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Microstructure changes of extruded ultra high
molecular weight polyethylene after gamma irradiation
and shelf-aging
F.J. Medela, F. Garca-A lvarezb, E. Go mez-Barrenac, J.A. Pue rtolasa,)
aDepartment of Materials Science and Technology, Centro Politecnico Superior de Ingenieros, Universidad de Zaragoza,
Calle Mar a de Luna 3, 50018 Zaragoza, SpainbDepartment of Orthopaedic Surgery, Hospital Lozano Blesa, Zaragoza, Spain
cDepartment of Orthopaedic Surgery, Hospital Fundacion Jimenez Daz, Universidad Autonoma de Madrid, Madrid, Spain
Received 16 September 2004; accepted 27 November 2004
Available online 2 February 2005
Abstract
Ultra high molecular weight polyethylene (UHMWPE) components in joint prostheses may undergo oxidative degradation in the
long term. This leads to material embrittlement, associated with a subsurface defect named white band that favours surface
delamination and premature implant failure. The polymer microstructure, which affects the mechanical properties of the material, is
altered by oxidative degradation. In this study, the microstructure of bar-extruded UHMWPE (GUR 1050) was compared before
irradiation, one week after 25 kGy gamma irradiation in air (GUR 1050), and 7 years after commercial (25e40 kGy) gamma
irradiation in air and shelf-aging (GUR 415). This was performed using transmission electron microscopy (TEM) and differential
scanning calorimetry (DSC) which help to characterize the changes in material microstructure and crystallinity during degradation.
Quantitative (lamellar thickness), semiquantitative (lamellar twisting, orientation, lamellar density), and qualitative (lamellarborder, stacking) parameters were recorded in the surface, subsurface and inner material. There was an evolution in the degradation
in the bar-extruded UHMWPE microstructure during irradiation and shelf-aging. Changes in the in-depth microstructure indicate
the progression of an oxidation front. The stacking or high lamellar concentration in the subsurface in shelf-aged samples was
coherent with higher crystallinity and with a degradation process controlled by oxygen diffusion and free radical distribution after
gamma irradiation.
2005 Elsevier Ltd. All rights reserved.
Keywords: UHMWPE; Microstructure; TEM; DSC; Degradation
1. Introduction
In the past decades, ultra high molecular weight
polyethylene (UHMWPE) has been the preferred
interposition material for joint prostheses. Its micro-
structure, based on the extremely high molecular weight
(4e6! 106 g/mol), confers optimal mechanical proper-
ties such as high wear and fatigue resistance and highfracture toughness. Those properties, along with a low
friction coefficient and high biocompatibility, make
UHMWPE the perfect candidate to articulate against
metallic alloys or ceramics [1]. However, wear and
degradation can limit the in vivo service and duration of
the reconstructed joint system [1,2].
The UHMWPE microstructure includes an amor-
phous region, with entangled long molecular chains, and
a crystalline region, with thin lamellar crystals or
) Corresponding author. Tel.: C34 976762521; fax: C34
976761957.
E-mail address: [email protected] (J.A. Pue rtolas).
0141-3910/$ - see front matter 2005 Elsevier Ltd. All rights reserved.
doi:10.1016/j.polymdegradstab.2004.11.015
Polymer Degradation and Stability 88 (2005) 435e443
www.elsevier.com/locate/polydegstab
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lamellae. Both regions are separated by a narrow border
which is considered a part of the lamella. Tie molecules
interconnect the regions by crossing the amorphous
region from one lamella to another. The tie molecules
and entanglements in the amorphous phase are what
help to provide the excellent mechanical properties of
this material [3,4].The material has usually been irradiated for sterili-
zation (between 25 and 40 kGy), but this has a negative
effect on the entanglement density of long molecular
chains, as well as the concentration of tie molecules [5].
Molecular chains undergo scission and free radicals
appear in the amorphous region and on the crystal
surfaces. The free radicals can take part in the cross-
linking of the material or oxidative degradation in the
presence of oxygen [5,6]. In the amorphous region, free
radicals disappear by recombination or by reacting with
oxygen since the molecular chain is more mobile and
oxygen easily diffuses in this phase. However, in the
crystalline regions of UHMWPE, radicals are long
lasting [7]. They diffuse towards the amorphous region
at a slow rate and participate in different stages of
oxidation. Finally, UHMWPE also contains degrada-
tion products such as ketones, acid groups, and esters,
as shown by FTIR [8].
Natural aging of UHMWPE on the shelf and in vivo
cause maximum subsurface degradation (between 1 and
2 mm under the surface) [9]. The oxidation causes
embrittlement of the material and loss of mechanical
properties. As a result, research in orthopaedics has
focused on the physico-chemical characterization of the
degradation. Many studies have been performed usingdensity measurements, calorimetry, and FTIR [10e22].
However, it is still unclear how aging changes the
microstructure and how it affects degradation profiles.
Advances in this area could help to explain how
UHMWPE loses its mechanical properties.
We analysed the microstructural variations due to
irradiation and aging in bar-extruded UHMWPE.
Differential scanning calorimetry (DSC) and transmis-
sion electron microscopy (TEM) studies were performed
to determine depth-dependent changes in microstruc-
tural characteristics of non-irradiated material, freshly
gamma irradiated in air, and shelf-aged gamma
irradiated in air commercial components. We propose
a model of microstructural changes based on our
findings and previous reports in the literature.
2. Materials and methods
2.1. Materials
The polyethylene resins were bar-extruded Ticona
GUR 1050 processed by a commercial converter (Perplas
Medical Ltd.), and components manufactured from
bar-extruded Hoechst GUR 415 or 4150 according to
the new nomenclature [2]. The experimental samples
made from the resins were classified into three different
groups.
The first group was from three pucks (10 mm thick),
machined from a bar of extruded GUR 1050. Three
sections were cut from the centre of each puck witha microtome, at 0.1e0.3 mm, 1 mm, and 3 mm from the
surface. Samples were prepared for DSC and TEM tests
from every 200 mm thick section.
The second group consisted of three pucks machined
from extrusion bars of GUR 1050 UHMWPE, and then
gamma irradiated in air at conventional sterilization
dosage (25 KGy; Aragogamma, Spain). Again, three
sections were extracted from the centre of each puck
(0.1e0.3 mm, 1 mm, and 3 mm from the puck surface).
Those sections were used for DSC analysis and TEM,
and tested one week after the irradiation process.
The third group corresponded to naturally shelf-aged
Hoechst GUR 415 material, obtained from three tibial
components of knee prostheses that had never been
implanted (Natural Knee system, manufactured by
Intermedics Orthopedics, Austin, TX, in 1991). They
were discarded for clinical use after being stored for 7
years on the shelf after sterilization. All prostheses had
a wide subsurface white band in sections. On the back of
the component we cut 200 mm sections at different
depths to obtain a surface group (0.1e0.3 mm deep),
a white band or subsurface group (1 mm deep), and an
inner material (below white band, 3 mm deep). The
samples of each section were divided in two parts, one
for DSC measurements and another for TEM.
2.2. Transmission electron microscopy
Subsequent sample preparation for TEM included
different phases. First, 200 mm sections of UHMWPE
were stained with 99% chlorosulphonic acid at 60 C
for 5 h, which is thought to stabilize the amorphous
regions. Samples were washed with acetone (at 0 C)
and rinsed with distilled water. Stained samples were
dried at 60 C for 1 h and later embedded in epoxy and
cured at 60 C for 2 days. Ultrathin sections (w60 nm
thick) were cut with a diamond knife and collected on
carbon grids. Then the sections were post-stained with
uranyl acetate in 1% methanol for 4 min. A Jeol 100CX
TEM (operating at 100 kV) was used to produce
micrographs at 20,000! and 60,000! magnifications.
The best 5 TEM preparation samples were chosen from
each group and analysed using the Digital Micrograph
3.3.1 software package (Gatan Inc., Pleasanton, CA,
USA).
Morphological variables were selected by image
analysis and evaluated quantitatively or semiquantita-
tively. These variables assessed lamellar properties
(thickness, boundaries, kinking) and interlamellar
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features (distance or spacing, chaotic distribution,
concentration, stacking). Some were ranged on a
semiquantitative scale of one dot (minimum) to three
dots (maximum). Lamellar thickness and interlamellar
distance in stacked lamellae were measured at least five
times per 60,000! images using the software.
2.3. Differential scanning calorimetry
A PerkineElmer DSC-7 was used for the calorimetric
analysis. Samples were heated from 25 to 180 C at a rate
of 10 C/min. Their mass ranged from 3e4 mg. Fusion
heat was obtained by integrating the area under the
endothermic peak from 80 C to 160 C. Melting
temperature was registered as the maximum of the
endothermic melting peak. In addition to the direct
parameters, sample crystallinity was calculated by com-
paring the fusion heat of the sample to the fusion heat for
a fully crystalline polyethylene material (290 J/g) [17]. An
estimation of the lamellar thickness, Lc, was obtained
from DSC data using the ThomsoneGibbs equation:
TmZTm0
1 2s=LcrcDH0m
1
where Tm is the melting point of the polymer, Tm0 is the
equilibrium melting point of a perfect crystalline poly-
ethylene, s the specific surface energy, rc the crystallinity
phase density, and DH0m the enthalpy of melting of
a perfect crystalline polyethylene. Lamellar thickness
was estimated by considering DH0mZ 290 J/g, Tm0Z
145.7 C, rcZ 1.005 g/cm3, and taking a constant value
for sZ
93! 10
7
J/cm
2
[18].
3. Results
3.1. Calorimetric analysis
The thermogram of the ram-extruded material was
fairly typical, with a strong endothermic peak (Fig. 1a).
As seen in Table 1, non-irradiated specimens had
a melting temperature of 135.5G 1.1 C, an enthalpy
content of 140G 12 J/g, a crystallinity percentage of
49G 4%, and an estimated lamellar thickness (using the
ThomsoneGibbs equation) of 27G 3 nm. In the first
group, there were no significant differences between
specimens from different depths.
Gamma-irradiated, one week shelf-aged UHMWPE
samples had a higher melting temperature (137.3G
0.4 C) and crystallinity (53G 1%; Table 1). Lamellar
thickness was also higher (32G 2 nm) than virgin
UHMWPE. As in non-irradiated samples, there were
no significant differences with depth in the DSC results.
A typical thermogram of irradiated UHMWPE is shown
in Fig. 1a, along with the thermogram of virgin
UHMWPE.
Finally, the thermal values of samples from aged
tibial components varied with depth. Fig. 1b shows the
typical thermograms of the three regions. Samples from
the subsurface (where the white band was present), had
the highest crystallinity (71G 3%), and an increased
melting temperature (139.8G 1.2 C), as well as higher
lamellar thickness (48G 9 nm). In contrast, surface
specimens had the lowest enthalpy content, melting
temperature (137.1G 0.1 C), and lamellar thickness
(32G 1 nm). Inner samples, which were already near the
wide white bands of the prostheses, had an enthalpy of
190G 1 J/g, crystallinity percentage of 65G 1, melting
temperature of 140.1G 1.0 C and lamellar thickness of
50G 9 nm. The direct parameters obtained from the
Fig. 1. (a) Thermograms of virgin, non-irradiated, UHMWPE, and
gamma-irradiated (25 kGy) plus one week shelf-aging UHMWPE. (b)
Thermograms of the three regions (surface, subsurface or white band,
and inner or below white band) on gamma-irradiated (25 kGy) plus 7
years of shelf-aging prostheses.
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DSC experiments and the crystallinity percentages, as
well as the estimated Lc values for these three material
groups are also presented in Table 1.
3.2. Transmission electron microscopy
The structure of extruded, non-irradiated GUR 1050
UHMWPE was a semicrystalline polymer. The crystal-
line region included lamellae that appeared as narrow
white ribbons that were more or less curved, with sharp
boundaries (Fig. 2a). Zones among the lamellae denoted
the amorphous region. The boundary between lamellae
and amorphous region was so thin that it was hard to
perceive. Lamellar thickness was between 25e30 nm. All
these key variables are shown in Table 2.
The lamellae in the TEM images of gamma-irradi-
ated, one week shelf-aged UHMWPE (Fig. 2b) were less
contrasted than non-irradiated polymer (Fig. 2a).Lamellar thickness averaged 35 nm, which is clearly
thicker than virgin UHMWPE. A slight decrease in the
lamellar concentration could be deduced from the
20,000! images. The sharpness of the lamellar bound-
aries also decreased. There were no significant changes
in the other variables.
There were marked differences between the irradi-
ated, 7-year shelf-aged samples and the non-irradiated
material. As shown in Fig. 3, the lamellae were thicker in
the irradiated, 7-year shelf-aged group than in the virgin
specimens, and the boundaries were broader and clearly
visible. On the other hand, there were some differences
in the depth of the shelf-aged samples. In the surface
specimens, lamellae were kinked and their distribution
was chaotic. In the white band specimens, lamellae
appeared straightened and formed stacks in many areas.
In the latter, interlamellar distances ranged between
25e30 nm (measured between adjacent lamellae).
Lamellar concentration or density in the white band
(Fig. 3b) was much higher than at the surface. Finally,
some features of the inner samples (Fig. 3c) were similar
to the subsurface, but with no significant stacking. Table
2 includes the results of the quantitative and qualitative
microstructural parameters for all the materials.
4. Discussion
Many studies have analysed the changes in UHMWPE
after irradiation and natural aging [10e22,24e26].
Table 1
Enthalpic contents, % crystallinity, melting temperature data and lamellar thickness estimations based on the ThomsoneGibbs equation of non-
irradiated (virgin), gamma-irradiated and one week aged, and gamma-irradiated and 7 years aged extruded UHMWPE
UHMWPE Enthalpic
contents
(J/g)
% Crystallinity
(ref. 290 J/g)
Melting
temperature
( C)
Lamellar
thickness
(nm)a
Virgin 140G 12 49G 4 135.5G 1.1 27G 3
GammaC 1 week 154G 4 53G 1 137.3G 0.4 32G 2GammaC 7 years
Surface 169G 5 57G 2 137.1G 0.1 32G 1
Subsurface 206G 8 71G 3 139.8G 1.1 48G 9
Inner region 190G 1 65G 1 140.1G 1.0 50G 9
a The values for s and rc are mentioned in the text.
Fig. 2. TEM images (60,000!) of virgin ram-extruded UHMWPE (a),
and gamma-irradiated (25 kGy) UHMWPE after one week aging (b).
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However, although variation in-depth profiles in terms of
physico-chemical properties (density, oxidation index,
crystallinity, etc.) are well documented, little is known
about microstructural depth changes and its relationship
with physico-chemical changes. On the other hand, DSC
thermograms and TEM images suggest an in-depth
material distribution in the 7-year shelf-aged UHMWPE
but not in the freshly irradiated UHMWPE or virgin
material. In view of these findings, a global model of
structural evolution after gamma irradiation in air can be
proposed to discuss our results in relation with the
literature. This model would rely on three consecutive
stages.
4.1. First stage (virgin UHMWPE)
This stage relates to virgin UHMWPE. Its micro-
structure can be considered a semicrystalline polymer
with crystalline and amorphous phases. The crystalline
phase consists of folded long molecules added to thin
orthorhombic crystals, named lamellae. Those lamellae
are randomly oriented and separated by highly en-
tangled polymer molecules, which form the amorphous
phase. Some tie molecules connect different lamellae
through the amorphous phase and improve the me-
chanical properties of UHMWPE quite remarkably
[4,25,28]. These well-known features are represented in
Fig. 4a.
In the TEM images, typical white ribbons are easily
identified as randomly oriented lamellae, immersed
within a dark region corresponding to the amorphous
phase. Lamellar boundaries appeared to be sharp,
probably because there was only primary crystallization
during the processing of the extruded bars, and fold
surfaces of the lamellae lie almost parallel to the electron
beam of the TEM [29]. Several studies support our
results [4,23,25,29e32]. Regarding the physico-chemical
properties at this stage, crystallinity values are
reportedly around 50% [27], depending on the process-
ing route, resin, molecular weight, etc. There is no
detectable oxidation and the density is about 0.93 g/cm3
[1,14]. According to the DSC thermograms, crystallinity
was 49G 4% and melting temperature was
135.5G 1.1 C, as found in previous studies [1,2].
Kurtz and Schmitt point out that the crystallinephase of UHMWPE consists of folded long molecules,
added to thin orthorhombic crystals (10e50 nm thick,
and 10e50 mm long). Lin and Argon [33] also report
similar features for polyethylene single crystals obtained
from a solution, with an orthorhombic structure
(5e25 nm thick, and 1e50 mm long). Our estimated
Lc, using the melting temperature data and the
ThomsoneGibbs equation was 27G 3 nm, in agree-
ment with measured Lc values on TEM images of virgin
UHMWPE (compare Tables 1 and 2).
4.2. Second stage (low degradation)
At low doses, gamma or electron beam irradiation
causes the radiolytic scission of molecular chains by
cleavage of CeC and CeH bonds, producing different
free radicals. Since irradiation affects both crystalline
and amorphous regions, the mobility of the free radicals
is different. Depending on their location and mobility,
they can undergo recombination (leading to cross-
linking, branching, and the formation of double bonds),
stabilize, or react with incoming oxygen [5]. Irradiating
in the absence of oxygen will increase cross-linking and
decrease crystallinity [10,18,26]. It also decreases above
100 Mrad since the crystals are seriously damaged [24].However, at low and medium doses in air, crystallinity
increases after gamma [10,25,26] or electron beam
[16,22,24] irradiation. In those cases, the degradation
process (via oxygen) is more probable, favouring
oxidative chain scission as oxygen molecules react with
free radicals. Recrystallization processes are favoured by
oxidative reactions, and crystallinity will increase.
In the proposed microstructure for this stage, the
crystallinity and lamellar thickness are higher than in the
virgin samples. In addition, lamellar boundaries are less
sharp, darker and wider in TEM images (see Fig. 4b).
Our DSC and TEM results on gamma-irradiated
UHMWPE confirm the increase in crystallinity. One
week after irradiation, the estimation for UHMWPE
crystallinity, melting temperature and lamellar thick-
ness increased by 8%, 2 C, and 5 nm, respectively
(Table 1). According to the TEM images, the lamellae
were thicker (32e38 nm), than virgin UHMWPE.
Although our thermodynamic results agree with
other reports, there was an apparent contradiction in
the lamellar size. Bhateja et al. [16] and Premnath et al.
[22] found that in the first hours after beta irradiation,
UHMWPE crystallinity and melting temperature in-
creased but there was no change in lamellar thickness, as
Table 2
The results of a semiquantitative analysis of lamellar variables
Key features Virgin
UHMWPE
Gamma
C 1
week
GammaC 7 years
Surface Subsurface
(white band)
Inner
region
Thickness (nm) 25e30 32e38 32e38 30e35 32e38
Border/frontier No Yes Yes Yes YesTwisting Spacing (nm) 30e35 35e40 45e50 25e30 35e40
Chaotic
appearance
Orientation Density of
lamellae
Stacking No No No Yes No
In the qualitative variables the scale ranges from one dot () minimum,to three dots () maximum.
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detected by SAXS measurements. In our samples,
lamellar thickness increased one week after gamma
irradiation in air.
These findings can be explained by the Thomsone
Gibbs equation (Eq. (1)) and the relation provided by
Bershtein and Egorov [34] for the surface enthalpy of the
lamellae qi, (Eq. (2)), which relates this thermodynamicproperty to lamellar thickness and total melting
enthalpy, DHm:
qiZDH0m DHm
Lc=2:5 2
where DH0m is again the melting enthalpy of a perfect
crystalline polyethylene. The surface enthalpy, s, and qiare related by the expression sZ qi Tmsi, where Tm isthe melting point of the polymer and si the entropy of
the polymer [34].
In the first hours after irradiation, the increase of
DHm in the virgin sample does not correspond to an
increase in the degree of crystallinity, since the lamellarsize remains constant. According to Eq. (2), the increase
is associated with a decrease in surface enthalpy, qi. On
the other hand, the positive shift of the melting
temperature can only be related to a decrease in the
free energy surface, s. Both changes are attributed to the
radiolytic scission of tie molecules, which subsequently
rearrange into the crystals improving the surface of the
original lamellae. However, the increase in melting
temperature, enthalpy, and lamellar size could be related
to the beginning of a secondary crystallization at the
surface. An indication of this process is the change in
the lamellar boundary. As seen in the TEM images, theboundaries are less sharp. After the secondary crystalli-
zation, the surface folds of the lamellae are less parallel to
the TEM electron beam than in the virgin samples [13].
The low degradation level associated with this stage
can be explained within the general framework of
UHMWPE degradation, which is controlled by the
diffusion of oxygen and free radicals after irradiation.
The oxidation process requires that oxygen and radicals
generated during irradiation coincide in space and time.
The theoretical simulation of oxygen diffusion into
UHMWPE, along with the time evolution of the spatial
radical concentration [35] implies that the surface
degradation of up to 0.5e1 mm deep remains basically
constant (not time dependent). However, the subsurface
is strongly degraded with physical and chemical changes
after more than 5 years post-irradiation [13,19,23,35].
This is why the thermodynamic parameters and the
microscopic features in the 7-year old samples were
similar to the ones after one week of natural aging.
Fig. 3. TEM image (60,000!) of gamma-irradiated (25 kGy) plus 7
years of shelf-aging prostheses. Surface zone (a), subsurface or strong
degradation zone corresponding to the white band (b), and inner or
medium degradation zone below the white band (c).
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Both situations can be considered as two imagescorresponding to a stage of low degradation. There was
an apparent increase in lamellar tortuosity at the surface
after long shelf-aging (see Fig. 4c), which is mainly due to
oxygen accumulation at the lamellar boundaries [32].
4.3. Third stage (strong degradation)
The microstructure in the third stage is linked to the
oxidative degradation process that generates the white
band defect. This introduces important changes in
material properties such as density, molecular weight,
crystallinity degree or toughness. As widely accepted,
the changes only occur after irradiation in air followed
by an incubation period of more than 4e5 years.
Our microscopic model for this stage includes
lamellar thickening. The concentration is high with
predominant stacking of lamellae that almost lie straight
and parallel (see Fig. 4d). There are also small
crystallites within the amorphous region. The model is
based on the results from DSC and TEM from highly
degraded material (see Fig. 1b and Fig. 3b) and data
from the literature.
The DSC results in the white band region imply
an increase in crystallinity and melting temperature after
7 years of shelf-aging. The shoulder in the DSCthermograms (Fig. 1b) may reflect the presence of new
crystallites produced by chain scission processes that
generate shorter molecular chains. As a result, new
crystallization can occur in the amorphous region with
crystals that are shorter than the original lamellae.
Generalized chain scission also produces an overall
decrease in tie molecules, allowing for lamellar rap-
prochement and reordering [31], which increases me-
chanical brittleness [21,36] and melting temperature, as
shown by DSC (see Fig. 1b).
This small crystallite production is supported by
previous findings of a decrease in the interlamellar space
at SAXS and associated with the shoulder of the DSC
thermograms [22]. Partial recrystallization in the amor-
phous region has also been proposed [17]. Other studies
of crystallinity and melting temperatures confirm an
increase in fusion heat after some months of aging,
mostly with high radiation dosage [22]. The conven-
tional dosage of 25 kGy produces a mild increase in
fusion heat in the early months, which proceeds at
a lower rate with aging time [10e11]. Later on, fusion
heat continues to increase, almost inadvertently in the
first year [10,31,32], but quite noticeably after 5 years
[9e11,21].
Fig. 4. Schematic drawings of UHMWPE microstructure evolution after irradiation and shelf-aging: (a) first stage in virgin UHMWPE, (b) freshly
irradiated UHMWPE, (c) second stage in the surface region after 7 years shelf-aging UHMWPE, and (d) third stage in the white band area.
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Finally, the findings in the subsurface region (related
to high degradation), were basically similar to the deeper
region, with some differences. Whereas the melting
transition occurred at the same temperature (140 C),
neither the enthalpy content nor the TEM images were
similar. According to the micrographs, the lamellae were
more tortuous, less oriented, and not clustered. On theother hand, the incipient shoulder in the DSC thermo-
grams and the lower value of crystallinity could indicate
the lack of new crystallization, which would have
produced the small crystals in the subsurface region.
However, both thermal aspects suggest that the inner
region is in a medium degradation stage. This behavior
is supported by Blanchet and Burroughs [35], who found
that the combination of oxygen diffusion and radicals
concentration explains the presence of carbonyl groups
in the inner region (close to the subsurface). Their
density is higher than at the surface but lower than at
the white band, which corresponds to the highest
degradation region.
5. Conclusions
Both irradiation and post-irradiative degradation of
UHMWPE cause thermal and microstructural changes.
There was an increase in crystallinity in UHMWPE just
after gamma irradiation in air. As expected, lamellar
crystals appeared to thicken soon after gamma irradi-
ation. Lamellar thickness seemed to remain almost
constant after irradiation and during shelf-aging, as
shown by TEM. As degradation proceeded, crystallinityincreased at the subsurface region, whereas the surface
regions had relatively low crystallinity contents due to
the oxygen diffusion front and the specific spatial radical
concentration at the surface. Subsurface areas had high
crystallinity contents and lamellar stacking. In addition,
shoulders in thermograms of subsurface regions denote
the crystallization of new small crystals in highly
degraded zones. The lower enthalpy content and the
absence of stacking at the inner region indicate that this
region is immersed in a low degradation stage,
compared to the subsurface.
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