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<front>
<journal-meta>
<journal-id journal-id-type="publisher-id">Front. Mech. Eng.</journal-id>
<journal-title-group>
<journal-title>Frontiers in Mechanical Engineering</journal-title>
<abbrev-journal-title abbrev-type="pubmed">Front. Mech. Eng.</abbrev-journal-title>
</journal-title-group>
<issn pub-type="epub">2297-3079</issn>
<publisher>
<publisher-name>Frontiers Media S.A.</publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id pub-id-type="publisher-id">1728890</article-id>
<article-id pub-id-type="doi">10.3389/fmech.2025.1728890</article-id>
<article-version article-version-type="Version of Record" vocab="NISO-RP-8-2008"/>
<article-categories>
<subj-group subj-group-type="heading">
<subject>Original Research</subject>
</subj-group>
</article-categories>
<title-group>
<article-title>Dynamic characteristics of negative stiffness structure with high static and low dynamic stiffness</article-title>
<alt-title alt-title-type="left-running-head">Wang et al.</alt-title>
<alt-title alt-title-type="right-running-head">
<ext-link ext-link-type="uri" xlink:href="https://doi.org/10.3389/fmech.2025.1728890">10.3389/fmech.2025.1728890</ext-link>
</alt-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname>Wang</surname>
<given-names>Yuanshao</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="aff" rid="aff2">
<sup>2</sup>
</xref>
<uri xlink:href="https://loop.frontiersin.org/people/3248706"/>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Data curation" vocab-term-identifier="https://credit.niso.org/contributor-roles/data-curation/">Data curation</role>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Writing &#x2013; original draft" vocab-term-identifier="https://credit.niso.org/contributor-roles/writing-original-draft/">Writing - original draft</role>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Zhang</surname>
<given-names>Bao</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="corresp" rid="c001">&#x2a;</xref>
<uri xlink:href="https://loop.frontiersin.org/people/3249907"/>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Methodology" vocab-term-identifier="https://credit.niso.org/contributor-roles/methodology/">Methodology</role>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Writing &#x2013; review &#x26; editing" vocab-term-identifier="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/">Writing - review and editing</role>
</contrib>
<contrib contrib-type="author" corresp="yes">
<name>
<surname>Su</surname>
<given-names>Xiaoping</given-names>
</name>
<xref ref-type="aff" rid="aff1">
<sup>1</sup>
</xref>
<xref ref-type="corresp" rid="c001">&#x2a;</xref>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Conceptualization" vocab-term-identifier="https://credit.niso.org/contributor-roles/conceptualization/">Conceptualization</role>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Validation" vocab-term-identifier="https://credit.niso.org/contributor-roles/validation/">Validation</role>
<role vocab="credit" vocab-identifier="https://credit.niso.org/" vocab-term="Writing &#x2013; review &#x26; editing" vocab-term-identifier="https://credit.niso.org/contributor-roles/Writing - review &#x26; editing/">Writing - review and editing</role>
</contrib>
</contrib-group>
<aff id="aff1">
<label>1</label>
<institution>School of Mechanical and Power Engineering, Nanjing Tech University</institution>, <city>Nanjing</city>, <country country="CN">China</country>
</aff>
<aff id="aff2">
<label>2</label>
<institution>Nanjing Tech University Pujiang Institute</institution>, <city>Nanjing</city>, <country country="CN">China</country>
</aff>
<aff id="aff3">
<label>3</label>
<institution>Naveco Automobile Co., Ltd.</institution>, <city>Nanjing</city>, <country country="CN">China</country>
</aff>
<author-notes>
<corresp id="c001">
<label>&#x2a;</label>Correspondence: Bao Zhang, <email xlink:href="mailto:zhangbao1350@126.com">zhangbao1350@126.com</email>; Xiaoping Su, <email xlink:href="mailto:suxiaoping@njtech.edu.cn">suxiaoping@njtech.edu.cn</email>
</corresp>
</author-notes>
<pub-date publication-format="electronic" date-type="pub" iso-8601-date="2025-11-20">
<day>20</day>
<month>11</month>
<year>2025</year>
</pub-date>
<pub-date publication-format="electronic" date-type="collection">
<year>2025</year>
</pub-date>
<volume>11</volume>
<elocation-id>1728890</elocation-id>
<history>
<date date-type="received">
<day>20</day>
<month>10</month>
<year>2025</year>
</date>
<date date-type="rev-recd">
<day>03</day>
<month>11</month>
<year>2025</year>
</date>
<date date-type="accepted">
<day>10</day>
<month>11</month>
<year>2025</year>
</date>
</history>
<permissions>
<copyright-statement>Copyright &#xa9; 2025 Wang, Zhang and Su.</copyright-statement>
<copyright-year>2025</copyright-year>
<copyright-holder>Wang, Zhang and Su</copyright-holder>
<license>
<ali:license_ref start_date="2025-11-20">https://creativecommons.org/licenses/by/4.0/</ali:license_ref>
<license-p>This is an open-access article distributed under the terms of the <ext-link ext-link-type="uri" xlink:href="https://creativecommons.org/licenses/by/4.0/">Creative Commons Attribution License (CC BY)</ext-link>. 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 terms.</license-p>
</license>
</permissions>
<abstract>
<p>Negative stiffness (NS) structures have obvious advantages in attenuating low-frequency vibration. Although most existing NS structures exhibit good damping effects, their stability is poor, limiting their application in complex mechanical systems. To improve their damping and stability, a negative stiffness structure composed of rubber spring and elastic beam (NSS-RB) is proposed. Its elastic properties are studied via numerical modeling. Numerical and experimental results show NSS-RB has high static and low dynamic stiffness, achieving good damping and stability. Applied to a power battery package damping system, NSS-RB outperforms the rubber spring (RS) system in vibration reduction: the low-frequency vibration attenuation rate exceeds 90%, with good ride comfort and no instability.</p>
</abstract>
<kwd-group>
<kwd>negative stiffness</kwd>
<kwd>elastic beam</kwd>
<kwd>damping system</kwd>
<kwd>dynamics</kwd>
<kwd>vibration</kwd>
</kwd-group>
<funding-group>
<funding-statement>The authors declare that no financial support was received for the research and/or publication of this article.</funding-statement>
</funding-group>
<counts>
<fig-count count="15"/>
<table-count count="1"/>
<equation-count count="13"/>
<ref-count count="23"/>
<page-count count="9"/>
</counts>
<custom-meta-group>
<custom-meta>
<meta-name>section-in-acceptance</meta-name>
<meta-value>Engine and Automotive Engineering</meta-value>
</custom-meta>
</custom-meta-group>
</article-meta>
</front>
<body>
<sec sec-type="intro" id="s1">
<label>1</label>
<title>Introduction</title>
<p>NS structures are widely used in energy absorption, vibration reduction, protection and other fields (<xref ref-type="bibr" rid="B19">Wang et al., 2019</xref>; <xref ref-type="bibr" rid="B22">Zhong et al., 2019</xref>; <xref ref-type="bibr" rid="B23">Zhou et al., 2019</xref>). At present, NS structures have become a new way to improve the vibration reduction performance of mechanical systems (<xref ref-type="bibr" rid="B3">Chen et al., 2022</xref>; <xref ref-type="bibr" rid="B4">Dara et al., 2022</xref>; <xref ref-type="bibr" rid="B10">Jin et al., 2019</xref>; <xref ref-type="bibr" rid="B1">Alomar and Concli, 2021</xref>). Researchers have done a lot of research on NS structures. For example, (<xref ref-type="bibr" rid="B20">Yu et al., 2022</xref>) proposed a quasi-zero stiffness shock absorber composed of torsion bar spring and NS structure, and studied its static nonlinear stiffness characteristics by numerical method and finite element method. However, the dynamic stiffness characteristics of the shock absorber are not analyzed in this paper, and whether this structure can be applied to the impact load condition is not introduced. <xref ref-type="bibr" rid="B2">Chan et al. (2019)</xref> designed a three-dimensional NS structure and studied its energy absorption and resilience, and found that reasonable design of structural geometric parameters could effectively improve the level of energy absorption. However, the authors did not introduce the correlation of three-directional stiffness. <xref ref-type="bibr" rid="B7">Gholikord et al. (2022)</xref> comprehensively uses design, simulation and experimental techniques to analyze the mechanical properties of NS structures and improve the damping performance under cyclic loading. In the research process, M.G used quasi-static cyclic loads without considering alternating loads and impact loads. Whether the analysis results can reflect the dynamic characteristics of the NS structure needs to be further studied. In order to improve the mechanical performance of NS structure, many NS structures are developed, such as multi-stage quasi-zero stiffness mechanism, quasi-zero stiffness isolator, negative stiffness sandwich structure and so on (<xref ref-type="bibr" rid="B8">Guo et al., 2024</xref>; <xref ref-type="bibr" rid="B13">Peiman et al., 2022</xref>; <xref ref-type="bibr" rid="B11">Meng et al., 2021</xref>). More and more negative stiffness structures are used in engineering because of their excellent vibration absorption characteristics (<xref ref-type="bibr" rid="B5">Fanc et al., 2023</xref>; <xref ref-type="bibr" rid="B9">Hong et al., 2023</xref>; <xref ref-type="bibr" rid="B18">Wang et al., 2018</xref>). In recent years, some scholars have conducted research on negative stiffness damping and its applications in various fields (<xref ref-type="bibr" rid="B15">Shi et al., 2025</xref>; <xref ref-type="bibr" rid="B17">Sudheendra and Satish, 2025</xref>; <xref ref-type="bibr" rid="B6">Gao et al., 2025</xref>; <xref ref-type="bibr" rid="B16">Sonkusare and Bera, 2025</xref>).</p>
<p>The traditional NS structures are mainly monostable and multistable structures. The two types of NS structures can achieve good damping, but under alternating load and impact load, the existing NS structures have some problems such as poor resilience, dynamic instability, and stiffness jump. These problems limit the application of NS structures in engineering. In order to overcome the disadvantages of existing negative stiffness structures, a negative stiffness structure composed of rubber spring and elastic beam (NSS-RB) is presented in the paper. The structure has high static stiffness and low dynamic stiffness, excellent damping and stability performance. And NSS-RB is applied to the vibration reduction system of electric vehicle power battery pack. The elastic properties of NSS-RB are studied by building the numerical model, and the rationality of NSS-RB is verified by the test method. The main research contents are as follows:<list list-type="order">
<list-item>
<p>The NSS-RB is designed and the elastic characteristics of high static and low dynamic stiffness are analyzed.</p>
</list-item>
<list-item>
<p>The NSS-RB stiffness test is carried out to verify the correctness of the theoretical model.</p>
</list-item>
<list-item>
<p>The dynamic characteristics of NSS-RB are analyzed by vibration contrast test.</p>
</list-item>
</list>
</p>
</sec>
<sec id="s2">
<label>2</label>
<title>Theoretical aspects</title>
<sec id="s2-1">
<label>2.1</label>
<title>Structure and principle</title>
<p>
<xref ref-type="fig" rid="F1">Figure 1</xref> shows the structure and principle of NSS-RB. The structure is shown in <xref ref-type="fig" rid="F1">Figure 1a</xref>, which is composed of upper plate, bottom bracket, rubber spring, elastic beam and the moving rod system. The upper end of the rubber spring is fixed on the upper plate, and the lower end is fixed on the bottom bracket. There are two cavities in the rubber spring, and the elastic beam and moving rod system are arranged in the cavity 1. The moving rod system comprises a pole and a slider connecting rod mechanism. The slider connecting rod mechanism is symmetrically arranged on both sides of the rod. Both ends of the elastic beam are installed in the grooves of the bottom bracket, and the sliders are installed on the elastic beam. The stiffness of NSS-RB is composed of the rubber spring stiffness k<sub>r</sub>(<italic>x</italic>) and the elastic beam stiffness k<sub>e</sub>(<italic>x</italic>), k<sub>r</sub>(<italic>x</italic>) and k<sub>e</sub>(<italic>x</italic>) are in parallel. NSS-RB damping is the rubber spring damping C<sub>R</sub>.</p>
<fig id="F1" position="float">
<label>FIGURE 1</label>
<caption>
<p>Structure and principle of NSS-RB. <bold>(a)</bold> The structure. <bold>(b)</bold> The principle.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g001.tif">
<alt-text content-type="machine-generated">Diagram labeled with parts of a mechanical system. Panel (a) shows a cross-section of the system with components like the upper plate, rubber spring, cavities, pole, slider, elastic beam, connecting rod, and bottom bracket. It includes a force diagram with symbols indicating various forces and resistances. Panel (b) demonstrates two states of compression and bending under force, with arrows indicating directions of movement. The left image is labeled &#x201C;compression&#x201D; and &#x201C;bending,&#x201D; while the right shows &#x201C;Max compression&#x201D; and &#x201C;Max bending.&#x201D;</alt-text>
</graphic>
</fig>
<p>
<xref ref-type="fig" rid="F1">Figure 1b</xref> shows the principle of NSS-RB. In the working process, the rubber spring is compressed and the elastic beam is bent. When the external force F increases, the bar moves downward, the two sliders move toward the bar, the cavity 2 is gradually compressed, and the rubber spring stiffness is nonlinear. When the external force F continues to increase, cavity 2 is completely compressed, and the stiffness of the rubber spring becomes large. The stiffness of the elastic beam varies greatly when the distance between the two sliders is different, and the stiffness is negative.</p>
<p>The stiffness curve of the rubber spring is shown in <xref ref-type="fig" rid="F2">Figure 2</xref>. The stiffness curve is divided into three sections. The linear stiffness of section&#x2160;is 65&#xa0;N/mm, which is mainly used for damping, and the deformation range of <xref ref-type="sec" rid="s1">Section 1</xref> is 0&#x2013;8.0&#xa0;mm. <xref ref-type="sec" rid="s2">Section 2</xref> is nonlinear stiffness, rubber cavity 2 is compressed gradually, the deformation range is 8.00&#x2013;11.0&#xa0;mm. <xref ref-type="sec" rid="s3">Section 3</xref> is limited stiffness, rubber cavity 2 is fully compressed to prevent excessive deformation of rubber spring.</p>
<fig id="F2" position="float">
<label>FIGURE 2</label>
<caption>
<p>Stiffness curve of rubber spring.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g002.tif">
<alt-text content-type="machine-generated">Graph showing force in newtons versus displacement in millimeters. Three regions are labeled: I for linear stiffness up to around 8 mm, II for variable stiffness between 8 and 11 mm, and III for limit stiffness after 11 mm. The curve shows increasing force with displacement, steeper in regions II and III.</alt-text>
</graphic>
</fig>
</sec>
<sec id="s2-2">
<label>2.2</label>
<title>Mechanical model</title>
<p>The mechanical properties of NSS-RB are determined by the rubber spring and the elastic beam. The rubber spring is a variable cross-section structure with nonlinear stiffness, which provides positive stiffness for NSS-RB. The elastic beam is a rectangular structure with equal section, which provides negative stiffness for NSS-RB. The mechanical model of elastic beam is shown in <xref ref-type="fig" rid="F3">Figure 3</xref>.</p>
<fig id="F3" position="float">
<label>FIGURE 3</label>
<caption>
<p>Mechanical model of elastic beam.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g003.tif">
<alt-text content-type="machine-generated">Diagram showing a beam with points A, B, C, and D and forces applied at B and C. The beam is supported at A and D. The upper part illustrates load distribution and dimensions labeled L_AB, L_BC, and L_CD. The lower section displays beam deflection with labels for angles and displacements, including positions \(O_1\), \(E\), and \(M\). Dimensions of a rectangle are shown as b and h.</alt-text>
</graphic>
</fig>
<p>The two ends of the elastic beam A and D are constrained, and Z-direction loads are applied at points B and C. In <xref ref-type="fig" rid="F3">Figure 3</xref>, L<sub>AB</sub> &#x3d; L<sub>CD</sub>. Because of the symmetry of segment AB and segment CD, segment AB and segment BC are selected to analyze the elastic characteristics. In the process of loading, elastic beams produce composite deformation, that is, tensile deformation and bending deformation (<xref ref-type="bibr" rid="B14">Quan et al., 2020</xref>; <xref ref-type="bibr" rid="B12">Mykola and Konstantin, 2021</xref>; <xref ref-type="bibr" rid="B21">Zang et al., 2021</xref>).</p>
<p>The shape of the segment AB is similar to a parabola after loading, and when the deformation is small, the segment AB is approximately circular. The deflection of E&#x2032; on segment AB&#x2019; is y and the angle is &#x3b8;, there is<disp-formula id="e1">
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<sub>A</sub> &#x3d; 0; <italic>x</italic> &#x3d; L<sub>AB</sub>, <italic>y</italic>
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</disp-formula>
</p>
<p>According to <xref ref-type="disp-formula" rid="e2">Equation 2</xref>, then <xref ref-type="disp-formula" rid="e1">Equation 1</xref> can be expressed as<disp-formula id="e3">
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</mml:mfenced>
</mml:mrow>
</mml:math>
<label>(3)</label>
</disp-formula>
</p>
<p>According to <xref ref-type="disp-formula" rid="e3">Equation 3</xref>, the deflection and angle of the end B are<disp-formula id="e4">
<mml:math id="m4">
<mml:mrow>
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<mml:mrow>
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</mml:mrow>
</mml:math>
<label>(4)</label>
</disp-formula>
</p>
<p>The bending moment M acts on both ends of segment BC to make it bend. The force model of the segment BC can be equivalent to that the midpoint of segment BC is acted on by force 2F and the force direction is downward. The end B and end C are subjected to the force F, and the force direction is upward. The deflection of the midpoint O<sub>1</sub> is<disp-formula id="e5">
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<mml:mrow>
<mml:mn>48</mml:mn>
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</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(5)</label>
</disp-formula>
</p>
<p>According to <xref ref-type="disp-formula" rid="e4">Equations 4</xref>, <xref ref-type="disp-formula" rid="e5">5</xref>, the deformation at the midpoint of the elastic beam is<disp-formula id="e6">
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<mml:mn>3</mml:mn>
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<mml:mrow>
<mml:mn>3</mml:mn>
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<mml:mi>I</mml:mi>
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<mml:mo>&#x2b;</mml:mo>
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<mml:mn>3</mml:mn>
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</mml:mrow>
<mml:mrow>
<mml:mn>48</mml:mn>
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</mml:mrow>
</mml:mfrac>
</mml:mrow>
</mml:math>
<label>(6)</label>
</disp-formula>
</p>
<p>The stiffness K of the elastic beam is<disp-formula id="e7">
<mml:math id="m7">
<mml:mrow>
<mml:mi mathvariant="normal">K</mml:mi>
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</mml:math>
<label>(7)</label>
</disp-formula>
</p>
<p>Where b is the width of the elastic beam and h is the height of the elastic beam.</p>
<p>
<xref ref-type="disp-formula" rid="e7">Equation 7</xref> shows that the stiffness of the elastic beam is affected not only by its structure size but also by the distance L<sub>BC</sub>. And the height h and L<sub>BC</sub> have the greatest influence on the stiffness. The stiffness k<sub>B</sub> is proportional to h<sup>3</sup> and inversely proportional to L<sub>BC</sub>. In the process of elastic beam deformation, if L<sub>BC</sub> is gradually reduced, the negative stiffness characteristic can be realized. The maximum deformation of the elastic beam can be calculated according to <xref ref-type="disp-formula" rid="e6">Equation 6</xref>, and the calculation results provide a basis for the design of the moving distance of the elastic beam.</p>
</sec>
<sec id="s2-3">
<label>2.3</label>
<title>Numerical example</title>
<p>In this part, the elastic characteristics of elastic beams and NSS-RB are analyzed by numerical example. The parameters of the elastic beam are shown in <xref ref-type="table" rid="T1">Table 1</xref>. And the influence of L<sub>BC</sub> on the stiffness and maximum deformation is analyzed.</p>
<table-wrap id="T1" position="float">
<label>TABLE 1</label>
<caption>
<p>The parameters of the elastic beam.</p>
</caption>
<table>
<tbody valign="top">
<tr>
<td align="left">Structure parameters</td>
<td align="left">L &#x3d; 120&#xa0;mm, <italic>b</italic> &#x3d; 5&#xa0;mm, <italic>h</italic> &#x3d; 2&#xa0;mm</td>
</tr>
<tr>
<td align="left">Distance parameters</td>
<td align="left">L &#x3d; 120mm, L<sub>AB</sub> &#x3d; 30&#xa0;mm, L<sub>BC</sub> &#x3d; 60&#xa0;mm, L<sub>CD</sub> &#x3d; 30&#xa0;mm</td>
</tr>
<tr>
<td align="left">Material parameters</td>
<td align="left">
<italic>&#x3c1;</italic> &#x3d; 7.9 &#xd7; 10<sup>3</sup>&#xa0;kg/m<sup>3</sup>, <italic>E</italic> &#x3d; 2.9 &#xd7; 10<sup>11</sup>&#xa0;N/m<sup>2</sup>, <italic>&#x3b3;</italic> &#x3d; 0.30</td>
</tr>
</tbody>
</table>
</table-wrap>
<p>
<xref ref-type="fig" rid="F4">Figure 4</xref> shows the relationship between the stiffness of the elastic beam and the L<sub>BC</sub> reduction. The stiffness decreases with the decrease of L<sub>BC</sub> and is nonlinear negative stiffness. The stiffness is 76.3&#xa0;N/mm at the initial position L<sub>BC</sub> &#x3d; 60&#xa0;mm, and the stiffness is 21.2&#xa0;N/mm at the position L<sub>BC</sub> &#x3d; 28&#xa0;mm. The stiffness is reduced by 72.2%.</p>
<fig id="F4" position="float">
<label>FIGURE 4</label>
<caption>
<p>Stiffness curve of the elastic beam.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g004.tif">
<alt-text content-type="machine-generated">Line graph depicting the decrease in stiffness measured in newtons per millimeter versus displacement in millimeters. The stiffness starts at 76.3 N/mm and gradually declines as displacement increases from 0 to 32 mm.</alt-text>
</graphic>
</fig>
<p>
<xref ref-type="fig" rid="F5">Figure 5</xref> shows the relationship between the deformation of the elastic beam and the L<sub>BC</sub> reduction. The maximum load of the elastic beam is 150&#xa0;N, and the maximum deformation is the deflection of the middle point of the elastic beam. The maximum deformation increases with the decrease of L<sub>BC</sub>. The maximum deformation is 3.93&#xa0;mm at the initial position L<sub>BC</sub> &#x3d; 60&#xa0;mm, and the maximum deformation is 7.29&#xa0;mm at the position L<sub>BC</sub> &#x3d; 28&#xa0;mm.</p>
<fig id="F5" position="float">
<label>FIGURE 5</label>
<caption>
<p>Deformation curve of the elastic beam.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g005.tif">
<alt-text content-type="machine-generated">A line graph depicts the relationship between displacement in millimeters (x-axis) and deformation in millimeters (y-axis). The curve shows a gradual increase, starting at approximately 3.93 millimeters of deformation at zero displacement, and ends around 8 millimeters of deformation at 32 millimeters of displacement. Data points are marked with blue squares.</alt-text>
</graphic>
</fig>
<p>The kinematic model of the moving bar system is shown in <xref ref-type="fig" rid="F6">Figure 6</xref>. Under the action of force F, the pole drives the connecting rod mechanism to move downward, which results in the decrease of L<sub>BC.</sub> It is necessary to establish the relationship between the displacement of moving bar system and L<sub>BC</sub> to avoid motion interference. Connecting rod <inline-formula id="inf1">
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<label>(8)</label>
</disp-formula>
</p>
<fig id="F6" position="float">
<label>FIGURE 6</label>
<caption>
<p>Kinematic model of the moving bar system.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g006.tif">
<alt-text content-type="machine-generated">Motion diagram and geometrical relationship illustration. The left side shows a vertical force labeled &#x22;F&#x22; acting downward on a structure, with arrows showing movement. The right side depicts a geometrical relationship with points B, B&#x27;, C, C&#x27;, O1, O3, and O&#x27;3 connected by lines and arcs, illustrating relationships between the points.</alt-text>
</graphic>
</fig>
<p>According to <xref ref-type="disp-formula" rid="e8">Equation 8</xref>, when O<sub>3</sub> moves to O<sub>3</sub>&#x2019;, there is<disp-formula id="e9">
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<label>(10)</label>
</disp-formula>
</p>
<p>According to <xref ref-type="disp-formula" rid="e9">Equations 9</xref>, <xref ref-type="disp-formula" rid="e10">10</xref>, the relationship between the displacement of moving bar system and L<sub>BC</sub> is described according to <xref ref-type="disp-formula" rid="e11">Equation 11</xref>.<disp-formula id="e11">
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</disp-formula>
</p>
<p>The maximum load of NSS-RB is 250&#xa0;N. <xref ref-type="fig" rid="F7">Figure 7</xref> shows the relationship between the deformation of NSS-RB and the L<sub>BC</sub> reduction. The deformation increases with the decrease of L<sub>BC</sub> and shows nonlinear characteristics. The maximum deformation is 1.75&#xa0;mm at the initial position L<sub>BC</sub> &#x3d; 60&#xa0;mm, and the maximum deformation is 11.28&#xa0;mm at the position L<sub>BC</sub> &#x3d; 28&#xa0;mm.</p>
<fig id="F7" position="float">
<label>FIGURE 7</label>
<caption>
<p>Deformation curve of NSS-RB.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g007.tif">
<alt-text content-type="machine-generated">Line graph showing the relationship between displacement in millimeters on the x-axis and deformation in millimeters on the y-axis. The graph features several data points connected by a line, starting at 1.75 mm displacement and increasing to 11.28 mm deformation at 32 mm displacement.</alt-text>
</graphic>
</fig>
<p>NSS-RB stiffness k<sub>P</sub> is the sum of the rubber spring stiffness and the elastic beam stiffness. NSS-RB stiffness is shown in <xref ref-type="fig" rid="F8">Figure 8</xref>. When the deformation D<sub>C</sub> &#x3c; 8.0&#xa0;mm, NSS-RB stiffness shows negative stiffness characteristics. The rubber spring provides positive stiffness and the elastic beam provides negative stiffness. When D<sub>C</sub> &#x3d; 0.0&#xa0;mm, k<sub>P</sub> &#x3d; 141.3&#xa0;N/mm; When D<sub>C</sub> &#x3d; 8.0&#xa0;mm, k<sub>P</sub> &#x3d; 90.0&#xa0;N/mm; the stiffness decrease is 36.3%. When D<sub>C</sub> &#x3d; 8.0&#xa0;mm, the rubber spring cavity 2 begins to be compressed. When D<sub>C</sub> &#x3d; 10.0&#xa0;mm, the rubber spring cavity 2 is fully compressed. The high static stiffness and low dynamic stiffness of NSS-RB are conducive to load and damping, a significant change in system stiffness is achieved when different displacements occur under different loads, rather than a simple linear relationship.</p>
<fig id="F8" position="float">
<label>FIGURE 8</label>
<caption>
<p>Stiffness curve of NSS-RB.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g008.tif">
<alt-text content-type="machine-generated">Graph depicting stiffness (in newtons per millimeter) versus displacement (in millimeters) for an elastic beam, rubber spring, and NSS-RB. The elastic beam shows a consistent low value, while the rubber spring and NSS-RB increase sharply after eight millimeters. Labels indicate when cavity two begins compression and when it is completely compressed.</alt-text>
</graphic>
</fig>
<p>The design of elastic beam distance L<sub>BC</sub> should not only meet the requirements of stiffness and deformation, but also meet the requirements of structural strength. The maximum stress expression of a rectangular elastic beam <inline-formula id="inf2">
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</disp-formula>
</p>
<p>The load at point B of the elastic beam <italic>F</italic>
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</disp-formula>
</p>
<p>The elastic beam material is 55SI2MNB and the tensile strength is 1,274&#xa0;MPa. <xref ref-type="fig" rid="F9">Figure 9</xref> shows the relationship between the maximum stress of the elastic beam and the L<sub>BC</sub> reduction. The maximum stress is 1,214.9&#xa0;MPa and appears at the initial position (L<sub>BC</sub> &#x3d; 60&#xa0;mm). The stress decreases with the decrease of L<sub>BC</sub>, and the relationship is linear. Therefore, in order to meet the strength requirements, it is necessary to control the initial distance L<sub>BC</sub>, that is, the initial value should not be higher than 60&#xa0;mm.</p>
<fig id="F9" position="float">
<label>FIGURE 9</label>
<caption>
<p>Stress curve of the elastic beam.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g009.tif">
<alt-text content-type="machine-generated">Line graph depicting the relationship between stress, measured in megapascals (MPa), and displacement, measured in millimeters (mm). The stress decreases linearly from 1200 MPa to 900 MPa as displacement increases from 0 to 32 mm. Data points are marked with triangles on the line.</alt-text>
</graphic>
</fig>
</sec>
</sec>
<sec id="s3">
<label>3</label>
<title>NSS-RB application</title>
<p>In recent years, with the rapid development of electric vehicle (EV), the safety of EV has been paid more and more attention. The spontaneous combustion accident of power battery pack (PBP) is increasing gradually, which has seriously endangered the life safety of drivers and passengers. Under long-term vibration condition, the power battery and high-voltage system produce large extrusion deformation, which causes leakage, short-circuit and spontaneous combustion. Therefore, the damping design of PBP is very important.</p>
<p>At present, rubber spring (RS) system is widely used in the design of PBP damping system. The low-frequency vibration attenuation rate of the rubber mount system is usually below 80%, which can not meet the damping performance requirements of PBP. In order to improve the damping rate of low frequency vibration, the negative stiffness structure is a better choice. In this part, NSS-RB specimens are made according to the analysis results, and the stiffness test and vibration test are carried out.</p>
<sec id="s3-1">
<label>3.1</label>
<title>Stiffness test</title>
<p>The lower end of NSS-RB specimen is fixed on the support of the test bench, and the upper end is fixed on the fixture of the hydraulic column. The test process is shown in <xref ref-type="fig" rid="F10">Figure 10</xref>. In static stiffness test, loading and unloading tests are carried out respectively, and the maximum displacement is 12&#xa0;mm. In dynamic stiffness test, the loading frequency of the sine wave is 2.0&#xa0;Hz and the amplitude is &#xb1;0.2&#xa0;mm, and the initial compression of NSS-RB specimen is selected by 2&#xa0;mm and 4&#xa0;mm respectively. Force and displacement data are collected during the test to analyze the static and dynamic stiffness characteristics of NSS-RB specimen.</p>
<fig id="F10" position="float">
<label>FIGURE 10</label>
<caption>
<p>NSS-RB stiffness test.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g010.tif">
<alt-text content-type="machine-generated">Diagram on the left shows a labeled structure with a loading point on top and a fixed point at the bottom, indicating deformation. The photo on the right depicts industrial machinery conducting a similar loading test, with cylindrical components and a supportive base.</alt-text>
</graphic>
</fig>
<p>
<xref ref-type="fig" rid="F11">Figure 11</xref> shows the static stiffness test result of NSS-RB specimen, which is in good agreement with the theoretical result. The deformation is less than 8&#xa0;mm, and the test stiffness shows negative stiffness. At the initial position, the test value is 155.8&#xa0;N/mm, the theoretical value is 141.3&#xa0;N/mm, and the agreement is 90.7%. In other locations, the agreements are greater than 90%. The test results at the initial position is larger than the theoretical results, the main reason is that the elastic beam buckles before elastic deformation occurs, which is not considered in the theoretical analysis.</p>
<fig id="F11" position="float">
<label>FIGURE 11</label>
<caption>
<p>Static stiffness curve of NSS-RB.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g011.tif">
<alt-text content-type="machine-generated">Graph showing stiffness versus displacement in millimeters. A solid green line represents theoretical values, while a dashed red line shows test values. Both lines follow a similar path, rising sharply after 8 mm of displacement. An inset graph displays damping stiffness, with both values decreasing slightly.</alt-text>
</graphic>
</fig>
<p>
<xref ref-type="fig" rid="F12">Figure 12</xref> shows the dynamic stiffness test result of NSS-RB specimen. When the initial compression is 2&#xa0;mm, the dynamic stiffness is 128.14&#xa0;N/mm and the loss factor is 0.148. When the initial compression is 4&#xa0;mm, the dynamic stiffness is 120.5&#xa0;N/mm and the loss factor is 0.261. The smaller the loss factor shows that the greater the elasticity of the specimen. The results show that the dynamic stiffness decreases with the increase of NSS-RB deformation.</p>
<fig id="F12" position="float">
<label>FIGURE 12</label>
<caption>
<p>Dynamic stiffness curve of NSS-RB.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g012.tif">
<alt-text content-type="machine-generated">Graph showing force versus displacement for precompression at two millimeters and four millimeters. The red line represents precompression two millimeters with the equation y = 128.14x + 152.74. The green dashed line represents precompression four millimeters with the equation y = 120.5x + 297.87.</alt-text>
</graphic>
</fig>
</sec>
<sec id="s3-2">
<label>3.2</label>
<title>Vibration test</title>
<p>The PBP has a mass of 150&#xa0;kg and is supported by six RSs. NSS-RB is used instead of RS, and the vibration comparison test was carried out. The PBP vibration test is shown in <xref ref-type="fig" rid="F13">Figure 13</xref>. The PBP is fixed on the vibration test bench, and an acceleration sensor is arranged at the upper and lower ends of the elastic support respectively. The random vibration test with amplitude &#xb1;5&#xa0;mm and with amplitude &#xb1;10&#xa0;mm are carried out respectively. The test acquisition equipment is LMS.Test.Lab, the acquisition frequency is 30&#xa0;Hz, the resolution is 0.01, and the acquisition time is 20&#xa0;s.</p>
<fig id="F13" position="float">
<label>FIGURE 13</label>
<caption>
<p>Vibration comparison test.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g013.tif">
<alt-text content-type="machine-generated">Diagram and photograph of a testbed setup. On the left, a labeled diagram shows components: the frame, acceleration sensors, battery pack, testbed, and rubber cushion. On the right, a photo depicts the physical testbed with wires visible, under an industrial ceiling.</alt-text>
</graphic>
</fig>
<p>
<xref ref-type="fig" rid="F14">Figure 14</xref> shows the random vibration test data with an amplitude of &#xb1;5&#xa0;mm. <xref ref-type="fig" rid="F14">Figure 14a</xref> shows the time-domain vibration data of PBP. The average vibration acceleration of PBP equipped with RS is 0.42&#xa0;m/s<sup>2</sup>, and the average vibration acceleration of PBP equipped with NSS-RB is 0.33&#xa0;m/s<sup>2</sup>. Compared to RS, NSS-RB reduced the acceleration by 21.4%.</p>
<fig id="F14" position="float">
<label>FIGURE 14</label>
<caption>
<p>Random vibration test data with amplitude &#xb1;5&#xa0;mm. <bold>(a)</bold> Time domain data. <bold>(b)</bold> Frequency domain data. <bold>(c)</bold> Vibration transmissibility.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g014.tif">
<alt-text content-type="machine-generated">Three graphs labeled a, b, and c. Graph a shows acceleration (m/s&#xB2;) over time (seconds) with RS and NSS-RB lines. Graph b depicts amplitude (m/s&#xB2;) over frequency (Hz), also with RS and NSS-RB lines. Graph c illustrates transmission rate (%) over time (seconds), again comparing RS and NSS-RB. RS is represented by a red dashed line, and NSS-RB by a green solid line.</alt-text>
</graphic>
</fig>
<p>
<xref ref-type="fig" rid="F14">Figure 14b</xref> shows the frequency-domain vibration data of PBP. The first peak frequency of the RS system is 5.9&#xa0;Hz, and the amplitude is 0.052&#xa0;m/s<sup>2</sup>; the first peak frequency of the NSS-RB system is 5.5&#xa0;Hz, and the amplitude is 0.032&#xa0;m/s<sup>2</sup>. Compared with RS system, the natural frequency of NSS-RB system moves to low frequency, and the peak value decreases obviously.</p>
<p>
<xref ref-type="fig" rid="F14">Figure 14c</xref> shows the vibration transmission curve. The average transmission rate of RS system is 20%, and that of NSS-RB system is 12%. The comparison results show that the damping effect of NSS-RB system is better than that of RS system under the small amplitude vibration conditions.</p>
<p>
<xref ref-type="fig" rid="F15">Figure 15</xref> shows the random vibration test data with an amplitude of &#xb1;10&#xa0;mm. The time domain vibration data is shown in <xref ref-type="fig" rid="F15">Figure 15a</xref>, and the average acceleration of PBP with RS system is 0.83&#xa0;m/s<sup>2</sup>, the average acceleration of PBP with NSS-RB system is 0.56&#xa0;m/s<sup>2</sup>. The NSS-RB system reduces the acceleration by 20% compared to the RS system.</p>
<fig id="F15" position="float">
<label>FIGURE 15</label>
<caption>
<p>Random vibration test data with amplitude &#xb1;10&#xa0;mm. <bold>(a)</bold> Time domain data. <bold>(b)</bold> Frequency domain data. <bold>(c)</bold> Vibration transmissibility.</p>
</caption>
<graphic xlink:href="fmech-11-1728890-g015.tif">
<alt-text content-type="machine-generated">Three graphs compare RS and NSS-RB data. Graph (a) shows acceleration over time, indicating more fluctuation in RS. Graph (b) shows amplitude versus frequency, with RS peaking higher. Graph (c) depicts transmission rate over time, where RS remains higher than NSS-RB.</alt-text>
</graphic>
</fig>
<p>The frequency-domain vibration data is shown in <xref ref-type="fig" rid="F15">Figure 15b</xref>, the first peak frequency of the RS system is 6.2&#xa0;Hz, and the amplitude is 0.064&#xa0;m/s<sup>2</sup>; the first peak frequency of the NSS-RB system is 4.7&#xa0;Hz, and the amplitude is 0.039&#xa0;m/s<sup>2</sup>. <xref ref-type="fig" rid="F15">Figure 15c</xref> shows the vibration transmission curve, the average transmission rate of RS system is 21.5%, and that of NSS-RB system is 9.5%.</p>
<p>The results also show that with the increase of the amplitude of random vibration, the natural frequency of RS system moves to high frequency and the damping performance becomes worse, the natural frequency of NSS-RB system moves to low frequency and the damping performance becomes better. Therefore, compared with RS, NSS-RB has obvious advantage in damping.</p>
</sec>
</sec>
<sec sec-type="conclusion" id="s4">
<label>4</label>
<title>Conclusion</title>
<p>In this paper, a negative stiffness structure composed of rubber spring and elastic beam (NSS-RB) is presented. The rubber spring provides positive stiffness and the elastic beam provides negative stiffness. Numerical and experimental results show that NSS-RB has high static stiffness and low dynamic stiffness, and the stiffness decreases with the increase of its deformation. The characteristic is very suitable for loading and damping.</p>
<p>The application of NSS-RB in the damping system of PBP is introduced. The NSS-RB system reduces the vibration of the battery pack, which has a positive impact on the safety of electric vehicle vehicles. Under amplitude vibration conditions, the damping effect of NSS-RB system is better than that of RS system. with the increase of the amplitude of random vibration, the natural frequency of NSS-RB system moves to low frequency and the damping performance becomes better.</p>
</sec>
</body>
<back>
<sec sec-type="data-availability" id="s5">
<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 authors.</p>
</sec>
<sec sec-type="author-contributions" id="s6">
<title>Author contributions</title>
<p>YW: Data curation, Writing &#x2013; original draft. BZ: Methodology, Writing &#x2013; review and editing. XS: Conceptualization, Validation, Writing &#x2013; review and editing.</p>
</sec>
<ack>
<title>Acknowledgements</title>
<p>The authors would like to acknowledge the support of Naveco Automobile Co., Ltd for providing the materials and apparatus.</p>
</ack>
<sec sec-type="COI-statement" id="s8">
<title>Conflict of interest</title>
<p>Author BZ was employed by Naveco Automobile Co., Ltd.</p>
<p>The remaining 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>
</sec>
<sec sec-type="ai-statement" id="s9">
<title>Generative AI statement</title>
<p>The authors declare that no Generative AI was used in the creation of this manuscript.</p>
<p>Any alternative text (alt text) provided alongside figures in this article has been generated by Frontiers with the support of artificial intelligence and reasonable efforts have been made to ensure accuracy, including review by the authors wherever possible. If you identify any issues, please contact us.</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>
<fn-group>
<fn fn-type="custom" custom-type="edited-by">
<p>
<bold>Edited by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/2872905/overview">Fen Lin</ext-link>, Nanjing University of Aeronautics and Astronautics, China</p>
</fn>
<fn fn-type="custom" custom-type="reviewed-by">
<p>
<bold>Reviewed by:</bold> <ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/3250965/overview">Ming Cao</ext-link>, Nanchang University, China</p>
<p>
<ext-link ext-link-type="uri" xlink:href="https://loop.frontiersin.org/people/3256702/overview">Bo Li</ext-link>, Jiangsu University of Technology, China</p>
</fn>
</fn-group>
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