de e mined ega ding his ma e ial based on he
expe imen al da a. Jopek [35] in es iga ed he dynamic beha iou o
TRISTAL low ca bon s eel using he TAT. The expe imen was pe o med
on a de ice in he labo a o y o high de o ma ion a es a he Facul y o
Mechanical Enginee ing in B no. The LS DYNA p og am was used o
simula e he mechanical beha iou o TRISTAL s eel unde dynamic
loading. Kuncicka e al. [36] showed he esul s o he impo an pa-
ame e s implemen ed in Johnson-Cook cons i u i e equa ion o TRIS-
TAL s eel. Nume ic simula ion con i med a sa is ac o y co ela ion wi h
expe imen ally obse ed da a.
The s udy o dynamic beha iou o ma e ials p oduced by he 3D
p in ing me hod ha e been add essed by se e al s udies. Zhang e al.
[37] in es iga ed he dynamic p ope ies o 3D-p in ed ce amics. Due o
di e en s uc u es o AM pa compa ed o adi ionally manu ac u ed
he di e ences in dynamic beha iou was obse ed. Sha ma e al. [38]
in es iga ed he e ec o p in ing pa ame e s on he dynamic beha iou
o polyamide samples p oduced by he selec i e lase mel ing (SLM)
me hod. S o age modulus inc eases as he lase powe , bed empe a u e
and scan leng h inc eased while i dec eased wi h he inc ease in he
scan spacing. Mansou e al. [39] in es iga ed he dynamic p ope ies o
PLA ma e ial samples p oduced ia FDM echnology. A ew samples
we e ein o ced wi h g aphene and subsequen ly subjec ed o dynamic
es s. The esul s showed ha he inco po a ion o g aphene imp o ed
he elas ic modulus, s eng h, and ha dness o he 3D p in ed samples.
S udies [40,41] in es iga ed he dynamic beha iou o Ti-6Al-4 V
samples ab ica ed by AM. The esul s ob ained h ough nume ic
simula ion showed a linea ela ionship wi h expe imen ally ob ained
esul s. Dynamic-mechanical p ope ies o AM AlSi10Mg aluminium
alloy we e in es iga ed ia SHPB o gain s ess-s ain cu es. Di e ences
in he dynamic p ope ies o his alloy p oduced wi h di e en ma e ial
o ien a ions accompanied wi h aniso opic p ope ies we e obse ed
[42–44]. A se ies o TATs we e pe o med on addi i ely (by SLM) and
con en ionally manu ac u ed 316 L s ainless s eel samples. A di e ence
in dynamic p ope ies was obse ed be ween e ical, ho izon al (SLM)
and con en ionally manu ac u ed specimens [45,46]. Resea che s
[47,48] es ed AM as-buil ma aging s eel specimens, which we e sub-
jec ed o dynamic loadings o in es iga e he dynamic beha iou ,
de o ma ion mechanisms, mic os uc u al and ex u e e olu ion ia
SHPB. Resul s showed, as-buil samples exhibi ed ac u e a he s ain
a e o 3500 s
−1
.
Ma aging s eel p oduced by AM is no pe ec ly known in ega d o
he dynamic beha iou . No many exis ing s udies we e ocused on
dynamic in es iga ion o M300 ma aging s eel ab ica ed ia SLM. The
aim o his s udy is o analyse he dynamic beha iou o M300 ma aging
s eel ia Taylo an il es . Mechanical p ope ies especially comp essi e
yield s eng h and mic oha dness in as-p in ed s a e we e e alua ed o
gain he in o ma ion abou he ma e ial model, which is implemen ed
in o he Johnson-Cook cons i u i e equa ion and subsequen ly used o
nume ic simula ion. The Real expe imen is accompanied wi h he
ollowing analysis e ealing a se e e s uc u e change. C ys allog aphic
ex u e, a e age g ain size, high angle g ain bounda ies and geome i-
cally necessa y disloca ion densi y a e desc ibed in de ail.
2. Expe imen al p ocedu e
Me al powde o he M300 ma aging s eel was used o p oduce he
samples. Fou a ious ypes o samples, which we e used o di e en
ypes o analysis we e ab ica ed ( ypes o samples a e lis ed in Table 1).
Fu he mo e, he chemical composi ion o as-p in ed sample ( ype 1)
was de e mined using he Q4 TASMAN (B uke , Rudice, Czech Repub-
lic) de ice. The gained chemical composi ion o his sample (p esen ed
in Table 2) complied wi h he i gin chemical composi ion o powde
p o ided by he p oduce . Cylind ical samples o es ing we e ab i-
ca ed using he RENISHAW RenAM 500E (RENISHAW, New Mills, UK)
3D p in e . Meande Ha ching Pa en s a egy wi h 67◦ o a ion a e
each laye was used o ab ica ion o he samples (see Fig. 1a). The
s a egy p o ides su icien mel ing p ocess, which exhibi s low po osi y
and o ma ion o a a ou able s uc u e [49]. Sample po osi y ( ype 2)
was e alua ed by op ical mic oscope Olympus DSX500, which was used
o scan he su ace o he sample. The building di ec ion (BD) was
di ec ed o he Z axis ( e ical di ec ion). P ocess pa ame e s used o
ab ica ion a e lis ed in Table 3. The eq. (1) [50,51] was used o he
calcula ion o he ene gy densi y, which was se du ing he building
p ocess.
E=P
h (1)
whe e E is lase ene gy densi y (J.mm
−3
), P is lase powe (W), is
scanning speed (mm.s
−1
), h is ha ch spacing (mm) and is laye hick-
ness (mm).
Mic oha dness o he samples ( ype 3) was measu ed in as-p in ed
s a e. Mic oha dness measu emen was pe o med in wo a ious di-
ec ions i.e. ho izon al and e ical, using load o 200 g and dwell ime
10s. To gain he comp essi e yield s eng h, necessa y machining
ope a ion was ca ied ou . Bo h aces o he sample we e no pe ec ly
la a e ab ica ion ( he e was a suppo on he i s ace and he second
ace was no la ). Pos p ocess ace u ning b ough a ou able su ace
quali y on bo h aces. Subsequen ly he samples we e placed in o a
special ix u e, which was used o comp essi e es and we e p essed a
he cons an speed 10 mm.min
−1
a he oom empe a u e 22 ◦C±1.
Machine wi h an EDC 60 (B no, Czech Republic) con ol uni was used
o comp essi e loading. Fo da a acquisi ion he TIRA es .2.1 so -
wa e was used. S ess–loga i hmic s ain cu es we e de e mined om
acqui ed da a.
Table 1
Types o di e en samples used o di e en ype o analysis.
Type Analysis s a e amoun [−]
1 Chemical composi ion as- ab ica ed 1
2 Po osi y e alua ion as- ab ica ed 1
3 Tes ing o mechanical p ope ies as- ab ica ed 8
4 Dynamic es ing as- ab ica ed 1
S. Kolomy e al.
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
285
Tes o dynamic beha iou ia TAT ook place in he labo a o y o
high s ain a es a he Facul y o Mechanical Enginee ing BUT in B no.
The de ice used o es ing o he dynamic p ope ies is shown in Fig. 2a.
The sample ( ype 4) oge he wi h he ca ie (see Fig. 2b) is placed in
he ai essel om whe e he sample was i ed owa ds he ixed ba .
Imminen ly he sample was sepa a ed om he ca ie , he impac e-
loci y was measu ed. The impac eloci y eached max. Value o 185 m.
s
−1
in his expe imen . Fig. 2c shows ini ial dimensions o he sample
used o dynamic es ing, whe e L
0
is he leng h o he sample and D
1
and
D
2
a e diame e s on bo h sample aces. Fig. 2d ep esen s ma e ial model
wi h he key pa ame e s (L
= inal leng h, X =leng h o non-de o med
a ea, L =leng h o de o med a ea, D1 =diame e o non-de o med
cylind ical a ea, D
max
=max. Diame e a e de o ma ion) subse-
quen ly in eg a ed in he nume ic simula ion.
De ailed s uc u e obse a ion o sample a e TAT, which was p e-
pa ed by puck cas ing and au oma ically polished and e ched by 2 %
ni al solu ion was examined. Mic oha dness o de o med sample was
measu ed in YZ plane (see Fig. 1b) along and pe pendicula o sample
axis (see Fig. 1c). The s uc u e was obse ed in he YZ plane using he
Olympus DSX500 (Olympus, P ag, Czech Republic) ligh mic oscope
and he KEYENCE VHX-F (KEYENCE, Mechelen, Belgium) digi al mi-
c oscope. Tescan Ly a 3 XMU FEG/SEMxFIB (Tescan, B no, Czech Re-
public) wi h Symme y EBSD de ec o was used o de ailed s udy o he
mic os uc u e. The scan s ep o he EBSD (elec on-backsca e )
scanning was 0.15
μ
m.
Nume ical simula ion o TAT was ealised using so wa e ANSYS
Explici dynamic (Ansys Inc., Canonsbu g, Pennsyl ania, USA). Hexag-
onal mesh was applied o e alua e he sample a e TAT ia ini e
elemen me hod (FEM). Close o 270 housand elemen s wi h 308
housand nodes we e implemen ed o he de ail de ini ion, wi h no
applied e-meshing. The s a ing empe a u e was se as 22 ◦C. The TAT
nume ical simula ion was ca ied ou using Johnson-Cook (J–C) eq. (2).
Each pa ame e om he equa ion was de e mined expe imen ally and
compa ed o pa ame e s acqui ed by he nume ic simula ion.
σ
= (
σ
0+Bφn) • ⎛
⎝1+Cln
˙
φ
˙
φ0
⎞
⎠• (1−T*m)(2)
whe e
σ
0
is s a ic low s ess, B is wo k ha dening coe icien , ˙
φis s ain
a e, n is wo k ha dening exponen , C is s ain a e sensi i i y, m is he
he mal so ening coe icien , and T* is homological empe a u e
de ined in he ange 0 <T* <1 by eq. (3)
T*=T−T0
Tm−T0
(3)
whe e T
0
is he e e ence empe a u e (a s a ic low s ess
σ
0
=
σ
), and
T
m
is he mel ing empe a u e.
3. Resul s and discussions
The p ocess o 3D p in ing is based on he concep o placing each
laye by laye un il he whole pa is ab ica ed. Di ec p in ed su ace is
depic ed in Fig. 3.Fig. 3a shows he on iew o he as-p in ed sample
whe e he ha ching pa hs a e clea ly isible. Dis ance be ween each pa h
is app oxima ely equal o 0.095 mm (ha ch spacing). Fig. 3b shows he
side iew o he p in ed sample. This su ace ea u ed a non-su icien
su ace quali y a e p in ing. The co e laye o p in ed samples con-
ains plen y o mic opo es and oids, which can nega i ely a ec dy-
namic and mechanical p ope ies [52]. The e o e, i is needed o
machine su aces, which a e conside ed o be unc ional.
AM echnology especially SLM can p oduce nea ly ully dense and
high-pe o mance pa s o a e y complex shape [53]. The combina ion
o implemen ed p ocess pa ame e s could a ec he o ming s uc u e
and he po osi y [54]. Po es, ca i ies, o oids could appea due o he
p o ec ing gas, which is en apped du ing he sin e ing p ocess [55,56].
S uc u e, which epo s lowe po osi y would ea u e highe a igue
esis ance and mechanical p ope ies [57]. Po osi y was examined on
Table 2
Chemical composi ion o es ed sample.
Elemen Ni Co Mo Ti Si Mn C P Fe
Q4 TASMAN [W %] 18.38 8.84 4.67 0.71 0.01 0.04 0.02 0.02 66.40
Fig. 1. (a) Meande Ha ching Pa en 67
◦ o a ion a e each laye and (b) C oss-
sec ion plane depic ed in he sample subjec ed o TAT and (c) lines 1–3 used o
mic oha dness measu emen and places I-III in YZ plane used o s uc u e
obse a ion.
Table 3
P ocess pa ame e s used o ab ica ion o he samples.
Ene gy
densi y [J/
mm
3
]
Lase
powe [W]
Scanning speed
[mm/s]
Lase
hickness
[mm]
Ha ch
spacing
[mm]
133 410 810 0.04 0.095
Fig. 2. (a) De ice used o es ing o dynamic p ope ies ia TAT, (b) assemble
con ains o sample and ca ie and ma e ial model (c) be o e de o ma ion (d)
a e de o ma ion.
S. Kolomy e al.
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
286
he sample ( ype 2 men ioned in Table 1), which was ab ica ed wi h
iden ical p ocess pa ame e s. Po osi y was e alua ed in ho izon al (see
Fig. 4a) and e ical di ec ion (see Fig. 4b). Th ee indi idual planes in
each di ec ion (pe pendicula and pa allel o BD) we e chosen. The
planes we e si ua ed on op, in middle heigh and in he bo om o he
sample. These planes we e sepa a ely scanned on op ical mic oscope
Olympus DSX500. Po osi y o he sample is calcula ed as a e age alue
om each single e alua ed plane (see Table 4). Fig. 4 shows he mic o
and mac o po es, which a e si ua ed dominan ly in co e laye o he
sample. In case o emo al he co e laye (0.4 mm om su ace) he
global po osi y would dec ease d ama ically. The po osi y was also
e alua ed wi hou conside ing he co e laye , which b ough he sig-
ni ican educ ion o po osi y.
3.1. Mechanical p ope ies
The as-p in ed samples ( ype 3 co esponding o Table 1) we e used
o he mic oha dness e alua ion. Fou indi idual samples we e
measu ed o de e mine mic oha dness in ho izon al (pe pendicula o
BD) and e ical (pa allel o BD) di ec ions, which is depic ed in Fig. 5.
The middle heigh plane was used o measu e mic oha dness in
ho izon al di ec ion due o he expec a ions o he highes po osi y
connec ed wi h lowe mic oha dness [58]. The esul ing alues o
mic oha dness a e gi en as he a e age alues calcula ed om 12 in-
den a ions in each di ec ion. A e age mic oha dness in ho izon al and
e ical di ec ion ea u ed o 411 HV and 410 HV espec i ely. I could
be concluded; he mic oha dness is independen on i s measu ing
di ec ion.
Bo h aces o as-p in ed samples ( ype 3) we e no pe ec ly la a e
ab ica ion. The i s ace o he sample ea u ed a building suppo , and
he second ace did no exhibi wi h an app op ia e su ace quali y. Face
u ning p o ided a a ou able su ace quali y, which ensu ed he su i-
cien condi ions o comp essi e es ing. The comp essi e s ess –log-
a i hmic s ain cu es o he examined samples a e shown in Fig. 6. The
di e en comp ession s oke was applied, which a ied o each sample:
sample 1 ea u ed he 6 mm s oke, sample 2 was exposed o 7 mm
comp ession s oke, sample 3 and sample 4 we e exposed o 8 mm and 9
mm comp ession s oke. Due o he a ious comp ession s oke he
imposed loga i hmic s ain was di e en o each sample. The a e age
Fig. 3. Su ace quali y in as-p in ed s a e: (a) on iew on SLM piece and (b) side iew.
Fig. 4. Ligh op ical mic oscopy (LOM) images show po osi y (c oss-sec ion in
middle heigh ) in (a, b) ho izon al di ec ion and (c, d) e ical di ec ion, (a–d)
co esponds o sample ype 2 acco ding o Table 1.
Table 4
E alua ed po osi y o he sample in ho izon al a e ical di ec ion.
SAMPLE Type 2 Po osi y in ho izon al
di ec ion [%]
Po osi y in e ical di ec ion
[%]
Sec ion 1 2 3 1 2 3
Unbounded a ea 0.161 0.180 0.170 0.160 0.150 0.190
Bounded a ea 0.022 0.025 0.031 0.025 0.023 0.029
Fig. 5. Mic oha dness o ou di e en samples in as-p in ed s a e. Mic o-
ha dness is gi en in ho izon al and e ical di ec ion.
S. Kolomy e al.
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
287
comp essi e yield s eng h calcula ed om all samples ea u ed 1177 ±
5 MPa. Addi i e manu ac u ed pa should wi hs and he highe
dynamical load he highe mechanical p ope ies, he pa exhibi ed
[59]. The inal dimensions ( inal heigh , maximal and minimal diam-
e e ) o comp essed samples we e impu ed in o nume ic simula ion o
pe o m dynamic beha iou .
3.2. Dynamic es ing
Dynamic beha iou o he sample ( ype 4) was examined using he
TAT de ice. Dimensions o es ed sample in unde o med s a e we e
measu ed and subsequen ly used o inal e alua ion as well as he di-
mensions a e de o ma ion. U ilisa ion o acqui ed pa ame e s led o
e alua ion o dynamic beha iou ia FEM. Impac eloci y was 185 m.
s
−1
, which in lic ed uni o m plas ic de o ma ion depic ed in Fig. 7.
De o med sample can be di ided in wo cha ac e is ic a eas i.e., unnel-
like, and cylind ical a ea. The i s a ea was exposed o high s ain a e,
which led in c ea ion o he unnel-like a ea, co esponding o se e e
plas ic de o ma ion. The c ea ion o unnel-like a ea ins ead o ba el (in
case o comp essi e es ) p o ed ha he sample was exposed o high
s ain a e (dynamic loading) and was no in luenced by he ic ion. The
second a ea was de ined as unde o med cylinde wi h he ini ial diam-
e e . The ac , ha any mac o c acks we e obse ed, can be a ibu ed o
low impac eloci y. Highe impac eloci y can cause des uc ion o he
sample due o c acks ini ia ion [29]. The nex ac o , which can a ec
de o ma ion could be impu i y, oids, po es e c., con ained in co e
laye , which can lead o c ack ini ia ion and apid des uc ion o he
sample [60].
The sample a e high s ain a e was obse ed ia scanning elec on
mic oscopy (SEM). SEM was used o de ail scan o a eas con aining
de ec s on he impac ed egion o he sample, which is depic ed in Fig. 8.
The uni o m plas ic de o ma ion o he sample o ehead (depic ed in
Fig. 8a) con ained a huge numbe o aces equally sp ead in whole a ea.
Fig. 8b showing he de ail a ea con aining isible impu i ies ma ked in
yellow ci cle wi hin his a ea. In addi ion, hey can se e as a s ess
concen a o , om which c acks can ini ia e du ing he mechanical as
well as dynamic loading. The de o med su ace con ained plen y o
c acks o med a e he on al impac . Close de ail o c ack is p esen ed
in Fig. 8c. Each c ack is o med in main di ec ion wi h se e al seconda y
mic o sc a ches pe pendicula o main c ack.
3.3. Nume ical simula ion
The choice o he cons i u i e equa ion was based on se e al e-
qui emen s in ol ing he physical na u e o he e en . The J–C equa ion
includes i e pa ame e s, whe e wo pa ame e s, i.e. he s a ic low
s ess and he ha dening coe icien , we e ob ained om comp essi e
es . The acqui ed esul s om comp essi e es showed ha he
comp essi e yield s eng h a e in he ange 1150 MPa o 1204 MPa. The
alue 1204 MPa was se in J–C cons i u i e equa ion, which was used o
he TAT nume ic simula ion.
Fig. 9a shows he dependences be ween he e o s (pe cen age di -
e ences be ween he expe imen and he simula ion in he obse ed
a eas) on he s ain a e sensi i i y. These cu es we e e alua ed om
he sample, which ea u ed he 185 m.s
−1
impac speed. The pe cen age
di e ences we e obse ed in he a eas o maximum sample diame e
D
max
and inal leng h L
. The a e age e o eached a minimum alue a
C=0.138. When he s ain a e coe icien inc ease/dec ease he de-
ia ion would inc ease. A e he op imiza ion o he s ain a e sensi-
i i y pa ame e C, he so ening exponen m was also op imized. TAT
expe imen s we e also pe o med a ele a ed empe a u es, speci ically
o a measu ed su ace impac empe a u e o 175 ◦C, whe e he hea ed
sample was accele a ed owa ds he ba 's ace. A he ba 's ace, he
su ace empe a u e o he sample was eco ded wi h a non-con ac
empe a u e me e . By compa ing he con ou o he sample, namely
he maximum sample diame e D
max
and he inal leng h L
o he sample
a e he expe imen and op imizing D
max
and L
o he sample in he
nume ical simula ion gi en he eco ded su ace impac empe a u e,
he so ening exponen m was op imized. The esul s o he so ening
exponen op imiza ion can be seen in Fig. 9b.
The dependence o de o ma ion s ain on he loga i hmic de o ma-
ion was ob ained (see Fig. 10) by subs i u ing indi idual pa ame e s
in o he cons i u i e equa ion acco ding o J–C. The cu es we e plo ed
o di e en s ain a es, i.e., 0.02, 1200, 3000 s
−1
. The cu e acqui ed
by comp essi e es ( ep esen ed by he yellow line) was also included.
The obse ed de ia ion be ween yellow and blue lines (comp essi e es
and J–C equa ion) ea u ed he minimal de ia ion. The pa ame e s
Fig. 6. Comp essi e s ess –loga i hmic s ain cu es o all he examined
samples in as-buil condi ions, he sample placed in ix u e and is also included.
Fig. 7. Sample subjec ed o TAT: (a) on iew o he impac ed o ehead o he sample, (b) side iew p esen ing unnel-like and cylind ical a ea o he sample.
S. Kolomy e al.

Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
288
co esponding o J–C equa ion, which we e inally ob ained by nume ic
simula ion a e shown in Table 5. The esul s o he e ec i e s ain, he
ac ual s ain in indi idual axis is depic ed in Fig. 11a-d. Fig. 11a shows
he dis ibu ion o XY s ain componen s h oughou he es ed sample
a e TAT, which exhibi ed he highes de o ma ion a impac ed o e-
head. Nume ically p edic ed dis ibu ions o he s ess is depic ed in
Fig. 8. SEM images o he de o med TAT sample o ehead imposed o high s ain a e: (a) on iew o he sample, (b) a ea o in e es , (c) de ail o mic o c ack.
Fig. 9. Dependence o he de ia ion on he s ain a e sensi i i y (a) and dependence o he de ia ion on he so ening exponen m (b).
Fig. 10. Dependence o de o ma ion s ain on he loga i hmic de o ma ion.
Table 5
Nume ically ob ained pa ame e s o J–C cons i u i e equa ion.
σ
0
[MPa] B [−] n [−] C [−] m [−]
1104 1099 0.449 0.138 0.46
Fig. 11. Nume ically p edic ed dis ibu ions o s ain in XY (a), dis ibu ion o
s ess (b), YY s ain (c) and XX s ain (d).
S. Kolomy e al.
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
289
Fig. 11b whe eas Fig. 11c p edic s he dis ibu ion o YY s ain wi hin
es ed sample, which eached maximum in icini y o he cen e.
Fig. 11d p edic s dis ibu ion o XX s ain in he TAT es ed sample.
3.4. Mic oha dness e alua ion
Mic oha dness in de o med s a e a e TAT was e alua ed in e ical
(YZ plane is depic ed Fig. 1b) di ec ion. The mic oha dness (acco ding
o Vicke s HV 0.2) was e alua ed in h ee indi idual measu emen s
(lines 1–3 co esponding o Fig. 1c) in longi udinal and ans e se di-
ec ion. Mic oha dness in line 1 (depic ed in Fig. 12a) was measu ed
along he sample axis. A o al o 193 indi idual inden ions in 0.1 mm
we e pe o med in his line. The cou se o he mic oha dness co e-
sponds wi h he con ou (depic ed in Fig. 12a) o de o med sample. The
mic oha dness copies he cou se o he con ou , which eached he
highes obse ed alue (465 HV) in he icini y o he impac ed sample
o ehead due o se e e plas ic de o ma ion no iced in his egion. This is
an inc ease o 13,1 % wi hin his a ea, compa ed o he sample in as-
p in ed s a e. The cou se shows ha he mic oha dness dec eased wi h
he inc easing dis ance, which is p obably caused due o ac o s co e-
sponding wi h a e age g ain size, high angle g ain bounda ies and
disloca ion densi y. These ac o s we e a ec ed by se e e plas ic
de o ma ion (desc ibed in Sec ion 3.5). The e alua ed mic oha dness
oscilla ed wi hin cylind ical a ea (inc eased and dec eased) acco ding o
he place, whe e he mic oha dness was measu ed. The s uc u e (close
iew is desc ibed in ollowing chap e ) o he as-buil samples ea u ed
mel ing pool s uc u e wi h wo dis inc egions, which co esponds o
di e en e ching con as (see Fig. 12A2). Da ke a eas p esen ing a
empe ed ma ensi e egion, which al e na e wi h b igh e a eas co e-
sponding o less ex ensi e empe ing [61]. SEM image (see Fig. 12A1)
e ealed a p esence o ine seconda y ca bides wi hin empe ed a ea.
The mic oha dness measu emen s con i med he lowe mic oha dness
o he da ke a eas (T =Tempe ed =393 ±5 HV 0.2), hen b igh e
a eas o less empe ed ma ensi e (Q =Quench =420 ±5 HV 0.2),
which can be conside ed as quickly quenched egion. O he cu en
wo k [62] discussed he ac ha as each subsequen laye is deposi ed,
he empe a u e inc eases due o hea ans e om he solidi ying laye
owa ds o he p e iously deposi ed laye . The inc ease o empe a u e
may cause he empe ing p ocess in neighbou ing laye s (i.e., in insic
empe ing du ing he SLM p ocess). Based on acqui ed da a, he cylin-
d ical a ea o as-de o med sample can be conside ed o ha e he same
mic oha dness as he sample in as-p in ed s a e. In o he wo ds, he
s ain a e in luenced he mic oha dness only in impac ed unnel-like
a ea o he sample, as well as he cylind ical a ea wi hin he sample
exhibi ed no signi ican changes.
Mic oha dness in line 2 and 3 (see Fig. 12b) was measu ed pe pen-
dicula o he sample axis. To al o 33 and 26 indi idual inden ions in
dis ance o 0.2 mm we e pe o med in hese lines, whe e line 2 p esen s
highe a e age alue (459 ±8 HV) o mic oha dness han line 3 (409 ±
7 HV). This is an inc ease o 12.2 % co esponding wi h geome ical and
s uc u e changes a ec ed by se e e plas ic de o ma ion, lowe a e age
g ain size and high ac ion o high-angle g ain bounda ies (HAGB,
desc ibed in ollowing chap e in de ail). Conside ing he cou se o he
alues in each line, acqui ed da a esul ed highe dispe sion in line 3
co esponding o di e en measu ed egion ( empe ed and quench). The
dispe sion in line 2 was diminished due he o e whelming e ec o
lowe a e age g ain size, high ac ion HAGB and disloca ion densi y.
3.5. S uc u e obse a ion
Fig. 13 shows a ligh op ical mic oscopy image aken om he
sample subjec ed o dynamic es ing ia TAT. The images ep esen he
longi udinal c oss-sec ion in YZ plane. The s uc u e in he cylind ical
a ea o he sample shows (see Fig. 13a) isible scanning pa hs and
cha ac e is ic mel pool s uc u e ypically c ea ed by he sin e ing
p ocess. The s uc u e ea u es semi-ellip ical g ains c ys allizing in he
solidi ying laye , which ha e hei longe axis pe pendicula o he lase
beam. The deposi ed laye is co e ed wi h he ollowing scanning pa h
c ea ing he o e lapped a eas. This ype o obse ed s uc u e is ypical
o c oss-sec ion made pa allel o he building di ec ion. SLM p ocess
causes a nonuni o mal cooling a e, which is slowe inside he mel pool
han a he bounda y esul ing in a di e en c ys alliza ion a es and
undesi able seg ega ion inside he mel ing pools [63]. This seg ega ion
can a ec mechanical p ope ies o pieces p oduced ia SLM. Due o
lowe se laye hickness (40
μ
m), i can be p edic ed ha indi idual
laye s could be emel ed se e al imes. The emel ing p ocess can cause
pa ial annealing o he al eady deposi ed laye esul ing in nonhomo-
geneous mechanical p ope ies. S uc u e in unnel-like a ea o he
sample is depic ed in Fig. 13b. De o ma ion unde s ain a e en ailed in
a change o s uc u e. The shape o a mel pools exhibi ed longe main
axis and sho e seconda y axis compa ed o pools in cylind ical a ea
esul ing in change o mechanical p ope ies.
EBSD O ien a ion image maps (OIMs) (depic ed in Fig. 14) we e
cons uc ed on images cap u ed a 1000×magni ica ion ep esen lon-
gi udinal (YZ plane) c oss-sec ion o he sample subjec ed o dynamic
es ia TAT. The g ains a e shown in he maps, using colou s ( ed, g een
and blue) ela ing o hei indi idual o ien a ions along he h ee p in-
cipal c ys al di ec ions i.e., 〈001〉,〈101〉, and 〈111〉, acco ding o Mille
indices ( he legend iangle is depic ed in each igu e). These o ien a ion
maps a e p esen ed on each a ea I-III co esponding o Fig. 1c. The g ain
o ien a ions in each a ea we e obse ed pa allel o he building di ec-
ion i.e., he longi udinal images (YZ plane) we e e alua ed pa allel o
he x axis (|| x).
G ain s uc u e in he cylind ical a ea (depic ed in Fig. 14a) ea u ed
mos ly an i egula shape wi hin his a ea I and exhibi ed no endency o
o m in ce ain o ien a ion. G ain s uc u e depic ed in Fig. 14d and g
p esen clus e s o ine equiaxed g ain and ew elonga ed g ains, which
can be seen legibly. Conside ing he OIM and o ien a ion oge he , i
appea s ha he elonga ed g ains o m pe pendicula o he sample axis.
Fig. 12. Dependence o Vicke s mic oha dness on dis ance in YZ plane: (a)
measu ed mic oha dness in line 1, (A1) p esence o ine seconda y ca bides,
(A2) wo di e en egions i.e., empe ed, and quenched s uc u e, (b) measu ed
mic oha dness in line 2 a 3.
S. Kolomy e al.
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
290
Fig. 14d desc ibes elonga ed g ains in he cen e o he sample, which
ea u e a endency o o m he <101>||z p e e en ial o ien a ion as well
as he a ea a he bounda y o he sample (see Fig. 14g) exhibi s he same
endency. Such clus e s o ine equiaxed g ains appea in icini y o he
impac ed o ehead, whe e he applied s ess eached he maximum
alue. The lowe impac ed s ess (co ela e wi h nume ic simula ion) on
he edge o de o med egion o he sample esul ed in a lowe numbe o
such clus e s o ine g ains. P asad e al. [64] obse ed c ea ion o he
clus e o ine g ains in a eas which we e subjec ed o he emel ing
p ocess o successi e laye s.
The a e age g ain size in all a eas was examined (examina ion was
ca ied ou in YZ plane conside ing he a eas I-III, see OIMs images
depic ed in Fig. 14a, d, g) using g ain e e diame e (de ined as a
maximum dis ance be ween wo poin s wi hin a single g ain). In each
a ea I-III he a e age g ain size sligh ly a ied, bu he highes obse ed
di e ence was among a eas I and II co esponding o cylind ical and
unnel-like egion, espec i ely. A e age max. G ain e e diame e in
a ea I (cylind ical shape o he sample, which was no signi ican ly
a ec ed wi h s ain a e) was e alua ed as 10.2
μ
m ( he examined g ain
size in a ea I is depic ed in Fig. 14b). A ea II and III exhibi ed a s uc u e
change compa ed o a ea I. Due o s ain a e a signi ican g ain
e inemen was obse ed wi hin a eas II and III (each a ea II and III was
chosen in unnel-like a ea o he sample). The a e age g ain size
dec eased o 3.1
μ
m and 3.6
μ
m (see Fig. 14e and h) in a ea II and III
espec i ely. This is an almos h ee imes ine s uc u e compa ed o
a ea I ( he cylind ical pa o he sample).
The c ys allog aphic ex u e in a eas I, II, and III was s udied
conside ing he in e se pole igu es (IPFs) o YZ plane. IPFs cap u ed in
a ea I (see Fig. 14c) ea u ed a dominan o ien a ion, which is o med o
〈111〉|| z. The c ys allog aphic ex u e o he as-buil sample can be
a ec ed by he ene gy densi y deposi ed du ing sin e ing p ocess
[65–67]. Fig. 14 and i showing cha ac e is ic IPFs o a eas II and III
si ua ed in he unnel-like a ea o impac ed o ehead. Conside ing he
IPFs o de o med egion in a ea II, i is e iden ha he p e alen c ys al
o ien a ion along he build di ec ion was o med o <001>|| x o ien-
a ion as well as in a ea III. The c ys allog aphic ex u e in hese a eas is
ela ed a he o he impac de o ma ion han o he sin e ing p ocess.
The HAGB ac ion (analysis based on OIM images, h eshold o a high-
angle g ain bounda y conside ed o be 15) in cylind ical a ea I exhibi ed
30.6 %, which was he lowes obse ed ac ion. The obse ed HAGB
exhibi ed no signi ican di e ence in a eas II and III (examined HAGB in
bo h a eas we e 50.8 % and 48.2 % espec i ely). I is e iden ha a e
se e e plas ic de o ma ion he inc ease o HAGB in unnel-like a ea o
he sample was obse ed. Howe e , he highes HAGB ac ion was
obse ed in he cen e o he impac ed o ehead.
Fig. 15 shows geome ically necessa y disloca ion (GND) densi y
maps es ima ed om he EBSD o ien a ion da a co esponding o a ea I-
III. GNDs ha e been mapped in ield 100 ×100
μ
m a ound g ain
bounda ies a ec ed by s ain a e. Black pixels in each map a e co e-
sponding o non-indexed egions. Colou -scale, which is p esen ed in
each map illus a es he es ima ed amoun o disloca ion densi y
(numbe o disloca ions/m
2
) con ained wi hin each measu ed pixel on
he map. Fig. 15a p esen s acqui ed GND in a ea I, which co esponding
o he lowes alue o 11.25 p obably due o he insu icien mac oscopic
s ess le el. The minimum GND densi y is in he cen e o he g ains wi h
high GND accumula ion in he icini y o he g ain bounda ies. G ains,
which showed a s ong endency o o m in <101>||z p e e en ial
o ien a ion exhibi ed a low GND densi y on hese slip sys ems. The GND
shows he highes le el 52.77 in he cen e o unnel-like a ea II (see
Fig. 15b) co esponding o he highes numbe o high-angle g ain
bounda ies, he lowes a e age g ain size and o he highes obse ed
mic oha dness. Fig. 15c depic s a ea III, whe e he GND dec eased as
well as a e age g ain size inc eased compa ed o a ea II. The se e e
plas ic de o ma ion ea u ed a dominan e ec in he cen e o he
unnel-like a ea o he de o med sample due o c ea ion o s uc u e wi h
he lowes a e age g ain size, highes ac ion o HAGB and GND
densi y.
Based on ob ained da a, he mic os uc u e and geome ical changes
we e in luenced by high impac eloci y accompanied wi h high s ain
a e. Mos a ec ed egion (conside ing s uc u e and geome ical shape)
was he unnel-like a ea in he icini y o impac ed o ehead o he
sample. Howe e , he cylind ical a ea I ea u ed e y simila mic o-
ha dness compa ed o as-p in ed samples. The inc ease o mic oha d-
ness in he unnel-like a ea was p obably in luenced by se e al ac o s:
a e age g ain size, numbe o disloca ions and HAGB ac ion. The
applied impac eloci y esul ed in se e e plas ic de o ma ion, which
mainly a ec ed he egion o he de o med o ehead. The a e age g ain
size dec eased due o a c ea ion o he clus e o ine g ains in he i-
cini y o he cen e sample axis. The c ea ion o such clus e s o ine
g ains was accompanied wi h o ming o disloca ions p esen ed domi-
nan ly on g ain bounda ies. The a ea II close o sample axis exhibi ed he
highes HAGB ac ion, which dec ease wi h inc easing dis ance om
he sample axis. These ac o s pe ec ly co ela e wi h nume ic simula-
ion, which con i med he highes obse ed s ess in he cen e a ea II o
he sample dec easing owa ds a ea III. Mapping o he dynamic
beha iou will ob ain a signi ican da a, which can be used in nume ic
simula ions. The acqui ed da a om comp essi e es ing we e imple-
men ed in Johnson-Cook equa ion used o nume ic simula ion. Thanks
o he J-C equa ion new dynamically loaded componen s can be
designed as e and mo e accu a e (based on nume ic simula ion).
App op ia e pa su ace quali y is expec ed o inc ease esis ance o
dynamic cyclic loading as well as he inal po osi y o he componen .
Fig. 13. Ligh op ical mic oscopy (LOM) images o a eas (a) I, (b) II p esen ed in Fig. 1c.
S. Kolomy e al.
Jou nal o Manu ac u ing P ocesses 125 (2024) 283–294
291
Fig. 14. OIMs o he sample subjec ed o dynamic es ia TAT in YZ plane (a) a ea I, (b) max. Fe e diame e in a ea I, (c) IPFs in a ea I, (d) a ea II, (e) max. Fe e
diame e in a ea II, ( ) IPFs in a ea II, (g) OIMs in a ea III, (h) max. Fe e diame e in a ea III, (i) IPFs in a ea III.
S. Kolomy e al.