Study of mechanical properties of epoxy/graphene and epoxy/halloysite nanocomposites
Abstract
CZ.02.1.01/0.0/0.0/16_019/0000867; Tomas Bata University in Zlin, TBU: IGA/FT/2022/005, IGA/FT/2023/007; Univerzita Palackého v Olomouci: IGA_PrF_2022_020, IGA_PrF_2023_024
Full text
Resea ch A icle
Lubomí Lapčík*, Ha un Sepe cioğlu, Youse Mu aja, Ba bo a Lapčíko á, Ma in Vašina,
Ma in O sík, Michal S aněk, and Shwe a Gau am
S udy o mechanical p ope ies o epoxy/
g aphene and epoxy/halloysi e nanocomposi es
h ps://doi.o g/10.1515/n e -2022-0520
ecei ed Oc obe 3, 2022; accep ed Feb ua y 3, 2023
Abs ac : This a icle aimed o compa e a ious mechan-
ical p ope ies o epoxy/g aphene and epoxy/halloysi e
nanocomposi es. G aphene nanopla ele s (GnPs)and hal-
loysi e nano ubes (HNTs)we e used as fille s a diffe en
concen a ions. The s udied fille s we e dispe sed in he
epoxy esin ma ices. Elas ic–plas ic mechanical beha io
modula ion was obse ed u ilizing he fille s’nanopa i-
cles and ca boxyl- e mina ed bu adiene–ac yloni ile
copolyme ubbe -modified epoxy esin. The hypo hesis
o he possible p eceding in e -pa icle gliding o he indi-
idual GnPs in he complex esin nanocomposi e ma ix
du ing mechanical es ings was also confi med. Inc eased
duc ili y (elonga ion a b eak inc eased om 0.33 mm
[nea ma ix] o 0.46 mm [1 w % GnPs][39% inc ease])
and plas ici y o he GnP nanocomposi e samples we e
obse ed. In con as , he dec easing mechanical s iffness
as eflec ed in he dec eased Young’s modulus o elas ici y
( om 3.4 o 2.7 GPa [20% dec ease]) was ound o he
epoxy/HNT nanocomposi es. The ob ained dynamic s iff-
ness o he in es iga ed nanocomposi es confi med he
complexi y o he mechanical esponse o he s udied
ma e ial sys ems as a combina ion o he duc ile and
b i le phenomena.
Keywo ds: g aphene, halloysi e, nanocomposi es, epoxy
polyme , CTBN ubbe , mechanical es ing
1 In oduc ion
Polyme ic and esin-based nanocomposi es a e widely
used in ma e ial enginee ing esea ch owing o hei
capaci y o modula e plas ic–elas ic mechanical pe o -
mance a s a ic and dynamic mechanical loadings [1].
These nanocomposi es a e cha ac e ized by high mechan-
ical oughness and wea esis ance, imp o ed sel -lub ica-
ion p ope ies, and low ic ion coefficien [2,3]. The e o e,
hey ha e a wide ange o applica ion po en ial in he
ae ospace [4], au omo i e [5], chemical, and elec onic
indus ies as well as high- ol age ou doo insula ion ma e-
ials [6–8].
The abili y o a ma e ial o abso b mechanical impac ,
i.e., i s oughness, equi es high o ce esis ance and he
exis ence o he de o ma ion mechanisms ha abso b and
dissipa e he applied mechanical ene gy o e a la ge pa h,
in a la ge olume, and o a sufficien ly long ime. Such
mechanisms may be inhe en in he ma e ial due o i s
specific mic os uc u e bu can also be delibe a ely inco -
po a ed in o he s uc u e o polyme /epoxy esin compo-
si es and blends [9,10]. Such syne gis ic effec can be
ob ained by p ope selec ion o he combina ion o he
nanofille pa icles’ ype (g aphene nanopla ele s [GnPs],
halloysi e nano ubes [HNTs],e c.),shape,andsu ace
chemis y, by modula ing he physicochemical cha ac e is ics
o he ma ix, e c., o example, by adding ubbe y plas ic
componen s [11,12]. Howe e , li e a u e indica es ha ela-
i ely ew s udies ha e ocused on ca boxyl- e mina ed bu a-
diene–ac yloni ile (CTBN)copolyme ubbe -modified epoxy
* Co esponding au ho : Lubomí Lapčík, Depa men o Physical
Chemis y, Facul y o Science, Palacky Uni e si y, 17. Lis opadu 12,
771 46 Olomouc, Czech Republic; Facul y o Technology, Tomas Ba a
Uni e si y in Zlin, Nam. T.G. Masa yka 275, 760 01 Zlin, Czech
Republic, e-mail: [email p o ec ed]
Ha un Sepe cioğlu: Depa men o Me allu gy and Mechanical
Enginee ing, Technology Facul y, Selçuk Uni e si y, Konya 42075,
Tu key
Youse Mu aja: Depa men o Physical Chemis y, Facul y o
Science, Palacky Uni e si y, 17. Lis opadu 12, 771 46 Olomouc,
Czech Republic
Ba bo a Lapčíko á: Depa men o Physical Chemis y, Facul y o
Science, Palacky Uni e si y, 17. Lis opadu 12, 771 46 Olomouc,
Czech Republic; Facul y o Technology, Tomas Ba a Uni e si y in
Zlin, Nam. T.G. Masa yka 275, 760 01 Zlin, Czech Republic
Ma in Vašina: Facul y o Technology, Tomas Ba a Uni e si y in Zlin,
Nam. T.G. Masa yka 275, 760 01 Zlin, Czech Republic; Depa men o
Hyd omechanics and Hyd aulic Equipmen , Facul y o Mechanical
Enginee ing, VŠB-Technical Uni e si y o Os a a, 17. Lis opadu
15/2172, 708 33 Os a a-Po uba, Czech Republic
Ma in O sík, Michal S aněk, Shwe a Gau am: Facul y o
Technology, Tomas Ba a Uni e si y in Zlin, Nam. T.G. Masa yka 275,
760 01 Zlin, Czech Republic
Nano echnology Re iews 2023; 12: 20220520
Open Access. © 2023 he au ho (s), published by De G uy e . This wo k is licensed unde he C ea i e Commons A ibu ion 4.0 In e na ional
License.
esins filled wi h GnPs exhibi ing he imp o ed ac u e
oughness [13–16].
Se e al polyme composi es ha e been epo ed in
ecen yea s, including polyes e , polyu e hane, epoxy,
and phenolics [17,18]. Among hese, epoxy polyme com-
posi es ha e gained emendous a en ion due o hei
high mechanical oughness and mois u e abso p ion p op-
e ies [19]. Addi ionally, hese esins show less sh inkage
and less oxic emissions du ing he cu ing p ocess [20].
The e o e, epoxy esins a e conside ed high-quali y ma e-
ials on an indus ial scale, despi e hei high cos [21].
In gene al, he plas ic o iscoelas ic de o ma ion o
ma e ials in on o he c ack apex emo es pa o he
c ack ene gy and hus con ols i s p og ess wi hin he
ma ix. The e o e, he diffe ence be ween b i le and duc-
ile ac u es is in hei spa ial localiza ion and hei em-
po al p og ession. Mos polyme composi e ma e ials can
b eak down by ei he b i le o duc ile ac u es depending
on he ex e nal condi ions o p ocesses aking place in he
ma e ial. The ansi ion be ween duc ile and b i le ac-
u es can be empe a u e dependen , wi h he empe a u e
egions o he wo dis inc mechanisms sepa a ed by he
emb i lemen empe a u e. The la e always lies below
he glass- ansi ion empe a u e. In he same sense, wi h
a d op in empe a u e, an inc ease in loading a e can ha e
an effec –al hough he diffe ence in loading a e mus be
an o de o magni ude g ea e o ha e an effec on he
na u e o he ac u e. Howe e , long- e m s a ic loading
below he yield s ess o many polyme s also leads o
b i le ac u e. In his case, he “ma e ial sel -de ence”
mechanisms canno de elop sufficien ly by c ea ing a
plas ic zone in on o he c ack ip [9].
T ibological p ope ies o esins o en indi ec ly influ-
ence hei mechanical s eng h, whe eas epoxy esins
exhibi limi ed ibological p ope ies [22]. Fo example,
he se ice li e o pipes made o polyme ic composi es
depends on he effec i i y o he ene gy dissipa ion du ing
fluid flow, he cha ac e o which is dependen on he
wall ic ion o he anspo ed medium. Such pipes a e
exposed unde se ice condi ions o long- e m s esses,
usually unde ela i ely low empe a u es, bu some-
imes also a he in e ac ion o an ac i e en i onmen .
Unde hese condi ions, hey canno p ope ly de elop
he “sel -de ense”mechanisms o c ack blun ing by
local plas ic de o ma ion, and om he exposed su ace
small c acks p opaga e inside he ma e ial o e en sha p
c acks, which e en ually lead o b i le ac u e [9].
Se e al me hods ha e been epo ed o imp o e hese
p ope ies, i.e., adding mic o-and nano-sized pa icles as
fille s in he esin ma ix [23,24]. A la ge a ie y o nano-
fille s, such as SiO
2
, MnO
2
, TiO
2
,Al
2
O
3
, SiC, Si
3
N
4
, ZnO,
MoS
2
, nanoclay, and ca bon nano ubes, ha e been epo ed
in diffe en ypes o polyme ic esins [25–28].Thesefille s
ha e demons a ed a ying efficiencies wi h ce ain limi a-
ions, which hinde hei p ac ical applica ions [29].
GnPs, consis ing o 30–40 laye s o g aphene, a e
widely used nanoma e ials due o hei high he mal s a-
bili y and conduc i i y, high Young’s modulus o elas i-
ci y, high op ical ansmi ance, high ac u e s eng h,
and imp o ed lub ica ion p ope ies [17,30]. Due o hei
inhe en , in insic ene gy-dissipa ing mechanisms (shee
bending and sliding), GnPs belong o highly ad anced
ma e ials used in composi e manu ac u ing [17,31]. How-
e e , i is necessa y o op imize he con en o g aphene
nanofille s in epoxy esins because highe con en leads
o nonuni o m dis ibu ion o g aphene in he polyme
ne wo k [32]. Ano he challenge is he obse ed high
agg ega ion a es o g aphene a ising om he ac ing
Van de Waals in e ac ion o ces [33–35]. Fo his eason,
i is necessa y o op imize a p ope mass a io o g a-
phene nanofille s o epoxy esin in o de o ob ain he
desi ed mechanical p ope ies.
Halloysi e, an aluminosilica e clay ma e ial [36],is
ano he fille commonly used in polyme esins owing
o i s cylind ical s uc u e, imp o ed mechanical pe o -
mance, and low cos [37,38]. HNTs exhibi highe dispe -
sion a io and ha e su ace hyd oxyl g oups wi h low
densi y, which esul s in hei smoo h diffusion in o he
polyme ma ix, leading o less agg ega ion [39]. Mo e-
o e , due o small basal spacing o c ys al planes, he
in e cala ion o HNTs wi h polyme s and addi i es is di -
ficul [40,41]. Howe e , HNT nanofille s belong o po en-
ial unc ional fille s used in indus ial p ac ice [42,43].
Published esul s confi med syne gis ic combina ion
o he plas ifica ion effec o he igid epoxy ma ix assigned
o he gliding o he indi idual GnP nanofille s and he
s iffening effec o he HNT nanofille s when ac u e ough-
ness inc eased. The la e plas ifica ion was also enhanced
by he addi ion o he CTBN polyme ic ubbe componen o
he composi e epoxy ma ix, hus imp o ing ma e ial’s ac-
u e oughness. A simila effec was also confi med by mole-
cula dynamics simula ions o mono helical so segmen s
based on New onian mechanics heo y [44].
In his s udy, GnPs and HNTs we e used sepa a ely as
fille s o imp o e he mechanical pe o mance, dispe -
sion, he mal s abili y, and op o-elec onic p ope ies o
he epoxy esin composi e. A a ying mass a io o bo h
fille s was used in p epa ed composi es, and he effec o
he applied nanofille s was e alua ed by uniaxial ensile
es ing, ac u e oughness measu emen s, uniaxial bending
es ing, inden a ion mic o-ha dness measu emen s, and
nondes uc i e ib a ion es ing.
2Lubomí Lapčík e al.
2 Ma e ials
2.1 Ma e ials
The esin and ha dene used in his s udy we e diglycidyl
e he o bisphenol A esin (DGEBA)wi h low iscosi y
( ade name: lamina ing esin MGS L285)(Figu e 1a)and
3-aminome hyl-3,5,5 ime hylcyclohexylamine ( ade
name: L285), espec i ely (bo h ma e ials we e p o ided
om Hexion, USA)(Figu e 1b). The liquid ubbe used was
CTBN copolyme (pu chased om Zibo Qilong, China)wi h
an a e age o 0.58–0.65 ca boxyl g oups pe molecule; i s
numbe a e age molecula weigh was abou 3,800 Da,
and he con en o ac yloni ile was o 8–12% (Figu e 1c).
The echnical da a o he CTBN a e gi en in Table 1. The
chemical s uc u es o epoxy, ha dene , and CTBN a e
showninFigu e1.Nanofille s used in his s udy we e non-
unc ionalized plana -shaped GnPs o 800 m
2
/g specific
su ace a ea, laye hickness o 3–7nmwi hana e age
laye wid h o 1.5 μm, and 99.9% pu i y (pu chased om
Nanog afi,Anka a,Tu key).TheHNTs(Al
2
Si
2
O
5
(OH)
4
)used
had wo laye s o nanocylind ical s uc u e (Esan Eczacıbası
(Is anbul, Tu key)), whose inne diame e , ou e diame e ,
and leng h we e in he ange o 1–20, 30–50, and 100–800 nm,
espec i ely.
2.2 P epa a ion o nanocomposi es and
epoxy blends
2.2.1 CTBN–epoxy blends
The chemical o mulas o he used epoxy blends a e
shown in Figu e 1. Fo p epa ing he epoxy blends wi h
CTBN liquid ubbe , 10 w % CTBN was mechanically
mixed wi h epoxy esin in a glass beake placed on a
p ehea ed pla e. The blends in he beake we e hen
s i ed by ul asonica ion o 15–20 min o ob ain homo-
geneous blends, ollowed by 1 h o degassing in he
acuum o en a 60°C. The amine-based cu ing agen
was subsequen ly added a a s oichiome ic a io o 80:20
(epoxy:ha dene )by weigh a slow s i ing. Blends we e
subsequen ly cas in o molds and cu ed o 1 h a 90°C,
ollowed by 3 h pos -cu ing a 120°C.
2.2.2 CTBN–GnPs–epoxy and CTBN–halloysi e–epoxy
composi es
The nano- ein o cemen a ios o he epoxy mix u es we e
c ea ed based on he li e a u e. Many au ho s [43,45–49]
ha e expe imen ally s udied he concen a ion o GnP and
HNTs in he epoxy ma ix o be in he ange o (0–1)and
(0–5)w %, espec i ely, and epo ed he effec o hese
concen a ions on ensile, ac u e, and flexu al p ope ies
o he nea ma ix. Fo p epa ing he epoxy mix u es wi h
GnPs and HNTs (see Figu e 2 o scanning elec on mic o-
scopy [SEM]), 0, 0.125, 0.25, 0.5, 0.75, and 1 w % GnPs and
0, 1, 2, 3, 4, and 5 w % HNTs we e added o he epoxy
esin, and he ob ained mix u es we e ans e ed in o a
RETSCH-PM 100 plane a y mill o mixing a a o a ion a e
o 200 pm o 25 h. The epoxy composi e mix u es we e
p epa ed using 10 mm diame e balls and a bowl made o
ungs en ca bide as mixing media. The mixing bowls we e
loaded wi h he epoxy mix u es and balls, esul ing in a
ball- o-powde mass a io o 30:1. Fi s , he mix u es we e
mixed o 30 min, hen es ed o 10 min o a oid o e -
hea ing, hen mixed again, and he cycle was con inued
un il he decided mixing ime was comple ed. Subse-
quen ly, 10 w % CTBN was added o each epoxy mix u e
con aining he GnP and HNT ein o cemen s o p epa ing
he CTBN–GnPs–epoxy and CTBN–HNTs–epoxy compo-
si es. The p epa ed mix u es we e s i ed using ul asoni-
ca ion o 25–30 min o ob ain he homogeneous mix u es,
ollowed by degassing in a acuum o en a 60°C o abou
1 h. Finally, he cu ing p ocedu e o CTBN–epoxy blends
Figu e 1: The chemical s uc u e o componen s (a)DGEBA, (b)3-
aminome hyl-3,5,5- ime hylcyclohexylamine, and (c)CTBN.
Table 1: P ope ies o he applied CTBN liquid ubbe
Pa ame e Value
Viscosi y (40°C)(Pa s)7−12
Ca boxyl con en (mmol/g)0.58−0.65
Ni ile g oup con en (%)8.0−12.0
Wa e con en (%)≤0.05
Vola ile con en (%)≤2.0
G aphene and halloysi e epoxy nanocomposi es 3
desc ibed in Sec ion 2.2.1 was ollowed o cu e he
CTBN–GnPs–epoxy and he CTBN–HNTs–epoxy compo-
si es. The same CTBN liquid ubbe concen a ion o 10
w % was used in all o he in es iga ed epoxy/g aphene
and epoxy/halloysi e nanocomposi es; he i gin epoxy
ma ix p epa ed was wi hou CTBN liquid ubbe .
3 Me hods
3.1 SEM analysis
Zeiss E oLS10 equipped wi h an ene gy-dispe si e X- ay
de ec o (Ge many)was used o SEM analysis. SEM
images we e aken by deposi ing nanofille samples on
a s anda d 400-g id coppe mesh. Fille s’ace one dispe -
sions we e ul asonica ed o 15 min, cas on he coppe
mesh, and ai d ied. SEM measu emen s we e pe o med
a an accele a ing ol age o 2 kV.
3.2 Uniaxial ensile es ing
Uni e sal Tes ing Machine Au og aph AGS-100 Shimadzu
(Japan)and Zwick 1456 mul ipu pose es e (Zwick Roell,
Ulm, Ge many)equipped wi h Compac The mos a ic Chambe
TCE Se ies we e used o ensile es ing o injec ion-molded
specimens. All da a we e eco ded as pe ČSN EN ISO 527-1
and ČSN EN ISO 527-2 s anda ds o he es ed gauge
leng h o 80 mm. All expe imen s we e pe o med a
oom empe a u e up o b eak wi h a 50 mm/min de o -
ma ion a e. Young’s modulus o elas ici y and elonga ion
a b eak we e ob ained om he s ess–s ain dependency
plo s. Each expe imen was epea ed 10×,andmean
alues and s anda d de ia ions o he measu ed quan-
i ies we e subsequen ly calcula ed. All expe imen s
we e pe o med a he ambien labo a o y empe a u e
o 25°C.
3.3 Cha py impac es ing
Impac es s we e ca ied ou using Zwick 513 Pendulum
Impac Tes e (Zwick Roell, Ulm, Ge many)acco ding o
he ČSN EN ISO 179-2 s anda d, allowing a 25 J ene gy
d op. Each expe imen was epea ed 10×and mean alues
and s anda d de ia ions o he ac u e oughness we e
calcula ed. All expe imen s we e pe o med a he ambien
labo a o y empe a u e o 25°C.
3.4 Mic o-ha dness
Mic o-inden a ion es s we e pe o med on a mic o-inden-
a ion es e (Mic o Combi Tes e , An on Paa , Aus ia),
acco ding o he ČSN EN ISO 14577 s anda d. The applied
diamond ip was cube-co ne shaped (Vicke s, An on
Paa , Aus ia). Measu emen pa ame e s we e se as ol-
lows: he maximum load o 3 N, loading a e (unloading
a e)o 6 N/min, and holding ime o 90 s. All expe imen s
we e pe o med acco ding o he dep h-sensing inden a-
ion me hod, allowing simul aneous measu emen o he
ac ing o ce on he inden e and he displacemen o he
inden e ’s ip. The inden a ion modulus (E
IT
)was calcula ed
om he plane s ain modulus o elas ici y (E*)using an
es ima ed Poisson’s a io(ν)o he samples (0.3–0.4 [50,51]):
()=*−EE ν1
.
IT 2(1)
Each measu emen was epea ed 10×, and mean alues
and s anda d de ia ions o he inden a ion modulus we e
calcula ed. All expe imen s we e pe o med a he ambien
labo a o y empe a u e o 25°C.
Figu e 2: SEM images o he s udied fille s: (a)GnPs, (b)HNT.
4Lubomí Lapčík e al.
3.5 Uniaxial h ee-poin bending es s
The uniaxial h ee-poin bending es was ca ied ou on
a Zwick 1456 es ing machine (Zwick Roell GmbH &Co.
KG, Ulm, Ge many)acco ding o he ČSN EN ISO 14125
s anda d. The esul s we e e alua ed using he Tes Xpe
so wa e. The dis ance be ween he suppo s was se o
64 mm, and he oundness o he suppo s and he load
mand el was 5 mm. The de o ma ion a e du ing he
h ee-poin bending es was 1 mm/min, and he loading
eloci y was 50 mm/min.
3.6 Displacemen ansmissibili y
measu emen s
Displacemen ansmissibili y T
d
is exp essed by he ol-
lowing equa ion [52]:
==Ty
ya
a
,
d2
1
2
1(2)
whe e y
1
is he displacemen ampli ude on he inpu side
o he es ed sample, y
2
is he displacemen ampli ude on
he ou pu side o he es ed sample, a
1
is he accele a ion
ampli ude on he inpu side o he es ed sample, and a
2
is he accele a ion ampli ude on he ou pu side o he
es ed sample. The displacemen ansmissibili y o a
sp ing–mass–dampe sys em, which is desc ibed by sp ing
(s iffness k),dampe (damping coefficien c),andmassm,is
gi en by he ollowing equa ion [53]:
()
()()
()
()()
=+
−+
=+·
−+·
Tkcω
kmω cω
∙
∙∙
12∙ζ∙
12∙ζ∙
.
d
22
22 2
2
22 2
(3)
Unde he condi ion dT
d
/d =0 in equa ion (3), i is pos-
sible o ob ain he equency a io
0
a which he displace-
men ansmissibili y eaches i s maximum alue [54,55]:
=+−
18∙ζ 1
2∙ζ
.
0
2
(4)
I is e iden om equa ion (4) ha he local ex eme o
he displacemen ansmissibili y is gene ally shi ed o
lowe alues o he equency a io wi h inc easing
damping a io ζ(o wi h dec easing ma e ial mechanical
s iffness k). The local ex ema (i.e., he maximum alue
o he displacemen ansmissibili y T
dmax
)is ound a
he equency a io
0
om equa ion (4). The mechanical
ib a ion es s we e pe o med by o ced oscilla ion me hod.
The displacemen ansmissibili y T
d
was expe imen ally
measu ed using he BK 4810 ib a o in combina ion wi h
aBK3560-B-030 signal pulse mul i-analyze and a BK 2706
powe amplifie a he equency ange om 2 o 3,200 Hz.
The accele a ion ampli udes a
1
and a
2
on he inpu and
ou pu sides o he in es iga ed samples we e eco ded by
BK 4393 accele ome e s (B üel & Kjæ , Næ um, Denma k).
Measu emen s o he displacemen ansmissibili y we e
done o h ee diffe en ine ial masses m( o 0, 90, and
500 g), which we e placed on he op side o he es ed
samples. The dimensions o he es ed specimen we e
60 mm ×60 mm ×3mm(leng h ×wid h × hickness).
Each measu emen was epea ed 5×a an ambien empe a-
u e o 22°C.
4 Resul s and discussion
A ypical shape o he used nanofille s, as obse ed by
SEM analysis, is shown in Figu e 2. He e he GnP lamella
s uc u e was clea ly isible in Figu e 2a wi h a laye
hickness o abou 3–7 nm and an a e age laye wid h
o 1.5–2.0 μm. In con as , he HNT nano ubes exhibi ed
a compac coagula ed s uc u e composed o indi idual
nano ubes o app oxima ely 30–50 nm diame e and
100–800 nm leng h (Figu e 2b).
Resul s o he ensile- es ing expe imen s o he s u-
died nanocomposi es a e shown in Figu e 3. The e was a
dec ease o he Young’s modulus o elas ici y (E)du ing
uniaxial es ing om 3.4 GPa (nea ma ix) o 2.7 GPa ( o
1 w % epoxy/GnP nanocomposi e)wi h inc easing GnP
fille concen a ion [56]. This effec was accompanied by
he inc easing nonlinea end o he ob ained magni-
udes o he elonga ion a b eak, indica ing inc easing
duc ili y and plas icizing effec o he GnP nanofille on
he mechanical beha io o he p epa ed epoxy/GnP nano-
composi es. Based on he li e a u e [11], i was assumed
ha his beha io was asc ibed o he gliding o he indi-
idual nanopla ele shee s wi hin complex epoxy/GnP
nanocomposi e ma ix accompanied by he c ack deflec-
ion, laye b eakage, and sepa a ion/delamina ion o GnP
laye s [13]. Howe e , he opposi e effec was ound in he case
o he epoxy/HNT nanocomposi es, whe e he Edec eased
om 3.4 GPa (nea ma ix) o 2.7 GPa ( o 5 w % epoxy/HNT
nanocomposi e), hus indica ing he dec easing mechanical
s iffness o he s udied ma e ials. Simul aneously, in con as
o he epoxy/GnP nanocomposi es, a mo e b i le beha io
wi h inc easing HNT fille concen a ion was obse ed. These
obse a ions we e demons a ed by cons an elonga ion a
b eak (abou 0.36 mm)dependency as shown in Figu e 3.
G aphene and halloysi e epoxy nanocomposi es 5
Based on he a o emen ioned ac s, i was assumed ha he
HNT nanofille inc eased he b i leness o he composi e due
o he limi ed mo emen o he s iffened HNT nano ubes
esul ing in he hinde ed gliding o he HNT nanofille s wi hin
he composi e ma ix.
The abo e-men ioned esul s o he uniaxial ensile
es s we e in excellen ag eemen wi h he obse ed ac-
u e oughness measu emen s (Figu e 4), whe e highe
ac u e oughness o 8.2 kJ/m
2
o epoxy/HNT nanocom-
posi es was ound compa ed o he 6.0 kJ/m
2
o epoxy/
GnP nanocomposi es (bo h a 1 w % fille concen a ion).
A highe HNT fille concen a ions (in he concen a ion
ange o 1–5w%)nonlinea dec easing end o ac u e
oughness was obse ed (Figu e 4).
In addi ion, he p esence o CTBN (Figu e 1c)ac ed
on he con inuous composi e ma ix as a kind o accel-
e a o , which o ces i o de elop local de o ma ions. The
de o ma ion mechanisms in he ma ix hen dissipa e he
ex e nal mechanical ene gy o e a la ge olume, hus
p e en ing he de elopmen o a single b i le c ack.
Op imal pe o mance o ubbe modifica ion equi es se -
e al condi ions o be me , namely he es ablishmen o
a wo-phase mo phology, he p o ision o sa is ac o y
in e acial adhesion, and he es ablishmen o a ce ain
c i ical dis ance be ween adjacen ubbe domains [9].
Analogous beha io was obse ed o mul i-phase ha d
and so segmen al flexible polyme s, whe e ha d phases
se ed as s iffening elemen and he so phases p o ided
elas ici y [44].
Resul s o he mic o-ha dness s fille concen a ion
measu emen s o bo h he s udied epoxy nanocomposi es
a e shown in Figu e 5. A nonlinea dec easing end o
he inden a ion modulus E
IT
wi h inc easing fille con-
cen a ion was obse ed. In he case o he epoxy/GnP
nanocomposi es, E
IT
dec eased om 4.3 GPa (nea ma ix)
o 3.4 GPa ( o 1 w % GnP nanocomposi e). Simila ly, in
he case o he epoxy/HNT nanocomposi es, E
IT
dec eased
om 4.3 GPa (nea ma ix) o 3.8 GPa ( o 5 w % HNT
Figu e 3: Nanofille concen a ion dependencies o he Young’s modulus o elas ici y and he elonga ion a b eak o he s udied GnPs and
HNT nanocomposi es. Applied de o ma ion a e was o 50 mm/min. Con inuous line –Young’s modulus o elas ici y, dashed line –
elonga ion a b eak.
Figu e 4: Nanofille concen a ion dependencies o he unno ched ac u e oughness o he s udied GnPs and HNT nanocomposi es.
6Lubomí Lapčík e al.
nanocomposi e). The plas icizing effec o he applied
nanofille s was assumed as he mos p obable cause o
his dec ease o su ace ha dness.
Resul s o he uniaxial h ee-poin bending es s o
he s udied nanocomposi es a e shown in Figu e 6. He e,
nonlinea dec easing pa e ns we e ound o bo h he
s udied nanocomposi es. Such beha io is ypical o
b i le ma e ials. A nonlinea dec ease o he bending
modulus (E
B
) om 4.3 GPa (nea ma ix) o 2.8 GPa ( o
1 w % GnP nanocomposi e)wi h inc easing GnP fille
concen a ion was ound. This effec was accompanied
by he inc easing g adual nonlinea end o he ob ained
magni udes o he elonga ion a b eak ( om 5.0 mm [nea
ma ix]) o 6.0 mm ( o 1 w % epoxy/GnP nanocompo-
si e), indica ing inc easing composi e duc ili y due o
he plas icizing effec o he nanofille o he p epa ed
epoxy/GnP nanocomposi es. In he case o he epoxy/
HNT nanocomposi es, E
B
nonlinea ly dec eased om 4.3 GPa
(nea ma ix) o 3.0 GPa ( o 5 w % epoxy/HNT nanocompo-
si es), indica ing dec easing mechanical s iffness o he s udied
ma e ials. Howe e , he opposi e, a mino dec easing non-
linea end o he elonga ion a b eak s HNT fille concen a-
ion, was ound, whe e he elonga ion a b eak dec eased om
5.0 mm (nea ma ix) o 4.1 mm ( o 5 w % epoxy/HNT nano-
composi es). These esul s indica ed highe b i leness o
he epoxy/HNT nanocomposi es compa ed o he epoxy/
GnP nanocomposi es.
Resul s o he dynamic mechanical es s o he s u-
died nanocomposi es a e shown in Figu es 7 and 8.
Typical equency dependencies o displacemen ans-
missibili y a e depic ed in Figu e 7. The ob ained esul s
we e in excellen ag eemen wi h he uniaxial ensile
measu emen s, indica ing inc eased ma e ial s iffness based
on he
R1
peak posi ion shi o he highe exci a ion e-
quencies acco ding o equa ion (4). Howe e , a mino
dec ease o he la e s iffness was ound o low fille
concen a ions, as indica ed by he negligible shi o he
R1
o he lowe magni udes (Figu e 7a and b). The effec o
he ine ial mass magni udes on he equency dependen-
cies o he displacemen ansmissibili y is demons a ed
Figu e 5: Nanofille concen a ion dependencies o he inden a ion modulus o he s udied GnPs and HNT nanocomposi es.
Figu e 6: Nanofille concen a ion dependencies o he bending modulus and he elonga ion a b eak o he s udied GnPs and HNT
nanocomposi es. Applied de o ma ion a e was o 50 mm/min. Con inuous line –bending modulus, dashed line –elonga ion a b eak.
G aphene and halloysi e epoxy nanocomposi es 7
in Figu e 7c and d. I was ound ha he inc easing ine ial
mass led o he dec ease o he fi s esonance equency
peak posi ion, he eby esul ing in he imp o ed ma e ials’
mechanical ib a ion-damping p ope ies [53].Inaddi-
ion, he ob ained inc easing
R1
wi h GnP concen a ion
again confi med ma e ials’inc easing s iffness, simila o
he case o he p e ious ensile and ac u e oughness
measu emen s (Figu es 3 and 4). The la e findings fi
e y well wi h he epoxy/GnP nanocomposi e esul s shown
in Figu e 8, whe e he linea inc ease o he
R1
wi h he fille
concen a ion was obse ed. In con as , ob ained esul s
o he epoxy/HNT nanocomposi es exhibi ed dec eased
Figu e 7: F equency dependencies o he displacemen ansmissibili y o he es ed GnPs and HNT nanocomposi es (Inse in a and b:
nanofille s concen a ions)wi h applied ine ial mass o 90 g (inse in c and d: applied ine ial masses).
Figu e 8: Concen a ion dependencies o he fi s esonance equencies o he s udied GnPs and HNT nanocomposi es. Inse legend:
ine ial mass used.
8Lubomí Lapčík e al.
mechanical s iffness as indica ed by dec easing
R1
wi h
inc easing fille concen a ion o he applied ine ial
masses.
5 Conclusions
The possibili y o elas ic–plas ic mechanical beha io mod-
ula ion by means o he applica ion o nanosized GnPs and
HNT fille s in he complex epoxy esin-based nanocompo-
si es was confi med in his s udy. A complex nonlinea pa -
e n o Young’s modulus o elas ici y wi h inc easing GnP
fille concen a ion was ound. Simul aneously, in he con-
cen a ion ange o 0–1w %GnPnanofille concen a ion,
an inc easing duc ili y o he s udied nanocomposi es was
ound, as eflec ed in he samples’inc eased elonga ion a
b eak. This kind o beha io was in e p e ed by he in e -
pa icle gliding effec o he indi idual GnP nanopa icles
dispe sed in he complex epoxy esin ma ix. A ela i ely
cons an end o Young’s modulus o elas ici y (app oxi-
ma ely o abou 2.8 GPa)accompanied by he simila non-
linea pa e n o elonga ion a b eak (app oxima ely o
0.35 mm) o he s udied epoxy/HNT nanocomposi es in
he concen a ion ange o 1–5w %wasalso ound.I
was a ibu ed o he hinde ed local mo emen o he HNT
nanofille s in he ma ix du ing mechanical es s. F ac u e
mechanical es s confi med ha he ac u e oughness
ob ained a low fille concen a ions was highe in he
case o he s iffepoxy/HNT nanocomposi es compa ed o
he epoxy/GnP nanocomposi es due o he GnP fille ’s
gliding-dissipa i e effec . As ob ained by he uniaxial
h ee-poin bending es s, he elonga ion a b eak mea-
su emen s confi med he enhanced plas ici y and duc i-
li y wi h inc easing GnP fille concen a ion o he com-
plex epoxy/GnP nanocomposi es. This was eflec ed in
he exceeding magni ude o he elonga ion a b eak o
6 mm compa ed o 5.3 mm o he epoxy/HNT nanocom-
posi es (bo h a 1 w % nanofille concen a ion). A simila
effec was also confi med by mic o-ha dness es s, whe e
he obse ed inden a ion modulus o 3.4 GPa o epoxy/
GnP nanocomposi es was lowe compa ed o 4.0 GPa o
epoxy/HNT nanocomposi es (bo h a 1 w % nanofille con-
cen a ion), hus indica ing mo e dissipa i e mechanical
beha io o he epoxy/GnP nanocomposi es. The la e we
asc ibed o he abo e-men ioned GnP nanofille gliding
ic ion. As a no el app oach, he nondes uc i e mechan-
ical ib a ion damping me hod o o ced oscilla ions was
applied in he low- equency egion o 2–3,200 Hz o
he compa ison o mechanical p ope ies based on he
fi s esonance equency peak posi ion. The plas ifica ion
effec o he epoxy/GnP nanocomposi es was confi med by
he lowe magni ude o he fi s esonance equency peak
posi ion o 2.6 kHz compa ed o he obse ed magni ude o
he
R1
o 2.8 kHz o epoxy/HNT nanocomposi es (bo h
esul s ob ained a 1 w % nanofille concen a ion and
ze o ine ial mass).
Funding in o ma ion: This s udy was suppo ed by he
Eu opean Regional De elopmen Fund in he Resea ch
Cen e o Ad anced Mecha onic Sys ems p ojec , p ojec
numbe CZ.02.1.01/0.0/0.0/16_019/0000867. LL and YM
would like o exp ess hei g a i ude o financing his
esea ch by he in e nal g an s o Palacky Uni e si y
in Olomouc IGA_P F_2022_020, IGA_P F_2023_024 and o
Tomas Ba a Uni e si y in Zlin (p ojec nos IGA/FT/2022/005
and IGA/FT/2023/007). Financial suppo o YM by
Fische schola ship o he Facul y o Science, Palacky
Uni e si y in Olomouc, in he yea 2022/2023, is also
g a e ully acknowledged.
Au ho con ibu ions: All au ho s ha e accep ed espon-
sibili y o he en i e con en o his manusc ip and
app o ed i s submission.
Conflic o in e es : The au ho s s a e no conflic o
in e es .
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