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Development of Ti–Nb–Zr alloys with high elastic admissible strain
for temporary orthopedic devices
Sertan Ozan a,b, Jixing Lin c,d, Yuncang Li e, Rasim Ipek b, Cuie Wen a,e,⇑
a Faculty of Engineering and Industrial Sciences, Swinburne University of Technology, Hawthorn, Victoria 3122, Australiab Department of Mechanical Engineering, Ege University, 35100 Bornova, Izmir, Turkeyc Advanced Material Research and Development Center, Zhejiang Industry & Trade Vocational College, Wenzhou, Zhejiang 325003, Chinad Department of Materials Science and Engineering, Jilin University, Changchun, Jilin 130025, Chinae School of Aerospace, Mechanical and Manufacturing Engineering, RMIT University, Melbourne, Victoria 3083, Australia
a r t i c l e i n f o
Article history:
Received 13 September 2014
Received in revised form 19 March 2015
Accepted 20 March 2015
Available online 25 March 2015
Keywords:
Elastic admissible strain
Cytocompatibility
TNZ (Ti–Nb–Zr) alloys
Mechanical properties
Young’s modulus
a b s t r a c t
A new series of beta Ti–Nb–Zr (TNZ) alloys with considerable plastic deformation ability during
compression test, high elastic admissible strain, and excellent cytocompatibility have been developed
for removable bone tissue implant applications. TNZ alloys with nominal compositions of Ti–34Nb–
25Zr, Ti–30Nb–32Zr, Ti–28Nb–35.4Zr and Ti–24.8Nb–40.7Zr (wt.% hereafter) were fabricated using the
cold-crucible levitation technique, and the effects of alloying element content on their microstructures,
mechanical properties (tensile strength, yield strength, compressive yield strength, Young’s modulus,
elastic energy, toughness, and micro-hardness), and cytocompatibilities were investigated and compared.
Microstructural examinations revealed that the TNZ alloys consisted of b phase. The alloy samples dis-
played excellent ductility with no cracking, or fracturing during compression tests. Their tensile strength,
Young’s modulus, elongation at rupture, and elastic admissible strain were measured in the ranges of
704–839 MPa, 62–65 GPa, 9.9–14.8% and 1.08–1.31%, respectively. The tensile strength, Young’s modulus
and elongation at rupture of the Ti–34Nb–25Zr alloy were measured as 839 ± 31.8 MPa, 62 ± 3.6 GPa, and
14.8 ± 1.6%, respectively; this alloy exhibited the elastic admissible strain of approximately 1.31%.
Cytocompatibility tests indicated that the cell viability ratios (CVR) of the alloys are greater than those
of the control group; thus the TNZ alloys possess excellent cytocompatibility.
2015 Acta Materialia Inc. Published by Elsevier Ltd. All rights reserved.
1. Introduction
According to a report by the United Nations in 2013 [1], the
population of the age group 60 years and older is increasing
rapidly, and in the more developed regions of the world, the ratio
of elderly people is expected to increase by 45% as of 2050.
Orthopedic biomaterials are implanted into human bodies in order
to heal bone tissue diseases developed due to aging, various con-genital defects in bone tissue, injuries to bone tissue and joints
from traffic and sports accidents [2,3].
With the increasing utilization of orthopedic implant materials,
if biologically and mechanically compatible materials are not used
for implants, it is inevitable that the number of revision surgeries
will increase [4]. Genotoxic, cytotoxic, carcinogenic, mutagenic,
allergenic, neurological effects are taken into account while
evaluating the biological compatibility of an implant material [5].
The formation of stress shielding may occur in cases where an
implant material with a higher Young’s modulus than that of bone
tissue is used [6]. Resorption in bone tissue can occur when it
carries lower amounts of biological load due to a rigid implant
material carrying most of the loads [7]. In such cases, the implant
material may loosen [6]. The fact that titanium (Ti) alloys have a
lower Young’s modulus in comparison with 316L stainless steeland Co–Cr alloys is an important factor in their increasing use as
implant materials [3].
Since Young’s modulus of the (a + b) Ti–6Al–4V alloy (at
110 GPa) [8] is about 4 times greater than that of cortical bone tis-
sue (max. 27 GPa) [9], b Ti alloys with a relatively lower Young’s
modulus in comparison with a + b Ti alloys have been developed
for orthopedic implant applications [10–16]. As it is well known,
among the Ti alloys, Ti–6Al–4V is still the most used one for ortho-
pedic applications, even though it contains vanadium, which is
defined as toxic [17], as well as having aluminum, for which
neurological side-effects [18], and genotoxic effects [19] have been
http://dx.doi.org/10.1016/j.actbio.2015.03.023
1742-7061/ 2015 Acta Materialia Inc. Published by Elsevier Ltd. All rights reserved.
⇑ Corresponding author at: School of Aerospace, Mechanical and Manufacturing
Engineering, RMIT University, Melbourne, Victoria 3083, Australia. Tel.: +61 3 9925
7290.
E-mail address: [email protected] (C. Wen).
Acta Biomaterialia 20 (2015) 176–187
Contents lists available at ScienceDirect
Acta Biomaterialia
j o u r n a l h o m e p a g e : w w w . e l s e v i e r . c o m / l o c a t e / a c t a b i o m a t
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reported. Another important consideration is that the cold-forming
capabilities of b Ti alloys (e.g. Ti–15Mo–5Zr–3Al) are much better
in comparison witha + b Ti alloys (e.g. Ti–6Al–4V) [20]. The super-
ior cold-forming ability of b Ti alloys decreases the manufacturing
cost, thus creating an advantage for them in becoming commercial
products [4].
The role of Ca–P formations on implant’s surface is to accelerate
the assimilation of implant material and bone-tissue [21]. For
instance, on the surface of bio-inert Zirconia, calcium phosphate
formation enabling a chemical bond with the surrounding bone-
tissue does not occur, it only ensures morphological fixation while
staying in the body [22]. Ca–P formations enable a tight bond
between the implant and surrounding bone-tissue [23]. On the
other hand, it is crucial to prevent the formation of fibrous tissue
between the bone-tissue and implants [24]. A direct contact with-
out fibrosis tissue between implant material and bone is defined
as osseointegration. [24]. Implants may be isolated due to fibrous
tissue formed between the bone tissue and implant [25]. It is
beyond doubt that fibrous tissue formation between the implant
and surrounding tissue is not desired, it is a prerequisite for both
temporary and permanent implant materials. Unlike osseointegra-
tion, chemical bonding between implant and bone tissue is related
to calcium phosphate forming ability of implants [26]. The fast
formation of fixation betweenthe implant materialand bone is pro-
vided by calcium phosphate precipitates on the surface of the
implant material, which thereby increases bone conduction [27].
Methods such as alkaline treatment [28], micro-arc oxidation [29]
and sol–gel [30] are used in order to enhance the adherence of
the implant material to the bone tissue or, in other words, to
increase chemical bonding ability by providing calcium phosphate
formation on the surface. Permanent implants (e.g. artificial joints
and dental implants) should have an assimilation ability with bone
tissue when assessed on the basis of clinic needs [31]. It is expected
that such an implant should offer excellent bioactivity [32]. It is
well known that artificial joints take on the natural joint function
by replacing the severely damaged joint. It is crucial to introduce
artificial joints having the ability of assimilation with bone tissuewhich ensures patients to carry out daily activities properly for
the rest of their lives [33]. When viewed under this aspect, the bone
conductivity of permanent implant materials should be high [31].
However, the reverse is required in removable implant applica-
tions [34]; that is, calcium phosphate precipitates are undesirable
on the surface of removable implants so as to minimize the bone
conductance of the implant material, and to prevent assimilation
between the bone tissue and the implant material [27]. Contrary
to permanent implants, the bonding between implant and bone
should be weak enough to prevent refracture of the bone during
removal surgery [35]. Trauma implants, e.g. bone nails, lose their
function after a healing period and they are removed after fracture
union [36]. Unlike artificial joints, trauma implants (e.g. bone nails)
do not lead to any restriction of movement function when removedfrom the body at an assigned time after healing period of the bone
tissue, i.e., it is not necessary to remain in the body permanently as
artificial joints. Because of the tendency of calcium phosphate pre-
cipitation on the surface of some Ti alloys, assimilation occurs
between the bone tissue and the implant material which makes
them unadaptable as a choice of temporary implants [31]. It is cru-
cial to avoid assimilation of these devices with bone tissue for an
easy removal surgery [37]. In cases where there is no assimilation
between bone and implant material, the occurrence of new bone
fractures during surgery to remove the implant material is mini-
mized, and so the removal surgery is easier [34]. Implant removal
becomes necessary with patient demands and complaints [38].
Especially in the cases of implants used for athletes engaged in
contact sports [39] and for children [40], the implants may beremoved after a healing period [34]. This necessitates the design
of materials with a low Young’s modulus and high mechanical
strength, as well as low bone conductance for removable implant
applications [31,34,41]. Problems that arise during implant
removal surgery due to the assimilation of the bone and the
implant material can be prevented by inhibition of calcium phos-
phate precipitations on the surfaces of the implant materials [34].
It is possible to prevent bone atrophy during the time that the
implant stays in the body by using implant materials with a low
Young’s modulus [42]. By minimizing or eliminating the stress
shielding effect with the use of implant materials that have a low
Young’s modulus, problems relating to long recovery times of
patients following removal operations [39] can be resolved.
The objective of this study was to develop Ti alloys with low
rigidity, high mechanical strength, and reasonable elongation at
rupture for removable bone tissue implant applications. To this
end, studies showing that zirconium (Zr) prevents calcium phos-
phate formation on the surface of a material [27,43,44] and studies
describing the mechanical properties and phase stability changes
of Ti–Nb–Zr alloys containing high amounts of Zr [45,46] were
taken into account, and TNZ alloys with high Zr element (between
25 wt.% and 40.7 wt.%) were manufactured. Niobium (Nb), another
of the alloy elements used in this study, is a b isomorphous alloy
element [47]. Whereas the effect of Zr on binary Ti alloys is evalu-
ated as either neutral or weak b stabilization, Zr functions as an
effective b stabilizer in multi-element Ti alloys that contain Nb
or Ta [48]. In this study, the effects of Zr and Nb content on the
microstructures, mechanical properties, and cytocompatibility of
TNZ alloys with different electronic parameters were investigated
and compared.
2. Materials and methods
2.1. Alloy design
Using a trial-and-error method for the design of Ti alloys results
in time-consuming and uneconomical manufacturing processes[49]. The approach developed by Morinaga et al. [50], known as
the d-electron alloy design method, exploits the relationship
between the phase stability and elastic properties of Ti alloys by
using the electronic parameters of average bond order (Bo) and aver-
agemetal d-orbital energylevel (M d) [48]. In theliterature,thereare
reports of many Ti alloys that have been designed using the d-elec-
tron alloy design method [11,51–53]. It was reported by Abdel et al.
[48] that Young’s modulus decreases along the b/b + x phase
boundary with an increase in Bo and M d values, as seen in the
Bo M d diagram (Fig. 1) (adapted and redrawn from Ref. [48],
Copyright (2006), with permission from Elsevier). b/b + x phase
boundary presented with a dotted curve in Fig. 1, means that, the
phase stability of titanium alloys depends on the amount of other
alloying elements (e.g. Hf, Zr), as explained in Ref. [45].Bo is the measure of the covalent bond strength between Ti and
the alloying element, whereas the M d of the alloying transition-
metal is a value that relates the metallic radius of the elements
and their electronegativities [48]; these two parameters are values
that have been theoretically determined using the orbital method
in body-centered cubic titanium using the DV-Xa molecular orbital
method [48,50]. The average Bo and M d values are calculated using
the formula given by [54]:
Bo ¼ R X iðBoÞi ð1Þ
M d ¼ R X iðM dÞi ð2Þ
where X i is the atomic ratio of the given element, (Bo)i is the bondorder value of the given element [54], and (M d)i is the metal
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d-orbital energy level of the alloying transition-metal value of the
given element [54].
In this study, we combined the d-electron alloy design method
[50] with the molybdenum equivalence (Moeq) [55] and electron to
atom ratio ((e/a)ratio) [20] approaches in the design of the TNZ
alloys. The Moeq values were designed to be larger than 6 and
the (e/a)ratio of the TNZ alloys were in the range of 4.18–4.25. The
electronic parameters of the alloys including the Bo M d values,
Moeq, and (e/a)ratio are summarized in Fig. 1 (adapted and redrawn
from Ref. [48], Copyright (2006), with permission from Elsevier).
The locations of the designed TNZ alloys are shown on the
Bo M d graph, above and as close as possible to the b/b + x phase
boundary.
2.2. Material preparation
Since Ti is very active chemically at high temperatures, difficul-
ties may arise in obtaining a chemically homogeneous structure in
the production of Ti alloys in traditional arc or induction melting
furnaces, so the cold-crucible levitation melting method is used
for the production of Ti alloys via casting [51]. This method ensures
that the alloy is melted without any contact between the melt and
the melting crucible, and is also not affected by the melting point
difference between Ti and the alloying element [51]. The nominal
compositions of the TNZ alloys were Ti–34Nb–25Zr, Ti–30Nb–
32Zr, Ti–28Nb–35.4Zr and Ti–24.8Nb–40.7Zr; these alloys are
hereafter denoted TNZ-1, TNZ-2, TNZ-3, and TNZ-4, respectively.
As seen in Fig. 1 (adapted and redrawn from Ref. [48], Copyright(2006), with permission from Elsevier), with an increase in the
concentration of Zr or a decrease in the concentrations of Nb and
Ti, the position of the alloy moves from TNZ-1 to TNZ-4 along
the b/b + x boundary. Simultaneously, the Bo M d values increase,
while the Moeq value and the (e/a)ratio decrease. In the diagram, the
positions of the alloys are situated just above the boundary with as
close proximity as possible. Ingots of the alloys were re-melted 5
times in order to guarantee chemical homogeneity. Commercially
pure titanium (CP-Ti) Grade-2, furnished as cold worked, was used
as a control group for tensile test, as well.
2.3. Microstructural characterization
Disk-shaped samples with a diameter of 8 mm and thickness of 2 mm were cut from the ingots for phase analysis, microstructure
examination, and micro-hardness measurements using electrical
discharge machining (EDM). The samples used for microstructure
examination, phase analysis, and micro-hardness measurements
were consecutively ground with SiC grinding papers of up to
4000 grit. Following the grinding process, the samples were
polished using a colloidal silica and H2O2 mixture suspension,
and afterward the samples were cleaned for 5 min in an ultrasonic
bath using ethanol. Phase analyses of the samples were carried out
using a Bruker D8 Advance X-ray diffractometer (XRD) with a Cu
Ka radiation source at room temperature. Microhardness measure-
ments were made on the polished surfaces of the samples in accor-
dance with procedure listed in ASTM standard E384-94 [56] by
using microhardness tester (Buehler Micromet 2100). Nine differ-
ent measurements were made, and the minimum and maximum
microhardness values were not taken into account when calculat-
ing the average micro-hardness values. The samples for
microstructure characterization were etched with Kroll solution.
The microstructure of TNZ alloys was examined by optical micro-
scopy (Leica-MEF4M).
2.4. Mechanical property testing
Tensile samples with a gauge section of 8 mm 2 mm 1 mm
were cut using EDM. Both surfaces of the samples were ground
with SiC grinding papers of up to 2400 grit. Tensile tests were
carried out at 0.5 mm/min cross-head speed at room temperature
using an Instron 5567 testing system with advanced video exten-
someter. The gauge length of 8 mm was marked prior to the test
so that the video extensometer could detect it. Using the stress–
strain curves obtained from the tensile tests, tensile strength, yield
strength, Young’s modulus, elastic energy, toughness and elonga-
tion at rupture of the TNZ alloys were measured.
The slope of the linear part of the stress–strain curves was deter-
mined as Young’s modulus, and the 0.2% offset yield method was
used to determine the yield strength of the TNZ alloys. Tensile tests
were repeated on 5 samples for each alloy, and the average values
obtained from the 5 measurements were used in the calculationof the mechanical properties. The fracture surfaces of the tensile
samples were examined using field-emission scanning electron
microscopy (SEM, ZEISS SUPRA 40 VP). Cylindrical samples 5 mm
in diameterand 8 mmin lengthweremachined using EDM for com-
pression tests. The tests were carried out at a cross-head speed of
0.5 mm/min, using an MTS testing system at room temperature in
accordance with procedure listed in ASTM standard E9-09 [57].
The compressive yield strength of the TNZ alloys was calculated
from the averages of 3 samples for each alloy. As it is seen in
Fig. 5 (indicated by blue arrow), the compressive stress–strain
graph of TNZ alloys display ‘‘pre-deformation phenomenon’’ [58]
which makes it impossible to use the 0.2% offset approach for
calculating the compressive yield strength of the alloys.
Consequently, ‘‘two lines method’’ [58] was used to be able to cal-culate the compressive yield strength of the alloys.
2.5. MTS assay
Disk samples 8 mm in diameter and 2 mm in thickness for cell
culture were cut from the ingots using EDM. All samples for the
cytocompatibility assessment were sterilized in a muffled furnace
at 180 C for 3 h. The cytocompatibility of all alloys was evaluated
using a direct cell method according to the International Standard
ISO10993-5 [59]. The disk shaped TNZ and CP-Ti specimens were
put into the wells of the cell culture plate. At a density of 5 103
cells per well (Barwon Biomedical Research, Geelong Hospital,
Victoria, Australia) were seeded onto the surface of the samples.
In order to determine the in vitro proliferation of cells, MTSassay was used [60,61]. The cell morphology was observed by
Fig. 1. Location of TNZ alloys on B o M d map and electronic parameters of TNZ
alloys (adapted and redrawn fromRef. [48], Copyright (2006), withpermission from
Elsevier).
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means of SEM after cell culturing. Prior to SEM observation of
SaOS2 cells attached to the surface of samples, a series of processes
were carried out. Samples, on which cells were seeded, were fixed
in glutaraldehyde (3.9%) at room temperature for 1 h. Following
this process, dehydration of cells was performed by washing con-
secutively in ethanol solutions with a concentration of 60%, 70%,
80%, 90%, and 100%. Chemical drying of samples was performed
by using hexamethyldisilazane. Finally, by coating the samples
with gold, the samples were made ready for SEM observation. In
this study, all cell culture experiments were conducted in triplicate
and results were stated as means ± standard deviations.
2.6. Statistical analysis
The mechanical property values (tensile and yield strength,
Young’s modulus, elongation at rupture, elastic energy, toughness,
compressive yield strength, micro-hardness) and cell adhesion
density values were analyzed by using one-way ANOVA
(q < 0.05) followed by Tukey HSD post hoc test. q < 0.05 was taken
into consideration statistically significant.
3. Results and discussion
3.1. Microstructure of the TNZ alloys
It was determined following microstructural examinations that
the TNZ alloys display primary grain boundaries together with sec-
ondary grain structure, as shown in Fig. 2. In Fig. 2(c), dendritic
structure was clearly observable.
The XRD patterns of the TNZ alloys are given in Fig. 3. As shown,
only b diffraction peaks were detected in each TNZ specimen. The
diffraction peaks of b Ti shifted toward lower 2h degree values with
increases in the amount of Zr or decreases in the amounts of Nb
and Ti in the alloys. Similar results were reported by Ning et al.
[62]; however, in that study [62], the Nb level was kept constant
while increasing the Zr and decreasing the Ti, and it was suggested
that, as a result of the increase in Zr, the atomic radius of which is
larger in comparison with Ti, a greater number of Zr atoms
replaced Ti atoms, resulting in a shift of the peaks toward lower
2h degree values [62].
3.2. Micro-hardness of the TNZ alloys
Fig. 4 presents the microhardness of the alloys in comparison
with that of other Ti alloys as published in the literature, respec-
tively. As seen in Fig. 4, it is worth noting that the average micro-hardness levels of TNZ-1 (241.3 HV), TNZ-2 (244.4 HV), TNZ-3
(244.0 HV) and TNZ-4 (235.6 HV) are higher than those of CP-Ti
(134.0 HV) [63], Ti–29Nb–13Ta–4.6Zr (solution treated condition
– 180 HV) [64] and Ti–13Nb–13Zr (solution treated condition –
235 HV) [65], and lower than that of Ti–6Al–4V (as-cast – 294
HV) [66]. The micro-hardness value of the TNZ-1,2,3 alloys was sig-
nificantly (q < 0.05) higher than that of the TNZ-4 alloy. When
ranked the average micro-hardness value of TNZ alloys among
themselves, the alloys are ranked TNZ-2 > TNZ-3 > TNZ-1 > TNZ-4.
3.3. Compressive properties of the TNZ alloys
The compressive stress–strain graphs of the TNZ alloys are
shown in Fig. 5. It can be seen that under compression, the alloysexhibited considerable plastic deformation ability. As seen in
Fig. 5, the room temperature compression stress–strain curve of
the TNZ alloys is consisted of ‘‘elastic stage (I), a plastic yield plateau
stage (II), a parabola stage (III)’’ [67], consecutively. TNZ-2 displayed
the highest compressive yield strength among all the TNZ alloys,
and TNZ-3 displayed a compressive yield strength very close to
that of TNZ-2. Representative images of the alloy samples taken
before and after compression are inserted in Fig. 5, showing that
neither cracking nor fracturing was observed. Compression tests
were stopped after reaching a strain value of 65%.
The average compressive yield strength of the TNZ alloys is
given in Fig. 6. There are no significant (q > 0.05) differences
among the compressive yield strength of the alloys. However,
when a ranking in terms of average compressive yield strength is
made, the alloys are ranked TNZ-2 > TNZ-3 > TNZ-1 > TNZ-4. The
small differences among the compressive yield strengths of the
Fig. 2. Optical micrographs of as-cast TNZ alloys: (a) TNZ-1; (b) TNZ-2; (c) TNZ-3; (d) TNZ-4.
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alloys may have been caused by different second-phase particles
[68], grain size, or solid-solution strengthening effects [69].
Similarly, it can be observed that the microhardness levels of the
alloys present the same ranking order (Fig. 4).
It is worth noting that the compressive yield strength of the TNZ
alloys is about 4 times greater than the compressive yield strength
of bone tissue (Human Haversian: 180 MPa) [70]. However, in
recent years, metal foam materials have been manufactured that
compromise on the mechanical strength of the implant material
in order to ensure that the Young’s modulus value of the material
is similar to that of bone tissue [61,71]. Even though the design of
foam material takes bone ingrowth into consideration [72], the use
of such materials, especially for orthopedic implants carrying high
loads, is still uncommon due to the fact that metal foams possess
Fig. 3. XRD patterns of as-cast TNZ alloys.
Fig. 4. Microhardness of TNZ alloys in comparison with those of other Ti alloys published in the literature.
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lower mechanical strength, i.e. fatigue strength, tensile strength
and compression strength, in comparison with their solid counter-parts [73]. The fact remains that, metal foams also possess lower
corrosion resistance [74].
3.4. Tensile properties of the TNZ alloys
Fig. 7 shows the stress–strain graphs of the TNZ alloys obtained
via tensile tests. The tensile properties (tensile strength, yield
strength, and elongation at rupture) of the alloys are given in
Fig. 8. TNZ-1 exhibited the highest average tensile strength and
yield strength, and largest elongation. The ranking of the average
tensile strength, yield strength, and elongation of the alloys from
the highest to lowest is TNZ-1 > TNZ-2 > TNZ-3 > TNZ-4. In particu-
lar, the elongation at rupture of the alloys was in the range of 9.9–14.8%. When the TNZ alloys were evaluated statistically among
themselves; it was determined that the tensile and yield strength,
elongation at rupture, toughness, elastic energy of TNZ-1 were sig-
nificantly (q < 0.05) higher than TNZ-3 and TNZ-4 alloy. The fact
remains that, TNZ-2 had significantly (q < 0.05) higher tensile
and yield strength, elongation at rupture, toughness and elastic
energy than that of the TNZ-4, as well. However, there were no sig-
nificant differences (q > 0.05) in terms of Young’s modulus among
TNZ alloys. The tensile strength, yield strength, Young’s modulusand elongation at rupture of the CP-Ti, used as a control in this
study, were measured as 758 ± 14.1MPa, 607 ± 10.3 MPa,
109 ± 1.1 GPa, and 26 ± 0.2%, respectively. By statistically compar-
ing Young’s modulus of CP-Ti and TNZ alloys, it was determined
that CP-Ti had significantly (q < 0.05) higher Young’s modulus in
comparison with TNZ alloys.
It is noticeable that the elongation values of these as-cast TNZ
alloys are comparable to or slightly higher than those of the
thermomechanically processed biomedical Ti alloys currently in
use, such as Ti–12Mo–6Zr–2Fe [75], Ti–6Al–7Nb [76], Ti–15Mo
[77], Ti–13Nb–13Zr [78] and as-cast Ti–6Al–4V [79] with elonga-
tions of 12%, 10%, 12%, 15% and 8%, respectively. It should be noted
that as-cast Ti alloys generally present relatively lower elongation
values compared to those of their thermomechanically processedcounterparts [8]. However, the as-cast TNZ alloys studied in this
research exhibited fairly large elongation values that are compara-
ble to those of the annealed Ti alloys noted above.
In the case of the elastic deformation of material, the ability to
release absorbed energy on unloading is known as resilience, and
this property is measured by the resilience modulus or elastic
energy [80]. In calculating the elastic energy of the TNZ alloys,
the yield strength was taken as the elastic limit [80]. Toughness
is a measure indicating the ability of a material to absorb energy
during tensile deformation till fracture [80]. The toughness values
obtained by calculating the area under the tensile curve along with
the elastic energy values denoting the absorbed energy when the
alloys deformed elastically, and Young’s modulus values of
the alloys are given in Fig. 9. The elastic energy and toughness of the alloys were calculated using a Matlab-R2012b. The ranking
Fig. 5. Compressive stress–strain curve of as-cast TNZ alloys.
Fig. 6. Compressive yield strength of as-cast TNZ alloys.
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of the toughness and elastic energy of the alloys from the highest
to lowest is TNZ-1 > TNZ-2 > TNZ-3 > TNZ-4. As seen in Fig. 9, the
average Young’s modulus of the alloys was in the range of
62–65 GPa.
Ti alloys that are used as implant material are required to pos-
sess high mechanical strength and a low Young’s modulus, so thatthey can safeguard the host bone tissue without causing stress
shielding, which could lead to bone resorption and cause implant
loosening [81]. The mechanically compatible performance of an
orthopedic implant material can be evaluated by the elastic admis-
sible strain [82], the ratio of yield strength to Young’s modulus of
the material given by [4]:
d ¼ r=E ð3Þ
Fig. 7. Tensile stress–strain curves of as-cast TNZ alloys.
Fig. 8. Tensile mechanical properties (tensile strength, yield strength and elongation at rupture) of TNZ alloys.
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where d is the elastic admissible strain, r is the yield strength and E
is Young’s modulus of the material.
The mechanical properties of the TNZ alloys investigated in this
study, and of Ti–16Nb–10Zr [83] and some of the commercial Tialloys [8,81,84] published in the literature are listed in Table 1.
As can be seen, the elastic admissible strain values of the TNZ
alloys are in the range of 1.08–1.31%, and the highest elastic admis-
sible strain value for commercial Ti alloys stated in Table 1 is 0.99%
for annealed Ti–35.3Nb–5.1Ta–7.1Zr [8]. It can be concluded that
the TNZ alloys would offer promising performance in practical
applications in terms of mechanical compatibility. The Young’s
modulus values of TNZ-1, TNZ-2, TNZ-3, and TNZ-4 are 62.0 ± 3.6,
65.0 ± 4.2, 64.0 ± 4.5 and 63.0 ± 4.2 GPa, respectively. Young’s
modulus values of the TNZ alloys are lower than those of pure
CP-Ti (104 GPa) [8] and mill-annealed Ti–6Al–4V (110 GPa) [84],
and close to those of Ti–35.3Nb–5.1Ta–7.1Zr (55 GPa) [8] and
Ti–29Nb–13Ta–4.6Zr (60 GPa) [81].
The fracture surfaces of the TNZ alloys after tensile tests areshown in Fig. 10. It can be seen that the alloys exhibited a ductile
fracture surface with numerous dimples, exemplified by the white
arrows in Fig. 10(a–d). It is noticeable that the number of dimples
for TNZ-1 is particularly large and the dimples observed on the
fracture surface are deeper, in comparison with TNZ-2, TNZ-3,and TNZ-4. In addition, cleavages (indicated by the black arrows
in Fig. 10) were observed accompanying the dimples on the frac-
ture surfaces of the alloys. In particular, cleavage was the predomi-
nant fracture mechanism in TNZ-4. It is well known that the
fracture surfaces of ductile materials are rougher, whereas those
of brittle materials are smooth. Intergranular fracturing, which is
one of the indicators of brittle fracturing, was not observed on
the fracture surfaces of the alloys.
3.5. Cytocompatibility of the TNZ alloys
The healthy adhesion of osteoblast cells to the implant surface,
and their growth and proliferation, are important indicators of thecytocompatibility of the implant materials [61]. To this end, the
Fig. 9. Tensile mechanical properties (Young’s modulus, elastic energy and toughness) of TNZ alloys.
Table 1
Comparison of mechanical properties of TNZ alloys with those of some commercial titanium alloys.
Ti alloys Yield strength
(MPa)
Tensile strength
(MPa)
Young’s
modulus (GPa)
Elongation (%) Elastic admissible
Strain (%)
Alloy type References
Pure Ti (Grade 4) 485 550 104.1 15 0.47 a [8]
Ti–16Nb–10Zr (annealed) 485 520 70 22 0.69 b + a’’ [83]
Ti–15Mo (annealed) 544 874 78 21 0.70 b [84]Ti-6-4 ELI (mill annealed) 875 965 110 10–15 0.80 a + b [84]
Tiadyne 1610 (aged) 736 851 81 I0 0.91 b [84]
Ti–35.3Nb–5.1Ta–7.1Zr (annealed) 547 597 55 19 0.99 b [8]
Ti–29Nb–13Ta–4.6Zr (annealed) – 549 60 41.6 – b [81]
CP-Ti (cold worked) 607 ± 10.3 758 ± 14.1 109 ± 1.1 26 ± 0.2 0.56 a [This study]
Ti–34Nb–25Zr (TNZ-1) 810 ± 48.0 839 ± 31.8 62 ± 3.6 14.8 ± 1.6 1.31 b [This study]
Ti–32Zr–30Nb (TNZ-2) 782 ± 18.8 794 ± 10.1 65 ± 4.2 13 ± 1.8 1.20 b [This study]
Ti–35.4Zr–28Nb (TNZ-3) 729 ± 26.3 755 ± 28.3 64 ± 4.5 11.3 ± 1.5 1.14 b [This study]
Ti–40.7Zr–24.8Nb (TNZ-4) 682 ± 52.9 704 ± 49.5 63 ± 4.2 9.9 ± 1.1 1.08 b [This study]
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in vitro cytocompatibility of the TNZ alloys was assessed using
SaOS2 cells.
Following the cell culture of the TNZ alloys for 24 h, the surfaces
of alloys were examined in terms of the morphology of osteoblastcells using SEM. The adherence of osteoblast cells to the surfaces of
the samples is shown in Fig. 11. It can be seen that the osteoblast
cells started to proliferate following 24 h of cell culture. The osteo-
blast cells on the alloy surfaces display a polygonal morphology,
and a large number of filopodia have formed, providing anchoring
of the osteoblast cells on the materials’ surfaces (Fig. 11). The for-
mation of filopodia on the surfaces after cell culture is an indica-
tion that the initial cell adhesion and the growth of the cells
were healthy and strong [85]. Thus it can be concluded that the
TNZ alloys are favorable for cell growth and proliferation.
SEM images of the SaOS2 osteoblast cells on the surfaces of the
TNZ alloys after cell culture for 7 days are given in Fig. 12. It can be
seen that the SaOS2 cells display a healthy growth on the surfaces
of the alloys. Numerous osteoblast cells firmly adhered to andspread over the alloy surfaces. There was no difference in terms
of the morphology of the osteoblast cells on the four different alloy
surfaces (Fig. 12). Unhealthy cells are distinguished from healthy
cells on the basis of their reduced cell morphology caused by
shrinkage of the cells [86]. When this morphological property
specific to unhealthy cells was considered, it was observed that
very healthy cells proliferated on the surfaces of the alloys.
Fig. 13 shows a comparison of cell adhesion density for the TNZ
alloys and CP-Ti after 7 days of cell culture. After assessment of the
images of the osteoblast cells on the alloy surfaces, along with the
cell adhesion densities given in Fig. 13, it can be concluded that
osteoblast cells adhered well to the surfaces, and spread and grewin a healthy way. As can be seen from Fig. 13, the average cell adhe-
sion density of the TNZ alloys is greater than that of CP-Ti. Ranking
of the TNZ alloys and CP-Ti in terms of average cell adhesion den-
sity is TNZ-4 > TNZ-3 > TNZ-2 > TNZ-1 > CP-Ti. No significant dif-
ferences (q > 0.05) were confirmed in cell adhesion densities
between CP-Ti and TNZ-1, TNZ-2, TNZ-3 alloys. However, the cell
adhesion density of TNZ-4 was significantly (q < 0.05) higher than
CP-Ti. According to the obtained results, an increase in Zr in the
TNZ alloys and decreases in Nb and Ti result in an increase in cell
adhesion density. The highest cell adhesion density among the
alloys is that of TNZ-4, which also has the highest Zr (40.7%) and
the lowest Nb (24.8%) and Ti (35.5%). The three elements of Ti,
Nb, and Zr are all biocompatible elements, as previously reported
[87–89].Cells were seeded in the wells having only the medium within,
as well. As a negative control, they were incubated for the same
days. The cell viability ratios (CVR) of CP-Ti and the TNZ alloys
were calculated by dividing the live SaOS2 cell number inside the
experimental wells by the live SaOS2 cell number inside the con-
trol; the control group has a CVR of 1 and is accepted as being
cytocompatible as a reference in determining the cell viability
ratios of samples [85]. Fig. 14 presents the CVR values that enabled
assessment of the in vitro cytotoxicity of the TNZ alloys and CP-Ti.
The CVR values of the TNZ alloys were all greater than those of the
control group; hence it can be deduced that the alloys possess
exceptional cytocompatibility. In addition, the cell proliferation
ratios were similar in the experimental wells of the CP-Ti and
TNZ disks, so their cell viability ratio values are also very close(Fig. 14).
Fig. 10. Fracture surfaces of as-cast TNZ alloys (a) TNZ-1; (b) TNZ-2; (c) TNZ-3; (d) TNZ-4.
Fig. 11. Morphology of SaOS2 cells attached on the surface of TNZ-2 alloy after cell
culture for 24 h.
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4. Conclusions
The microstructures, mechanical properties and cytocompati-
bility of the as-cast Ti–Nb–Zr alloys have been examined. The con-
clusions are as follows:
1. Microstructural examinations revealed that the TNZ alloys dis-
play primary grain boundaries together with secondary grain
structure.
2. The average compressive yield strength and microhardness
values of the TNZ alloys exhibited the same ranking: TNZ-
2 > TNZ-3 > TNZ-1 > TNZ-4. The alloys exhibited considerable
ductility under compression and no fracturing or cracking was
observed on the samples after the compression tests. The com-
pressive yield strength of thealloys rangedfrom713 to 751 MPa.
3. Tensile test results showed that the TNZ alloys have elongation
at rupture values in the range of 9.9–14.8%, which is highly
desirable for biomedical applications. The tensile strength of
the TNZ alloys was in the range of 704–839 MPa and Young’s
modulus was in the range of 62–65 GPa.
4. The TNZ alloys exhibited elastic admissible strain values in the
range of 1.08–1.31%. Ti–34Nb–25Zr exhibited an elastic admis-
sible strain of 1.31%, the highest value compared to TNZ alloys
studied in this project.
Fig. 12. SEM images of SaOS2 cells attached on to surfaces of TNZ alloys after cell culture for 7 days: (a) TNZ-1; (b) TNZ-2; (c) TNZ-3; (d) TNZ-4.
Fig. 13. SaOS2 cell adhesion density of as-cast TNZ alloys and CP-Ti after cell culture for 7 days.
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5. The tensile strength, yield strength, elongation, elastic energy,
and toughness of the TNZ alloys all decreased when the Zr con-
tent increased and the amounts of Ti and Nb decreased. In other
words, the tensile mechanical properties decreased with a
decrease in the (e/a)ratio and Moeq values.
6. The TNZ alloys exhibited excellent cytocompatibility on SaOS2
cells.
7. The TNZ alloys designed in this study are suitable candidates for
removable orthopedic implant applications due to their high Zr
content, high elastic admissible strain value, superior plastic
deformation ability during compression test, and excellent
cytocompatibility.
Acknowledgments
SO would like to acknowledge the Council of Higher Education
(CoHE) of Turkey for PhD research scholarship. CW acknowledges
the financial support from the Australian Research Council (ARC)
through the ARC Discovery Project DP110101974.
Appendix A. Figures with essential color discrimination
Certain figures in this article, particularly Figs. 5 and 7–9 are dif-
ficult to interpret in black and white. The full color images can be
found in the on-line version, at http://dx.doi.org/10.1016/j.actbio.
2015.03.023.
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