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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Mater.</journal-id>
<journal-title>Frontiers in Materials</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Mater.</abbrev-journal-title>
<issn pub-type="epub">2296-8016</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">789143</article-id>
<article-id pub-id-type="doi">10.3389/fmats.2021.789143</article-id>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Materials</subject>
<subj-group>
<subject>Original Research</subject>
</subj-group>
</subj-group>
</article-categories>
<title-group>
<article-title>Comparison Between Different Composite Resins Used for Clear Aligner Attachments: An <italic>In-Vitro</italic> Study</article-title>
<alt-title alt-title-type="left-running-head">Gazzani et&#x20;al.</alt-title>
<alt-title alt-title-type="right-running-head">Evaluation of Mechanical Properties</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Gazzani</surname>
<given-names>Francesca</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1452196/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Bellisario</surname>
<given-names>Denise</given-names>
</name>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1628591/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Quadrini</surname>
<given-names>Fabrizio</given-names>
</name>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Parrinello</surname>
<given-names>Francesca</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Pavoni</surname>
<given-names>Chiara</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1628465/overview"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Cozza</surname>
<given-names>Paola</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<xref ref-type="aff" rid="aff4">
<sup>4</sup>
</xref>
</contrib>
<contrib contrib-type="author">
<name>
<surname>Lione</surname>
<given-names>Roberta</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff3">
<sup>3</sup>
</xref>
<xref ref-type="aff" rid="aff4">
<sup>4</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/1550604/overview"/>
</contrib>
</contrib-group>
<aff id="aff1">
<sup>1</sup>
<institution>Department of Systems Medicine</institution>, <institution>University of Rome &#x201c;Tor Vergata&#x201d;</institution>, <addr-line>Rome</addr-line>, <country>Italy</country>
</aff>
<aff id="aff2">
<sup>2</sup>
<institution>Department of Industrial Engineering</institution>, <institution>University of Rome &#x201c;Tor Vergata&#x201d;</institution>, <addr-line>Rome</addr-line>, <country>Italy</country>
</aff>
<aff id="aff3">
<sup>3</sup>
<institution>Department of Dentistry</institution>, <institution>UNSBC</institution>, <addr-line>Tirana</addr-line>, <country>Albania</country>
</aff>
<aff id="aff4">
<sup>4</sup>
<institution>Departmental Faculty of Medicine and Surgery, University of Rome &#x201c;Unicamillus&#x201d;</institution>, <addr-line>Rome</addr-line>, <country>Italy</country>
</aff>
<author-notes>
<fn fn-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1297912/overview">Michele Tepedino</ext-link>, University of L&#x2019;Aquila, Italy</p>
</fn>
<fn fn-type="edited-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1507994/overview">Edoardo Staderini</ext-link>, Agostino Gemelli University Polyclinic (IRCCS), Italy</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/1522397/overview">Bernardo Souki</ext-link>, Pontifical Catholic University of Minas Gerais, Brazil</p>
</fn>
<corresp id="c001">&#x2a;Correspondence: Francesca Gazzani, <email>francescagazzani@hotmail.it</email>
</corresp>
<fn fn-type="other">
<p>This article was submitted to Biomaterials, a section of the journal Frontiers in Materials</p>
</fn>
</author-notes>
<pub-date pub-type="epub">
<day>04</day>
<month>02</month>
<year>2022</year>
</pub-date>
<pub-date pub-type="collection">
<year>2021</year>
</pub-date>
<volume>8</volume>
<elocation-id>789143</elocation-id>
<history>
<date date-type="received">
<day>04</day>
<month>10</month>
<year>2021</year>
</date>
<date date-type="accepted">
<day>09</day>
<month>12</month>
<year>2021</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2022 Gazzani, Bellisario, Quadrini, Parrinello, Pavoni, Cozza and Lione.</copyright-statement>
<copyright-year>2022</copyright-year>
<copyright-holder>Gazzani, Bellisario, Quadrini, Parrinello, Pavoni, Cozza and Lione</copyright-holder>
<license xlink:href="http://creativecommons.org/licenses/by/4.0/">
<p>This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) and the copyright owner(s) are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these&#x20;terms.</p>
</license>
</permissions>
<abstract>
<p>Attachments are specific features of clear aligner treatment designed to ensure the aligner&#x2019;s retention and the predictability of tooth movements. The properties of composite resin used for their reproduction play a relevant role to preserve their integrity and shape over the time. Thus, the aim of the present evaluation was to compare the mechanical properties and the wear performance of two nanocomposite by means of mechanical and tribological tests. Twelve samples for both flowable nanocomposite (FNC) and conventional nanocomposite (CNC) were created. The two nanocomposites differ in terms of filler volume and viscosity of the mixture. The following tests were performed: thermal analysis and burning test; flat instrumented indentation test and a compression stress relaxation test; tribological analysis. Wear evaluation was performed by means of a contact probe surface profiler and a TayMap software for the 3D analysis. A customized step-sliding test was conducted to simulate the clinical application of materials with a polymethyl methacrylate (PMMA) ball used as counterpart. Wear evaluation of both resin surfaces and PMMA ball was performed. No differences were found in terms of polymeric nature and quantity of nanoparticles in the matrix. FNC showed lower density values (1.62&#xa0;g/cm<sup>3</sup>&#x20;&#xb1; 0.02) and inorganic percentage residue (41%) than the CNC (respectively 1.95&#xa0;g/cm<sup>3</sup>&#x20;&#xb1; 0.01 and 23%). Significant differences in terms of decrement of stress values, elastic modulus (1,114.12&#x20;&#xb1; 91.39&#xa0;MPa), and stress relaxation rate (24.39%&#x20;&#xb1; 3.23) were observed for the CNC when compared to the FNC (respectively, 835.04&#x20;&#xb1; 184.73&#xa0;MPa and 40.19%&#x20;&#xb1; 4.65). FNC showed higher values of dynamic friction coefficient (0.72&#x20;&#xb1; 0.017) and more worn and deeper profiles than the conventional ones. The step-sliding test with a PMMA ball confirmed a higher friction coefficient for FNC and a greater wear of the PMMA surfaces when used against flowable samples. Lower viscosity of FNC ensures a better adaptation during clinical attachment fabrication, whereas it has a negative impact on mechanical properties. CNC showed greater performance and resistance under mechanical stresses than the flowable ones, resulting in being more suitable for clinical&#x20;needs.</p>
</abstract>
<kwd-group>
<kwd>nanocomposite resins</kwd>
<kwd>attachments</kwd>
<kwd>clear aligner treatment</kwd>
<kwd>tribological analysis</kwd>
<kwd>mechanical properties</kwd>
</kwd-group>
</article-meta>
</front>
<body>
<sec id="s1">
<title>Introduction</title>
<p>Clear aligners treatment (CAT) requires the placement of resin buttons on tooth surfaces to enhance the aligners retention and to create pushing surfaces for a more predictable tooth movement (<xref ref-type="bibr" rid="B15">Morton et&#x20;al., 2017</xref>; <xref ref-type="bibr" rid="B7">D&#x2019;Anto et&#x20;al., 2019</xref>). In fact, the addition of these auxiliaries, usually referred to as attachments, maximize the contact points and the interaction between the aligner and tooth surfaces. Attachments&#x2019; position and configuration play a crucial role during the orthodontic treatment since they are strongly related to the force system induced by the aligner. Ideal composite resins suitable for attachment creation need specific esthetic and mechanical properties (<xref ref-type="bibr" rid="B2">Barreda et&#x20;al., 2017</xref>). As for the esthetic aspect, composite resin should be resistant to stain and with similar translucency of the underlying tooth (<xref ref-type="bibr" rid="B9">Feinberg et&#x20;al., 2016</xref>; <xref ref-type="bibr" rid="B2">Barreda et&#x20;al., 2017</xref>). On the other hand, more clinically significant are the mechanical features required. Since they represent needful auxiliary elements for aligners system, their integrity and shapes need to be maintained during the treatment to ensure the functional validity and to not compromise movements&#x2019; efficiency and aligner fitting (<xref ref-type="bibr" rid="B12">Kravitz et&#x20;al., 2008</xref>; <xref ref-type="bibr" rid="B8">Das et&#x20;al., 2015</xref>; <xref ref-type="bibr" rid="B7">D&#x2019;Anto et&#x20;al., 2019</xref>; <xref ref-type="bibr" rid="B14">Mantovani et&#x20;al., 2019</xref>). These materials (resin-based dental composite) are widely used in dentistry for dental restorations and orthodontic devices (<xref ref-type="bibr" rid="B1">Aminoroaya et&#x20;al., 2021</xref>). They are usually composed of two phases: an organic resin matrix and an inorganic/organic filler. The organic resin matrix is composed of monomers and light-sensitive initiators, whereas the filler phase consists of different size particles (micro/nano-sized fillers) which determine the material&#x2019;s properties (<xref ref-type="bibr" rid="B11">Fronza et al., 2015</xref>; <xref ref-type="bibr" rid="B21">Taheri et&#x20;al., 2015</xref>; <xref ref-type="bibr" rid="B5">Cho et&#x20;al., 2020</xref>; <xref ref-type="bibr" rid="B1">Aminoroaya et&#x20;al., 2021</xref>). The predominant bases monomer used are normally bis-GMA that is sometimes mixed with other dimethacrylates (<xref ref-type="bibr" rid="B10">Ferracane. 2011</xref>). Most of the composites contain an activator/initiator system to promote light-activated polymerization of the organic matrix forming cross-linked polymer networks (<xref ref-type="bibr" rid="B16">Nikolaidis. et&#x20;al., 2019</xref>). The most variable contents are represented by the filler particles and their size (<xref ref-type="bibr" rid="B19">Satterthwaite et&#x20;al., 2009</xref>; <xref ref-type="bibr" rid="B18">Satterthwaite et&#x20;al., 2012</xref>). The &#x201c;nanofill&#x201d; composites include nanoscale particles characterized by a size range of 1&#x2013;100 (<xref ref-type="bibr" rid="B10">Ferracane. 2011</xref>). Particles&#x2019; size may range from 20 nm to 5&#x20;&#x3bc;m and filler phase overall can represent 70% of the volume (<xref ref-type="bibr" rid="B13">Lang et&#x20;al., 1992</xref>; <xref ref-type="bibr" rid="B2">Barreda et&#x20;al., 2017</xref>). Attachments&#x2019; creation usually requires conventional (CNC) or flowable (FNC) dental nanocomposite resins (<xref ref-type="bibr" rid="B10">Ferracane 2011</xref>; <xref ref-type="bibr" rid="B14">Mantovani et&#x20;al., 2019</xref>) which mainly differ for filler volume and viscosity. Composite viscosity is determined by monomer composition and filler content. CNC is composed of small particle sizes with a high filler volume and high viscosity of the mixture. On the other hand, FNC present the same small particle sizes of conventional composites with a reduced filler volume, increased resin content, and lower viscosity of the mixture (<xref ref-type="bibr" rid="B3">Bayne et&#x20;al., 1998</xref>; <xref ref-type="bibr" rid="B4">Benetti et&#x20;al., 2015</xref>). This composition produces a composite with an easy adaptation to the attachments template, but a negative impact to wear performance and stability (<xref ref-type="bibr" rid="B6">Clelland et&#x20;al., 2005</xref>). In literature, many studies (<xref ref-type="bibr" rid="B9">Feinberg et&#x20;al., 2016</xref>; <xref ref-type="bibr" rid="B2">Barreda et&#x20;al., 2017</xref>; <xref ref-type="bibr" rid="B7">D&#x2019;Anto et&#x20;al., 2019</xref>; <xref ref-type="bibr" rid="B14">Mantovani et&#x20;al., 2019</xref>) investigated composite resins for this clinical application. <xref ref-type="bibr" rid="B7">D&#x2019;Anto et&#x20;al. (2019)</xref> demonstrated that composite viscosity does not have any influences on the shape and volume of attachments. However, no data are available on the comparison of mechanical and wear properties of different composite resins available especially when used for attachment. Since the choice of the best material with ideal properties seems to be relevant to ensure the stability and the efficiency of these auxiliary components of CAT, the aim of this study was to analyze the mechanical properties of two nanocomposite resins (CNC vs FNC) with different viscosities and filler volume by means of mechanical and tribological&#x20;tests.</p>
</sec>
<sec sec-type="materials|methods" id="s2">
<title>Materials and Methods</title>
<p>A series of 12 samples (6 FNC, 6 CNC) were realized for the experimental analysis. Photocurable thickness limits of about 1&#xa0;mm for each type of composite were respected and photo-masks with three thickness steps have been manufactured to optimize the deposition and the curing phase. All the masks were machined into a polycarbonate sheet in which five circular seats of 6&#xa0;mm of diameter have been obtained (<xref ref-type="fig" rid="F1">Figure&#x20;1</xref>). The diameter of 6&#xa0;mm has been chosen in order to carry out macroscopic mechanical tests as indentation tests and tribological tests for which a contact surface in the order of 5&#x2013;10&#xa0;mm is required as a minimum. An incremental addition of 1&#xa0;mm of material has been deposited into the mask&#x2019;s seats and then exposed to UV light until reaching 3&#xa0;mm of total thickness. For each sample, the UV lamp (TPC led curing light 50&#xa0;N, United&#x20;States) with an irradiance of 800&#xa0;mW/cm<sup>2</sup> was positioned at 5&#xa0;mm of distance and the UV curing time step was set at 25&#xa0;s. At the end of the curing process, the sample sizes and the weight were measured by means of a digital caliper and a precision balance, and these measures were evaluated as the average dimensions and calculated the density values. The primary endpoints of the present investigation were to evaluate the mechanical properties and the wear behaviour of the two nanocomposites. The secondary endpoints were to analyse their thermal properties and to observe the wear behaviour after the simulation of clinical conditions of use through a step-sliding test in combination with a&#x20;PMMA.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Samples&#x2019; preparation process: physical mask preparation for sample deposition, lamp exposition, and final samples.</p>
</caption>
<graphic xlink:href="fmats-08-789143-g001.tif"/>
</fig>
<sec id="s2-1">
<title>Thermal Analysis and Burning Test</title>
<p>Given the polymeric nature of the nanocomposite materials, thermal analysis was conducted by differential scanning calorimetry (DSC 7 by Perkin Elmer) in order to evaluate their thermal properties. After samples curing, a small amount (20&#xa0;mg) of each nanocomposite material was analysed by DSC scanning (range 20&#x2013;250&#xb0;C, rate 10&#xa0;C/min). Considering the amount of inorganic content for both materials analysed, a burning test was realized. Small quantities (150&#xa0;mg) of nanocomposites were inserted at 600&#xb0;C for 60&#xa0;min into a muffle and after that time the unburned residue was evaluated to calculate the percentage of inorganic content.</p>
</sec>
<sec id="s2-2">
<title>Mechanical Tests</title>
<p>Evaluation of the mechanical properties were performed through a flat instrumented indentation test (<xref ref-type="fig" rid="F2">Figure&#x20;2A</xref>) and a compression stress relaxation test. The first analysis was used to assess local mechanical behaviour of nanocomposite samples, while the second test was performed to evaluate the global mechanical properties and the stress relaxation behaviour. The flat indentation tests were carried out on the flat surface of the cylindrical samples, by using a universal material testing machine (Insight/5 by MTS) equipped with an indenter holder. Flat indenter of tungsten carbide was used with a diameter of 1&#xa0;mm. The tests were performed on 5 samples for each type of material and the indentation was centered with respect to the sample&#x2019;s diameter. The maximum penetration depth imposed was 0.3&#xa0;mm (10% of total thickness to avoid the influence of the substrate), the rate was 0.1&#xa0;mm/min, and the pre-load was 1&#xa0;N. The compression stress relaxation tests were performed by means of a universal testing machine (Alliance/50 by MTS) in compression configuration. Five samples have been compressed up to a maximum of 50&#xa0;MPa by compression plates and fixing the crosshead position and evaluating the stress decrease for 15&#xa0;min.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Experimental analysis: <bold>(A)</bold> Flat indentation test. <bold>(B)</bold> Step sliding&#x20;test.</p>
</caption>
<graphic xlink:href="fmats-08-789143-g002.tif"/>
</fig>
</sec>
<sec id="s2-3">
<title>Tribological Tests and Wear Evaluation</title>
<p>Tribological tests with alternative dry-sliding motion were performed on five samples for each type of nanocomposite by a standard tribometer (Linear Reciprocating Tribometer, C.S.M. Instruments, Peseaux, Switzerland) at about 20&#xb0;C and 40% RH. Tests were performed at 10&#xa0;N load and with a back-and-forth sliding (stroke length 4&#xa0;mm, frequency 2.5&#xa0;Hz, duration 10,000 cycles) of the alumina ball (6&#xa0;mm diameter). Samples&#x2019; wear was assessed by contact probe surface profiler (TalySurf CLI 2000; Taylor Hobson, Leicester, United&#x20;Kingdom). The profilometer was used to rebuild the wear patterns using a 5&#xa0;&#x3bc;m lateral resolution. The maximum and mean depth, the area, and the volume involved by the action of the counterpart on the surface of the samples were evaluated by using a TayMap software to calculate and qualitatively analyse the 3D wear patterns.</p>
</sec>
<sec id="s2-4">
<title>Customized Test and Simulation of Clinical Application</title>
<p>A more targeted test was performed to simulate more specifically the clinical condition of use of materials involved in the investigation. The implementation of materials provides their placement on the tooth in thicknesses of 1&#xa0;mm to build a step. A step-sliding test has been developed to simulate the insertion and removal of the appliance and the periodic work of the composites in combination with the material of the aligner. A step of each nanocomposite material was created on a ceramic support and a PMMA (polymethyl methacrylate) ball was used as counterpart during step-sliding tests (<xref ref-type="fig" rid="F2">Figure&#x20;2B</xref>). To assess the type of polymer of the commercial aligner, a thermal analysis by DSC (DSC 7 by Perkin Elmer) was performed. The step-sliding test was performed with a contact length of 10&#xa0;mm (5&#xa0;mm above the step and 5&#xa0;mm below the step), a duration of 10,000 cycles, a frequency of 2.5&#xa0;Hz, and a normal load of 1&#xa0;N. The wear behaviour of the samples was evaluated by contact profilometer (TalySurf CLI 2000; Taylor Hobson, Leicester, United&#x20;Kingdom), while the PMMA ball wear was assessed through weight difference before and after the test. The wear values of the nanocomposite samples were also evaluated by 3D maps of the samples&#x2019; surface at the top of the&#x20;step.</p>
</sec>
</sec>
<sec sec-type="results" id="s3">
<title>Results</title>
<p>
<xref ref-type="table" rid="T1">Table&#x20;1</xref> reports the measured dimensions of all fabricated samples in the pilot study and through these values the mean density was evaluated for each type of nanocomposite, in particular 1.62 (g/cm<sup>3</sup>)&#x20;&#xb1; 0.02 and of 1.95 (g/cm<sup>3</sup>)&#x20;&#xb1; 0.01, respectively for FNC and CNC. Analysing the DSC curves for the two materials, no differences were found in terms of polymeric nature of the composites or substantial changes in the quantity of nanoparticles in the matrix. However, the burning test reported an inorganic percentage residue of 41 and 23%, respectively, for the FNC and for CNC (<xref ref-type="fig" rid="F3">Figure&#x20;3A</xref>). Form a mechanical point of view, flat indentation tests showed a good repeatability for both materials (<xref ref-type="fig" rid="F3">Figure&#x20;3B</xref>). The maximum loads reached at a depth of 0.3&#xa0;mm were 364.94&#xa0;N&#x20;&#xb1; 27.87 and 723.66&#xa0;N&#x20;&#xb1; 38.37, respectively, for flowable and conventional samples. Equally significant differences have been found between the two materials in stress relaxation tests. Specifically, a lower decrease of stress value of the CNC material was found in comparison to the FNC (<xref ref-type="fig" rid="F3">Figure&#x20;3C</xref>). Elastic modulus&#x2019; evaluations reported greater values observed for the CNC (1,114.12&#x20;&#xb1; 91.39&#xa0;MPa) than the FNC (835.04&#x20;&#xb1; 184.73&#xa0;MPa). Higher values of stress relaxation were found for the FNC (40.19&#x20;&#xb1; 4.65) when compared with CNC (24.93&#x20;&#xb1; 3.23). As for tribological test, some FNC samples did not complete the number of cycles as the maximum limit of tangential force detected by the instrument was reached. Higher values of dynamic friction coefficient for FNC were found (<xref ref-type="fig" rid="F3">Figure&#x20;3D</xref>). The different wear behaviour of the samples has been also confirmed by the images and 3D maps as shown in <xref ref-type="fig" rid="F4">Figure&#x20;4</xref>. The comparison of the worn areas showed deeper wear profiles on FNC surfaces than on the conventional ones (<xref ref-type="fig" rid="F4">Figures 4</xref>, <xref ref-type="fig" rid="F5">5A,B</xref>). As reported in <xref ref-type="table" rid="T2">Table&#x20;2</xref>, worn surface and volume values for the FNC samples were higher than the CNC, and also as expected the maximum and mean depth of the wear were greater for FNC. The step-sliding test with a PMMA ball showed a higher average friction coefficient for FNC in <xref ref-type="fig" rid="F5">Figure&#x20;5C</xref>. Also, the PMMA surfaces significantly wore out during the test especially when used against FNC sample. The 3D maps of worn surfaces for both nanocomposites are reported in <xref ref-type="fig" rid="F6">Figure&#x20;6</xref> Extracted values and volume of the two samples (<xref ref-type="table" rid="T3">Table&#x20;3</xref>) showed that the extension of the surface involved is comparable among the two samples, while the worn volume is greater for FNC with a corresponding modification of the PMMA ball geometry.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>Measured dimensions and weight of the different fabricated samples.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="left"/>
<th colspan="4" align="center">H</th>
<th colspan="3" align="center">D</th>
<th align="center">Weight</th>
<th align="center">H<sub>mean</sub>
</th>
<th align="center">D<sub>mean</sub>
</th>
<th align="center">Density</th>
</tr>
<tr>
<th colspan="4" align="center">mm</th>
<th colspan="3" align="center">Mm</th>
<th align="center">g</th>
<th align="center">mm</th>
<th align="center">mm</th>
<th align="center">g/cm<sup>3</sup>
</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">CNC1</td>
<td align="char" char=".">2.714</td>
<td align="char" char=".">2.818</td>
<td align="char" char=".">2.824</td>
<td align="char" char=".">2.781</td>
<td align="char" char=".">5.96</td>
<td align="char" char=".">5.97</td>
<td align="char" char=".">5.95</td>
<td align="char" char=".">0.1508</td>
<td align="char" char=".">2.784</td>
<td align="char" char=".">5.96</td>
<td align="char" char=".">1.94</td>
</tr>
<tr>
<td align="left">CNC2</td>
<td align="char" char=".">2.661</td>
<td align="char" char=".">2.651</td>
<td align="char" char=".">2.665</td>
<td align="char" char=".">2.656</td>
<td align="char" char=".">5.94</td>
<td align="char" char=".">5.95</td>
<td align="char" char=".">5.94</td>
<td align="char" char=".">0.143</td>
<td align="char" char=".">2.658</td>
<td align="char" char=".">5.94</td>
<td align="char" char=".">1.94</td>
</tr>
<tr>
<td align="left">CNC3</td>
<td align="char" char=".">2.631</td>
<td align="char" char=".">2.619</td>
<td align="char" char=".">2.629</td>
<td align="char" char=".">2.586</td>
<td align="char" char=".">5.96</td>
<td align="char" char=".">5.97</td>
<td align="char" char=".">5.95</td>
<td align="char" char=".">0.1436</td>
<td align="char" char=".">2.616</td>
<td align="char" char=".">5.96</td>
<td align="char" char=".">1.97</td>
</tr>
<tr>
<td align="left">CNC4</td>
<td align="char" char=".">2.656</td>
<td align="char" char=".">2.651</td>
<td align="char" char=".">2.654</td>
<td align="char" char=".">2.659</td>
<td align="char" char=".">5.96</td>
<td align="char" char=".">5.94</td>
<td align="char" char=".">5.97</td>
<td align="char" char=".">0.1453</td>
<td align="char" char=".">2.655</td>
<td align="char" char=".">5.957</td>
<td align="char" char=".">1.96</td>
</tr>
<tr>
<td align="left">CNC5</td>
<td align="char" char=".">2.461</td>
<td align="char" char=".">2.465</td>
<td align="char" char=".">2.464</td>
<td align="char" char=".">2.463</td>
<td align="char" char=".">5.96</td>
<td align="char" char=".">6.03</td>
<td align="char" char=".">5.97</td>
<td align="char" char=".">0.1349</td>
<td align="char" char=".">2.463</td>
<td align="char" char=".">5.987</td>
<td align="char" char=".">1.94</td>
</tr>
<tr>
<td align="left">CNC6</td>
<td align="char" char=".">2.871</td>
<td align="char" char=".">2.87</td>
<td align="char" char=".">2.868</td>
<td align="char" char=".">2.869</td>
<td align="char" char=".">5.97</td>
<td align="char" char=".">5.98</td>
<td align="char" char=".">6.05</td>
<td align="char" char=".">0.1585</td>
<td align="char" char=".">2.869</td>
<td align="char" char=".">6</td>
<td align="char" char=".">1.95</td>
</tr>
<tr>
<td align="left">FNC1</td>
<td align="char" char=".">2.516</td>
<td align="char" char=".">2.542</td>
<td align="char" char=".">2.558</td>
<td align="char" char=".">3</td>
<td align="char" char=".">6.12</td>
<td align="char" char=".">6.23</td>
<td align="char" char=".">6.15</td>
<td align="char" char=".">0.1258</td>
<td align="char" char=".">2.537</td>
<td align="char" char=".">6.167</td>
<td align="char" char=".">1.66</td>
</tr>
<tr>
<td align="left">FNC2</td>
<td align="char" char=".">2.331</td>
<td align="char" char=".">2.328</td>
<td align="char" char=".">2.327</td>
<td align="char" char=".">2.326</td>
<td align="char" char=".">6.21</td>
<td align="char" char=".">6.16</td>
<td align="char" char=".">6.22</td>
<td align="char" char=".">0.1128</td>
<td align="char" char=".">2.328</td>
<td align="char" char=".">6.196667</td>
<td align="char" char=".">1.61</td>
</tr>
<tr>
<td align="left">FNC3</td>
<td align="char" char=".">2.625</td>
<td align="char" char=".">2.62</td>
<td align="char" char=".">2.617</td>
<td align="char" char=".">2.621</td>
<td align="char" char=".">6.16</td>
<td align="char" char=".">6.25</td>
<td align="char" char=".">6.13</td>
<td align="char" char=".">0.1287</td>
<td align="char" char=".">2.621</td>
<td align="char" char=".">6.18</td>
<td align="char" char=".">1.64</td>
</tr>
<tr>
<td align="left">FNC4</td>
<td align="char" char=".">2.803</td>
<td align="char" char=".">2.803</td>
<td align="char" char=".">2.801</td>
<td align="char" char=".">2.804</td>
<td align="char" char=".">6.3</td>
<td align="char" char=".">6.37</td>
<td align="char" char=".">6.33</td>
<td align="char" char=".">0.1443</td>
<td align="char" char=".">2.802</td>
<td align="char" char=".">6.333333</td>
<td align="char" char=".">1.63</td>
</tr>
<tr>
<td align="left">FNC5</td>
<td align="char" char=".">2.688</td>
<td align="char" char=".">2.68</td>
<td align="char" char=".">2.667</td>
<td align="char" char=".">2.673</td>
<td align="char" char=".">6.2</td>
<td align="char" char=".">6.23</td>
<td align="char" char=".">6.17</td>
<td align="char" char=".">0.13</td>
<td align="char" char=".">2.677</td>
<td align="char" char=".">6.2</td>
<td align="char" char=".">1.61</td>
</tr>
<tr>
<td align="left">FNC6</td>
<td align="char" char=".">2.398</td>
<td align="char" char=".">2.397</td>
<td align="char" char=".">2.403</td>
<td align="char" char=".">2.401</td>
<td align="char" char=".">6.16</td>
<td align="char" char=".">6.12</td>
<td align="char" char=".">6.1</td>
<td align="char" char=".">0.1135</td>
<td align="char" char=".">2.40</td>
<td align="char" char=".">6.126667</td>
<td align="char" char=".">1.60</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<fn>
<p>mm, millimeters; g: grams; H: height; D: diameter; FNC, flowable nanocomposite; CNC, conventional nanocomposite.</p>
</fn>
</table-wrap-foot>
</table-wrap>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>
<bold>(A)</bold> Differential scanning calorimetry curves. <bold>(B)</bold> Flat indentation curves and trend. <bold>(C)</bold> Stress relaxation curves. <bold>(D)</bold> Friction coefficient values monitored during 10,000 laps on the samples&#x2019; surfaces. The average friction coefficient for each material was evaluated in the range between 6,000 and 8,000 laps at &#x2b;1&#xa0;mm from the centred position of linear sliding.</p>
</caption>
<graphic xlink:href="fmats-08-789143-g003.tif"/>
</fig>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Qualitative evaluation of wear behavior. <bold>(A)</bold> Sample images after tribological tests. <bold>(B)</bold> 3D maps of FNC and CNC worn surfaces after tribological&#x20;tests.</p>
</caption>
<graphic xlink:href="fmats-08-789143-g004.tif"/>
</fig>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>
<bold>(A)</bold> Wear profiles analyses of FNC. <bold>(B)</bold> Wear profiles analyses of CNC. <bold>(C)</bold> Friction coefficient trend during step sliding test. The total number of cycles covered was 5,000, the sliding length was 10&#xa0;mm. The position at which the friction trends have been evaluated is &#x2b;2.5&#xa0;mm compared to the central sliding position (on the top of the step).</p>
</caption>
<graphic xlink:href="fmats-08-789143-g005.tif"/>
</fig>
<table-wrap id="T2" position="float">
<label>TABLE 2</label>
<caption>
<p>Evaluated worn surface and volume, and maximum and mean depth for the worn surfaces.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="left"/>
<th align="center">Worn surface</th>
<th align="center">Worn volume</th>
<th align="center">Max depth</th>
<th align="center">Mean depth</th>
</tr>
<tr>
<th align="center">mm<sup>2</sup>
</th>
<th align="center">mm<sup>3</sup>
</th>
<th align="center">&#x3bc;m</th>
<th align="center">&#x3bc;m</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">FNC</td>
<td align="char" char="plusmn">2.158&#x20;&#xb1; 0.17</td>
<td align="char" char="plusmn">0.030&#x20;&#xb1; 0.014</td>
<td align="char" char="plusmn">38.933&#x20;&#xb1; 15.792</td>
<td align="char" char="plusmn">14.867&#x20;&#xb1; 3.184</td>
</tr>
<tr>
<td align="left">CNC</td>
<td align="char" char="plusmn">0.901&#x20;&#xb1; 0.174</td>
<td align="char" char="plusmn">0.002&#x20;&#xb1; 0.001</td>
<td align="char" char="plusmn">15.951&#x20;&#xb1; 5.548</td>
<td align="char" char="plusmn">2.193&#x20;&#xb1; 0.921</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<fn>
<p>mm, millimeters;&#x20;&#x3bc;m, micrometers; FNC, flowable nanocomposite; CNC, conventional nanocomposite.</p>
</fn>
</table-wrap-foot>
</table-wrap>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>
<bold>(A)</bold> CNC and FNC samples and the respective PMMA balls used after step sliding test. <bold>(B)</bold> 3D maps of the CNC and FNC samples&#x2019; worn surface s at the top of the sample&#x20;step.</p>
</caption>
<graphic xlink:href="fmats-08-789143-g006.tif"/>
</fig>
<table-wrap id="T3" position="float">
<label>TABLE 3</label>
<caption>
<p>Worn surface and volume and maximum and mean depth of the worn surface of samples after step sliding&#x20;test.</p>
</caption>
<table>
<thead valign="top">
<tr>
<th rowspan="2" align="left"/>
<th align="center">Worn surface</th>
<th align="center">Worn volume</th>
<th align="center">Max depth</th>
<th align="center">Mean depth</th>
</tr>
<tr>
<th align="center">mm<sup>2</sup>
</th>
<th align="center">mm<sup>3</sup>
</th>
<th align="center">&#x3bc;m</th>
<th align="center">&#x3bc;m</th>
</tr>
</thead>
<tbody valign="top">
<tr>
<td align="left">FNC</td>
<td align="char" char=".">1.77</td>
<td align="char" char=".">0.0038</td>
<td align="char" char=".">56</td>
<td align="char" char=".">21.6</td>
</tr>
<tr>
<td align="left">CNC</td>
<td align="char" char=".">1.78</td>
<td align="char" char=".">0.0022</td>
<td align="char" char=".">7.98</td>
<td align="char" char=".">1.26</td>
</tr>
</tbody>
</table>
<table-wrap-foot>
<fn>
<p>mm, millimeters;&#x20;&#x3bc;m, micrometers; FNC, flowable nanocomposite; CNC, conventional nanocomposites.</p>
</fn>
</table-wrap-foot>
</table-wrap>
</sec>
<sec sec-type="discussion" id="s4">
<title>Discussion</title>
<p>Composite attachments are geometric buttons routinely required for all CAT. These powerful features are essential to control tooth movements and anchorage units, but they also increase aligners&#x2019; retention (<xref ref-type="bibr" rid="B14">Mantovani et&#x20;al., 2019</xref>). Rossini et&#x20;al. concluded that all kinds of attachments had a great impact on the quality and predictability of the tooth movements (<xref ref-type="bibr" rid="B20">Simon et&#x20;al., 2014</xref>; <xref ref-type="bibr" rid="B17">Rossini et&#x20;al., 2015</xref>). For this reason, the selection of composite resins plays a crucial role for the long-term stability of the attachments&#x2019; shape and for their structural integrity. The aim of the present investigation was to analyse two composite resins with different viscosity and filler volume in order to compare their mechanical properties and to identify which is more suitable for the attachment&#x2019;s reproduction. Our results showed how a greater degree of wear was observed when the attachment was reproduced with the composite presenting a higher percentage of inorganic particles. As a matter of fact, despite the lower content of inorganic filling content, the CNC resulted denser and it was characterized by a better mechanical resistance (<xref ref-type="fig" rid="F3">Figure&#x20;3A</xref>). According to our findings, <xref ref-type="bibr" rid="B2">Barreda et&#x20;al. (2017)</xref> compared attachment surfaces made of two composites with different particle size and filler content by means of Scanning Electron Microscopy (SEM). They concluded that the shape of attachments does not change within 6&#xa0;months. Thus, the movements related would still be effective in this time interval. Additional data suggested that the low viscosity, defined as the measure of a fluid resistance to flow, is related to a greater elastic modulus indicating that the material offers more resistance to the deformation (<xref ref-type="bibr" rid="B20">Simon et&#x20;al., 2014</xref>). On the other hand, once a strain is given to the FNC material, the viscous component gradually &#x201c;engages&#x201d; the deformation (<xref ref-type="fig" rid="F3">Figure&#x20;3C</xref>). Both FNC and CNC demonstrated a stress decrease after a strain application as expected by the material&#x2019;s nature; however, the rate of the decrease was higher for CNC. This underlines how for the CNC the loss of the applied load is faster over time, although the time investigated is relatively short (15&#xa0;min). As reported by <xref ref-type="bibr" rid="B22">Tanimoto et&#x20;al. (2006)</xref>, elastic modulus is not affected by the filler size, but it depends on stress transmission between the filler and the matrix. As widely described, resin composites differ from each other in terms of stain resistance, hardness, and wear behaviour (<xref ref-type="bibr" rid="B6">Clelland et&#x20;al., 2005</xref>; <xref ref-type="bibr" rid="B20">Simon et&#x20;al., 2014</xref>; <xref ref-type="bibr" rid="B1">Aminoroaya et&#x20;al., 2021</xref>). In the existing literature (<xref ref-type="bibr" rid="B8">Dasy et&#x20;al., 2015</xref>; <xref ref-type="bibr" rid="B9">Feinberg et&#x20;al., 2016</xref>; <xref ref-type="bibr" rid="B2">Barreda et&#x20;al., 2017</xref>; <xref ref-type="bibr" rid="B7">D&#x2019;Anto et&#x20;al., 2019</xref>), not many studies analysed the wear behaviour of the composite resins mainly used for attachments reproduction. On the other hand, <xref ref-type="bibr" rid="B2">Barreda et&#x20;al. (2017)</xref> demonstrated that the properties of composites could affect the surface, but not the shape of the attachments during use. More recently, their results have been confirmed by <xref ref-type="bibr" rid="B7">D&#x2019;Anto et&#x20;al. (2019)</xref> who concluded that viscosity values determine differences in terms of shape and volume. However, the wear behaviour of these materials has not been yet analysed related to their use for attachments reproduction. In this study, the mechanical and wear performances in laboratory tests on the nanocomposites used for the attachments were analysed. In order to carry out such macroscopic evaluations, sample sizes were chosen as small as possible to perform tests under sliding, and as large as possible to have a homogeneous curing under the lamp. Even if the exact clinical conditions are not repeated, at least the single curing step was correctly adopted and it was suitable for the purpose of evaluation and comparison of attachment materials. The tribological test conducted revealed higher values of dynamic friction for the FNC (0.72&#x20;&#xb1; 0.017) when compared with the CNC (0.41&#x20;&#xb1; 0.092) with a consequent greater susceptibility to the surface damages (<xref ref-type="fig" rid="F3">Figure&#x20;3D</xref>). The evaluation of these damages from a morphological point of view were made by 3D maps acquisition by a contact profilometer (<xref ref-type="fig" rid="F4">Figures 4</xref>, <xref ref-type="fig" rid="F5">5</xref>). In particular, it observed a superficial removal of composite material (worn areas). The qualitative evaluation highlighted deeper grooves and more significant wear traces on FNC samples. The same characteristics have been further confirmed by the step sliding test performed between the nanocomposites and the PMMA ball (<xref ref-type="table" rid="T3">Table&#x20;3</xref>). Also in this case, the results obtained revealed significant differences between the two materials, as shown in <xref ref-type="fig" rid="F5">Figures 5C</xref>, <xref ref-type="fig" rid="F6">6</xref>. A greater wear has been observed when the PMMA ball was used counterpart in the test with FNC samples indicating a larger abrasive damage among the two materials. As for the samples&#x2019; surfaces, the 3D analysis (<xref ref-type="fig" rid="F6">Figure&#x20;6</xref>) showed that the extension of the surface involved is comparable among the two samples, while the worn volume results were once again greater for the FNC&#x20;resin.</p>
</sec>
<sec id="s5">
<title>Strength and Limitations</title>
<p>A strength of the present investigation consisted of having identified the different mechanical and wear properties of the two nanocomposites highlighting the best application of the CNC for attachments reproduction. Wear properties and strength observed during the experimental analysis provide better performance and fitting of aligners, making these materials the best choice for the features design. A limitation of the present study is that although the tests conducted were highly repeatable, they move away from the real conditions of use. Further investigation should be thought to simulate and reproduce the insertion and removal of clear aligners and the periodic work of the composites in combination with their material.</p>
</sec>
<sec sec-type="conclusion" id="s6">
<title>Conclusion</title>
<p>CNC resins demonstrated a better mechanical behaviour from a materialistic point of view, and for this reason they seem to be considered the best choice for attachments creation during CAT. Moreover, wear properties in dry conditions and strength observed during the experimental analysis provide better performance and fitting of aligners, making these materials the best choice for the features design.</p>
</sec>
</body>
<back>
<sec id="s7">
<title>Data Availability Statement</title>
<p>The original contributions presented in the study are included in the article/Supplementary Material, further inquiries can be directed to the corresponding author.</p>
</sec>
<sec id="s8">
<title>Author Contributions</title>
<p>PC, RL, and FG proposed the research idea and wrote the article. DB and FQ improved the idea and performed the experimental analysis. They also contributed to the writing of the paper. CP and FP assisted the experimental analysis. All authors reviewed the article.</p>
</sec>
<sec sec-type="COI-statement" id="s9">
<title>Conflict of Interest</title>
<p>The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.</p>
<p>The reviewer BS declared a past collaboration with several of the authors CP, PC, and RL to the handling editor.</p>
</sec>
<sec sec-type="disclaimer" id="s10">
<title>Publisher&#x2019;s Note</title>
<p>All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors, and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.</p>
</sec>
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