<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd">
<article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article">
 <front>
  <journal-meta>
   <journal-id journal-id-type="publisher-id">
    wjet
   </journal-id>
   <journal-title-group>
    <journal-title>
     World Journal of Engineering and Technology
    </journal-title>
   </journal-title-group>
   <issn pub-type="epub">
    2331-4222
   </issn>
   <issn publication-format="print">
    2331-4249
   </issn>
   <publisher>
    <publisher-name>
     Scientific Research Publishing
    </publisher-name>
   </publisher>
  </journal-meta>
  <article-meta>
   <article-id pub-id-type="doi">
    10.4236/wjet.2024.123044
   </article-id>
   <article-id pub-id-type="publisher-id">
    wjet-135246
   </article-id>
   <article-categories>
    <subj-group subj-group-type="heading">
     <subject>
      Articles
     </subject>
    </subj-group>
    <subj-group subj-group-type="Discipline-v2">
     <subject>
      Chemistry 
     </subject>
     <subject>
       Materials Science, Engineering
     </subject>
    </subj-group>
   </article-categories>
   <title-group>
    The Method of Thermoelectric Energy Generations Based on the Axial and Radial Flux Electromagnetic Inductions
    <sup>*</sup>
   </title-group>
   <contrib-group>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Hiroshi
      </surname>
      <given-names>
       Uechi
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Lisa
      </surname>
      <given-names>
       Uechi
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff2"> 
      <sup>2</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Schun T.
      </surname>
      <given-names>
       Uechi
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff3"> 
      <sup>3</sup>
     </xref>
    </contrib>
   </contrib-group> 
   <aff id="aff1">
    <addr-line>
     aOsaka Gakuin University, Osaka, Japan
    </addr-line> 
   </aff> 
   <aff id="aff2">
    <addr-line>
     aBeckman Research Institute, University of California, CA, USA
    </addr-line> 
   </aff> 
   <aff id="aff3">
    <addr-line>
     aData-Scientist, Tokyo, Japan
    </addr-line> 
   </aff> 
   <pub-date pub-type="epub">
    <day>
     13
    </day> 
    <month>
     06
    </month>
    <year>
     2024
    </year>
   </pub-date> 
   <volume>
    12
   </volume> 
   <issue>
    03
   </issue>
   <fpage>
    715
   </fpage>
   <lpage>
    730
   </lpage>
   <history>
    <date date-type="received">
     <day>
      18,
     </day>
     <month>
      June
     </month>
     <year>
      2024
     </year>
    </date>
    <date date-type="published">
     <day>
      11,
     </day>
     <month>
      June
     </month>
     <year>
      2024
     </year> 
    </date> 
    <date date-type="accepted">
     <day>
      11,
     </day>
     <month>
      August
     </month>
     <year>
      2024
     </year> 
    </date>
   </history>
   <permissions>
    <copyright-statement>
     © Copyright 2014 by authors and Scientific Research Publishing Inc. 
    </copyright-statement>
    <copyright-year>
     2014
    </copyright-year>
    <license>
     <license-p>
      This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/
     </license-p>
    </license>
   </permissions>
   <abstract>
    The traditional thermoelectric energy conversion techniques are explained in detail in terms of the axial flux electromagnetic (AFE) and the radial flux electromagnetic (RFE) inductions, and applications to heat engines for the energy-harvesting technologies are discussed. The idea is induced by the analysis of thermomechanical dynamics (TMD) for a nonequilibrium irreversible thermodynamic system of heat engines (a drinking bird, a low temperature Stirling engine), resulting in thermoelectric energy generation different from conventional heat engines. The mechanism of thermoelectric energy conversion can be categorized as the axial flux generator (AFG) and the radial flux generator (RFG). The axial flux generator is helpful for low mechanoelectric energy conversion and activations of waste heat from macroscopic energy generators, such as wind, geothermal, thermal, nuclear power plants and heat-dissipation lines, and the device contributes to solving environmental problems to maintain clean and sustainable energy as one of the energy harvesting technologies.
   </abstract>
   <kwd-group> 
    <kwd>
     Axial Flux and Radial Flux Generators
    </kwd> 
    <kwd>
      Thermomechanical Dynamics (TMD)
    </kwd> 
    <kwd>
      Thermoelectric Energy Conversions
    </kwd>
   </kwd-group>
  </article-meta>
 </front>
 <body>
  <sec id="s1">
   <title>1. Introduction</title>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The prosperity of human society essentially requires advanced macroscopic energy generators (MEGs) such as turbines, motors and rotors for wind, hydroelectric, geothermal, thermal, nuclear power plants and so forth. However, the characteristic feature of MEGs is essentially directed to mass production and consumption of heat and energy, resulting in an enormous amount of abandoned waste heat and chemical substances, and so, our society needs to develop technologies for sustainable developmental goals (SDGs).</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>Based on very sensitive thermoelectric devices of low temperature heat engines (a drinking bird <xref ref-type="bibr" rid="scirp.135246-1">
     [1]
    </xref> and low temperature Stirling engines <xref ref-type="bibr" rid="scirp.135246-2">
     [2]
    </xref>), we proposed thermoelectric generators to activate discarded waste heat into usable electric power. The low temperature heat engines of a drinking bird and a Stirling engine can work at small temperature difference, producing usable electric energy <xref ref-type="bibr" rid="scirp.135246-3">
     [3]
    </xref>-<xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>. It is possible to activate electric power from abandoned waste heat by the method of axial flux electromagnetic induction <xref ref-type="bibr" rid="scirp.135246-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.135246-4">
     [4]
    </xref>.</p>
  </sec><sec id="s2">
   <title>2. The Traditional Thermomechanical Convertors, and the 3<sup>rd</sup> Kind New Convertor</title>
   <p>1) Macroscopic high-power thermoelectric generators</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The traditional mechanoelectric or thermoelectric convertors are categorized as the radial flux generator (RFG) by the classification of magnetic flux lines, which is suitable for huge energy productions and requires high speed rotations of turbines (<xref ref-type="fig" rid="fig1">
     Figure 1
    </xref> and <xref ref-type="fig" rid="fig2">
     Figure 2
    </xref>).</p>
   <fig id="fig1" position="float">
    <label>Figure 1</label>
    <caption>
     <title>Figure 1. Macroscopic high-power thermoelectric energy generators.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId14.jpeg?20240815031847" />
   </fig>
   <p>Although the radial flux generators (RFG) are qualified for producing high electric power, it is not qualified for reactivating electric power from a low temperature heat flow, such as 40˚C &lt; T &lt; 100˚C boiled water, waste heat from industries. In general, it is known that the system can only use 1/3 of produced total heat-energy, and 2/3 of heat-energy is not used or dissipated eventually in an external environment.</p>
   <p>2) Microscopic, thermoelectric power generation.</p>
   <p>The second traditional devices for thermoelectricity are microscopic power generators using crystal structure, transistors, a thermocouple (thermoelectrical thermometer), etc., known as Seebeck effect and Peltier effect (<xref ref-type="fig" rid="fig3">
     Figure 3
    </xref>). Microscopic and thermoelectric power generators are known as expensive and less efficient, and 2/3 of total heat-energy is dissipated as many kinds of waste.</p>
   <fig id="fig2" position="float">
    <label>Figure 2</label>
    <caption>
     <title>Figure 2. (a) The system is large and heavyweight. It loses 2/3 of produced heat-energy to generate electric power. (b) The typical steam turbine. High speed and temperature are necessary.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId15.jpeg?20240815031847" />
   </fig>
   <fig id="fig3" position="float">
    <label>Figure 3</label>
    <caption>
     <title>Figure 3. This is a microscopic energy harvesting technology (EHT). The p-doped and n-doped semiconductors induce heat flows and electric current.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId16.jpeg?20240815031846" />
   </fig>
   <p>3) The 3<sup>rd</sup>-kind, new thermoelectric energy production</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>On the other hand, the axial flux generator (AFG) is most suitable for activating sensitive boiled water, waste heat from industries. This is an important consequence derived from the analysis of thermomechanical dynamics (TMD), which is proposed by the authors for nonequilibrium irreversible states (NISs) of heat engines <xref ref-type="bibr" rid="scirp.135246-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>. The disk-magnet electromagnetic induction (DM-EMI) technique with a low temperature Stirling engine revealed that electric power generation from low heat flows can be possible. This is assured by the theoretical analysis of TMD, proving that an optimal speed of mechanical rotation can exist in low rotational speed (about 30 - 60 rpm <xref ref-type="bibr" rid="scirp.135246-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.135246-4">
     [4]
    </xref>). Therefore, a low temperature, thermoelectric generation Stirling engine (TEG-Stirling engine) can be constructed. In this review, we explain and emphasize that the analysis of thermomechanical dynamics (TMD) applied to TEG-Stirling engine generates a low-speed, low-weight, optimal TEG-Stirling engine.</p>
   <fig id="fig4" position="float">
    <label>Figure 4</label>
    <caption>
     <title>Figure 4. A drinking bird (DB).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId17.jpeg?20240815031846" />
   </fig>
   <p>The idea of the 3<sup>rd</sup>-kind, new thermoelectric energy production is induced by the analysis of thermomechanical dynamics (TMD) for a nonequilibrium irreversible thermodynamic system of heat engines (a drinking bird, a low temperature Stirling engine), resulting in thermoelectric energy generation different from conventional heat engines, 1) and 2).</p>
   <p>A drinking bird (DB) in <xref ref-type="fig" rid="fig4">
     Figure 4
    </xref> is also a simple and efficient heat engine. A cup of ordinary water produces mechanical motion, and the mechanical motion is changed to electric power (thermoelectric generation).</p>
   <p>We proposed and solved thermomechanical equation of motion for the drinking bird <xref ref-type="bibr" rid="scirp.135246-1">
     [1]
    </xref>.</p>
   <p>A low temperature Stirling engine (LTSE) is shown in <xref ref-type="fig" rid="fig5">
     Figure 5
    </xref>. The upward heat-flow is changed into mechanical work (the flywheel rotations). A cup of hot water produces mechanical motion, and the nonequilibrium irreversible motion is solved by deriving a dissipative equation of motion <xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>.</p>
   <fig id="fig5" position="float">
    <label>Figure 5</label>
    <caption>
     <title>Figure 5. A low temperature Stirling engine (LTSE).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId18.jpeg?20240815031847" />
   </fig>
   <p>The simple amusing toys are scientifically very fundamental. A drinking bird and a Stirling engine are heat engines, and the toys work in nonequilibrium irreversible states (NISs). The physical states of heat engines are not in thermodynamic nor mechanical equilibrium, and not simply explained by just thermodynamics + mechanics.</p>
   <p>Therefore, one needs a method for NISs. It should be emphasized that electric power can be produced from low-speed revolutions, for example, about 30 rpm - 60 rpm. This is an important fact derived from TMD analyses.</p>
  </sec><sec id="s3">
   <title>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>3. The Method of TMD</title>
   <p>The equation of motion and time-dependent physical quantities, such as internal energy 
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      <mi>
        ε 
      </mi> 
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         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
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    </math>, work W(t), entropy S(t) and temperature 
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      <mover accent="true"> 
       <mi>
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    </math> of heat engines are solved self-consistently by the method of thermomechanical dynamics (TMD). The method of TMD is a new classical approach proposed by the authors, along the work of Gibbs’ thermodynamics which is based on fundamental thermodynamics and needs profound discussions on physical foundations. Hence, readers who are interested in theoretical discussions should be directed to references <xref ref-type="bibr" rid="scirp.135246-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>.</p>
   <p>The method of TMD requires three conditions.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>1) The dissipative equation of motion</p>
   <p>In the case that mechanical and thermal states coexist, such as thermomechanical states of heat engines, the dissipative equation of motion for work must be constructed by considering phenomenological effects of frictional variations, time-dependent changes of physical quantities, thermal conductivity and efficiency.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>Because time-symmetry is broken in the system of heat engines, there is no Euler-Lagrange type derivation of a correct dissipative equation of motion. It would be useful to make use of Hamiltonian or Lagrangian method at the beginning to find an approximate dissipative equation of motion and then, find an appropriate dissipative equation of motion.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>2) The total energy-flow conservation law</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The thermodynamic work 
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   <p>Thermodynamic equilibrium is defined by 
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   <p>The expression of heat flow (entropy flow) is used</p>
   <p>
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   <p>in the analysis of heat engines.</p>
   <p>3) Temperature, 
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    </math>, in a nonequilibrium irreversible state</p>
   <p>The measure of a nonequilibrium irreversible state is defined by the ratio of entropy-flow against energy-flow:</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        τ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mfrac> 
       <mrow> 
        <mrow> 
         <mrow> 
          <mi>
            T 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            S 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
         <mo>
           / 
         </mo> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </mrow> 
       </mrow> 
       <mrow> 
        <mrow> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            ε 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
         <mo>
           / 
         </mo> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </mrow> 
       </mrow> 
      </mfrac> 
      <mo>
        = 
      </mo> 
      <mfrac> 
       <mrow> 
        <mrow> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            Q 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
         <mo>
           / 
         </mo> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </mrow> 
       </mrow> 
       <mrow> 
        <mrow> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            ε 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
         <mo>
           / 
         </mo> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </mrow> 
       </mrow> 
      </mfrac> 
      <mo>
        . 
      </mo> 
     </mrow> 
    </math> (3)</p>
   <p>The value of 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        τ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> is a dimensionless, positive-definite function, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        τ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        &gt; 
      </mo> 
      <mn>
        0 
      </mn> 
     </mrow> 
    </math>. The temperature in nonequilibrium state (NISs) is defined by,</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mover accent="true"> 
       <mi>
         T 
       </mi> 
       <mo>
         ˜ 
       </mo> 
      </mover> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <msub> 
       <mi>
         T 
       </mi> 
       <mn>
         0 
       </mn> 
      </msub> 
      <mi>
        τ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        , 
      </mo> 
     </mrow> 
    </math> (4)</p>
   <p>where 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         T 
       </mi> 
       <mn>
         0 
       </mn> 
      </msub> 
     </mrow> 
    </math> is the initial equilibrium temperature. When 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        τ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mn>
        1 
      </mn> 
     </mrow> 
    </math> holds identically with respect to time t, it defines thermodynamic equilibrium, which shows no work exists, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <msub> 
         <mi>
           W 
         </mi> 
         <mrow> 
          <mi>
            t 
          </mi> 
          <mi>
            h 
          </mi> 
         </mrow> 
        </msub> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          t 
        </mi> 
       </mrow> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mn>
        0 
      </mn> 
     </mrow> 
    </math>, at thermodynamic equilibrium. The conditions of near equilibrium states, local equilibrium, linearity of fluxes and forces of transport processes <xref ref-type="bibr" rid="scirp.135246-7">
     [7]
    </xref>-<xref ref-type="bibr" rid="scirp.135246-9">
     [9]
    </xref> are studied by the condition, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        τ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mfrac> 
       <mrow> 
        <mrow> 
         <mrow> 
          <mi>
            T 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            S 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
         <mo>
           / 
         </mo> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </mrow> 
       </mrow> 
       <mrow> 
        <mrow> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            ε 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             t 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mrow> 
         <mo>
           / 
         </mo> 
         <mrow> 
          <mtext>
            d 
          </mtext> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </mrow> 
       </mrow> 
      </mfrac> 
      <mo>
        ~ 
      </mo> 
      <mn>
        1 
      </mn> 
     </mrow> 
    </math> in the TMD method.</p>
  </sec><sec id="s4">
   <title>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>4. The Equation of Motion for Stirling Engine</title>
   <p>A theoretical and schematic low temperature Stirling engine is shown in <xref ref-type="fig" rid="fig6">
     Figure 6
    </xref>, and the device consists of the following functions:</p>
   <fig id="fig6" position="float">
    <label>Figure 6</label>
    <caption>
     <title>Figure 6. A theoretical and schematic structure of a low temperature Stirling engine <xref ref-type="bibr" rid="scirp.135246-6">
       [6]
      </xref>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId53.jpeg?20240815031848" />
   </fig>
   <p>1) Heat source: A homogeneous heat flow from boiled water (40˚C - 100˚C) and geothermal heat, etc. The heat flow coming into the system is defined by 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          Q 
        </mi> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          t 
        </mi> 
       </mrow> 
      </mrow> 
      <mo>
        &gt; 
      </mo> 
      <mn>
        0 
      </mn> 
     </mrow> 
    </math>.</p>
   <p>2) Heat exchangers: The power piston is used to improve the heat flow and the flywheel rotation affected by friction losses.</p>
   <p>3) Regenerator: The internal mechanism of heat exchangers between a hot plate and a cold plate. The thermomechanical conversion for work depends on thermal efficiency, heat transfer, viscous pumping and friction losses.</p>
   <p>4) Heat sink: The temperature difference between a hot plate and a cold plate is needed for internal heat flows.</p>
   <p>5) Displacer: The thermal heat flow from a hot plate to a cold plate exerts vertical oscillations of the displacer. The efficiency of displacer to maintain appropriate heat dissipations is essential for mechanical rotations of the flywheel.</p>
   <p>It is essential to understand that heat engines in general are not in thermodynamic equilibrium, but in nonequilibrium irreversible states (NISs). Therefore, it is important to have a different theoretical approach for NISs, which is the reason why we proposed the method of TMD. The piecewise continuous driving forces produced by frictional and thermal fluctuations are assumed to couple to thermodynamic work, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mi>
         w 
       </mi> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, of the flywheel and power-piston with an associating dissipation of heat.</p>
   <p>As the first requirement (1) of TMD, the dissipative equation of motion for a low temperature Stirling engine is proposed by:</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         I 
       </mi> 
       <mn>
         0 
       </mn> 
      </msub> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ″ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        + 
      </mo> 
      <mi>
        c 
      </mi> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        − 
      </mo> 
      <msub> 
       <mi>
         λ 
       </mi> 
       <mi>
         w 
       </mi> 
      </msub> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mi>
         w 
       </mi> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mrow> 
       <mo>
         | 
       </mo> 
       <mrow> 
        <mi>
          sin 
        </mi> 
        <mi>
          θ 
        </mi> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         | 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mn>
        0 
      </mn> 
      <mo>
        , 
      </mo> 
     </mrow> 
    </math> (5)</p>
   <p>where 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         λ 
       </mi> 
       <mi>
         w 
       </mi> 
      </msub> 
     </mrow> 
    </math> is a dimensionless coupling constant for heat and mechanical work, and the angle, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        θ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, is chosen as in <xref ref-type="fig" rid="fig7">
     Figure 7
    </xref>. The term 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mo>
         | 
       </mo> 
       <mrow> 
        <mi>
          sin 
        </mi> 
        <mi>
          θ 
        </mi> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         | 
       </mo> 
      </mrow> 
     </mrow> 
    </math> expresses piecewise continuous driving forces produced by rotations, frictional and nonequilibrium thermal fluctuations, and c is a friction constant.</p>
   <fig id="fig7" position="float">
    <label>Figure 7</label>
    <caption>
     <title>Figure 7. The rotational angle, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <mi>
         
   θ
  
        </mi>
  
        <mrow>
   
         <mo>
          
    (
   
         </mo> 
   
         <mi>
          
    t
   
         </mi> 
   
         <mo>
          
    )
   
         </mo>
  
        </mrow>
 
       </mrow>

      </math>, starting from the vertical axis.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId66.jpeg?20240815031848" />
   </fig>
   <p>Although the fundamental equation of motion (5) seems simple, its mathematical and physical consequences are profound. The piecewise continuous driving force in (5) immediately indicates that the acceleration is not defined as differentiable and continuous quantity as supposed in Newtonian mechanics. The acceleration cannot be determined as the second-order derivative derived from the trajectory of motion, because the driving force contains jump discontinuities in the entire domains of motion.</p>
  </sec><sec id="s5">
   <title>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>5. The Solution to the Dissipative Equation of Motion of TEG-Stirling Engine</title>
   <p>We show the computer simulations by employing the following incoming heat 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mrow> 
        <mi>
          i 
        </mi> 
        <mi>
          n 
        </mi> 
       </mrow> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>,</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mrow> 
        <mi>
          i 
        </mi> 
        <mi>
          n 
        </mi> 
       </mrow> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mi>
         H 
       </mi> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mrow> 
        <mn>
          1.0 
        </mn> 
        <mo>
          − 
        </mo> 
        <msup> 
         <mtext>
           e 
         </mtext> 
         <mrow> 
          <mo>
            − 
          </mo> 
          <mi>
            ξ 
          </mi> 
          <mi>
            t 
          </mi> 
         </mrow> 
        </msup> 
       </mrow> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> (6)</p>
   <p>and heat flow 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <msub> 
         <mi>
           Q 
         </mi> 
         <mrow> 
          <mi>
            i 
          </mi> 
          <mi>
            n 
          </mi> 
         </mrow> 
        </msub> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          t 
        </mi> 
       </mrow> 
      </mrow> 
     </mrow> 
    </math>, as shown in <xref ref-type="fig" rid="fig8">
     Figure 8
    </xref> and <xref ref-type="fig" rid="fig9">
     Figure 9
    </xref>, and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mi>
         H 
       </mi> 
      </msub> 
     </mrow> 
    </math> and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
       ξ 
     </mi> 
    </math> are free parameters to adjust in the computer simulations, e.g., 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mi>
         H 
       </mi> 
      </msub> 
      <mo>
        ~ 
      </mo> 
      <mn>
        100 
      </mn> 
      <mtext>
          
      </mtext> 
      <mtext>
        cal 
      </mtext> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        ξ 
      </mi> 
      <mo>
        ~ 
      </mo> 
      <mn>
        6.51 
      </mn> 
      <mo>
        × 
      </mo> 
      <msup> 
       <mrow> 
        <mn>
          10 
        </mn> 
       </mrow> 
       <mrow> 
        <mo>
          − 
        </mo> 
        <mn>
          3 
        </mn> 
       </mrow> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mrow> 
        <mrow> 
         <mn>
           1 
         </mn> 
         <mo>
           / 
         </mo> 
         <mtext>
           s 
         </mtext> 
        </mrow> 
       </mrow> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> for the current simulations.</p>
   <fig id="fig8" position="float">
    <label>Figure 8</label>
    <caption>
     <title>Figure 8. The total heat-in, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <msub> 
   
         <mi>
          
    Q
   
         </mi> 
   
         <mrow> 
    
          <mi>
           
     i
    
          </mi>
    
          <mi>
           
     n
    
          </mi>
   
         </mrow> 
  
        </msub> 
  
        <mrow>
   
         <mo>
          
    (
   
         </mo> 
   
         <mi>
          
    t
   
         </mi> 
   
         <mo>
          
    )
   
         </mo>
  
        </mrow>
 
       </mrow>

      </math>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId84.jpeg?20240815031849" />
   </fig>
   <fig id="fig9" position="float">
    <label>Figure 9</label>
    <caption>
     <title>Figure 9. The heat flow, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <mrow>
   
         <mrow> 
    
          <mtext>
           
     d
    
          </mtext>
    
          <msub> 
     
           <mi>
             Q 
           </mi> 
     
           <mrow> 
            <mi>
              i 
            </mi> 
            <mi>
              n 
            </mi> 
           </mrow> 
    
          </msub> 
    
          <mrow>
     
           <mo>
             ( 
           </mo> 
     
           <mi>
             t 
           </mi> 
     
           <mo>
             ) 
           </mo>
    
          </mrow>
   
         </mrow>
   
         <mo>
          
    /
   
         </mo>
   
         <mrow> 
    
          <mtext>
           
     d
    
          </mtext>
    
          <mi>
           
     t
    
          </mi>
   
         </mrow>
  
        </mrow> 
 
       </mrow>

      </math>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId87.jpeg?20240815031849" />
   </fig>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The dissipative equation of motion, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
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       </mi> 
       <mrow> 
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      </mrow> 
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    </math> and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
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        <mtext>
          d 
        </mtext> 
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            i 
          </mi> 
          <mi>
            n 
          </mi> 
         </mrow> 
        </msub> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          t 
        </mi> 
       </mrow> 
      </mrow> 
     </mrow> 
    </math> with 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
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       </mi> 
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         ( 
       </mo> 
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         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mi>
        η 
      </mi> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mrow> 
        <mi>
          i 
        </mi> 
        <mi>
          n 
        </mi> 
       </mrow> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
       ξ 
     </mi> 
    </math> and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
       η 
     </mi> 
    </math> are arbitrarily chosen small values) and Equation (5) are used to find the heat-energy solution for kinetic work, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mrow> 
        <mi>
          w 
        </mi> 
        <mi>
          k 
        </mi> 
       </mrow> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        θ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> by maintaining the total energy-flow conservation law, (1) and (2). The computations should be repeated by taking different values of 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
       ξ 
     </mi> 
    </math> and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
       η 
     </mi> 
    </math> until reasonable experimental values of angular velocity 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        θ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> are obtained.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The number of rotations 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mrow> 
        <mi>
          θ 
        </mi> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mn>
          2 
        </mn> 
        <mi>
          π 
        </mi> 
       </mrow> 
      </mrow> 
     </mrow> 
    </math> (revolutions) and the angular velocity 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mrow> 
        <msup> 
         <mi>
           θ 
         </mi> 
         <mo>
           ′ 
         </mo> 
        </msup> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mn>
          2 
        </mn> 
        <mi>
          π 
        </mi> 
       </mrow> 
      </mrow> 
     </mrow> 
    </math> (revolutions/s) of the flywheel are respectively shown in <xref ref-type="fig" rid="fig10">
     Figure 10
    </xref> and <xref ref-type="fig" rid="fig11">
     Figure 11
    </xref>. The maximum angular velocity seems stable and constant, but one can notice that the angular velocity in <xref ref-type="fig" rid="fig11">
     Figure 11
    </xref> has tiny fluctuations along the solution. The tiny fluctuations are caused by frictional variations and thermal fluctuations coming from the displacer and working fluid.</p>
   <fig id="fig10" position="float">
    <label>Figure 10</label>
    <caption>
     <title>Figure 10. The number of revolutions, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <mrow>
   
         <mrow> 
    
          <mi>
           
     θ
    
          </mi>
    
          <mrow>
     
           <mo>
             ( 
           </mo> 
     
           <mi>
             t 
           </mi> 
     
           <mo>
             ) 
           </mo>
    
          </mrow>
   
         </mrow>
   
         <mo>
          
    /
   
         </mo>
   
         <mrow> 
    
          <mn>
           
     2
    
          </mn>
    
          <mi>
           
     π
    
          </mi>
   
         </mrow>
  
        </mrow> 
 
       </mrow>

      </math>, in the time range 0 &lt; t &lt; 1000.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId116.jpeg?20240815031849" />
   </fig>
   <fig id="fig11" position="float">
    <label>Figure 11</label>
    <caption>
     <title>Figure 11. The angular velocity, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <mrow>
   
         <mrow> 
    
          <msup> 
     
           <mi>
             θ 
           </mi> 
     
           <mo>
             ′ 
           </mo> 
    
          </msup> 
    
          <mrow>
     
           <mo>
             ( 
           </mo> 
     
           <mi>
             t 
           </mi> 
     
           <mo>
             ) 
           </mo>
    
          </mrow>
   
         </mrow>
   
         <mo>
          
    /
   
         </mo>
   
         <mrow> 
    
          <mn>
           
     2
    
          </mn>
    
          <mi>
           
     π
    
          </mi>
   
         </mrow>
  
        </mrow> 
 
       </mrow>

      </math> (revolutions/s). Note the tiny fluctuations along the angular velocity.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId120.jpeg?20240815031849" />
   </fig>
   <p>The trajectory 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        θ 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> and angular velocity 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> are continuous and differentiable, whereas the angular acceleration 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ″ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> is piecewise continuous and has finite numbers of jump discontinuities in a finite interval. The whole view of acceleration results in an assembly of hedgehog-like spiny lines as shown in <xref ref-type="fig" rid="fig12">
     Figure 12
    </xref>. The realistic flywheel thermal motion is produced reasonably well by the dissipative equation of motion (5). When heat exchangers and regenerators work properly, the flywheel rotation persists for a long period of time. Numerical calculations and self-consistency relations are discussed in detail in <xref ref-type="bibr" rid="scirp.135246-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>. Thermodynamic work,</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         Q 
       </mi> 
       <mrow> 
        <mi>
          w 
        </mi> 
        <mi>
          k 
        </mi> 
       </mrow> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mo>
        = 
      </mo> 
      <mfrac> 
       <mrow> 
        <msub> 
         <mi>
           I 
         </mi> 
         <mn>
           0 
         </mn> 
        </msub> 
       </mrow> 
       <mn>
         2 
       </mn> 
      </mfrac> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <msup> 
       <mrow> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mn>
         2 
       </mn> 
      </msup> 
     </mrow> 
    </math> (Joule) (7)</p>
   <p>is shown in <xref ref-type="fig" rid="fig13">
     Figure 13
    </xref>. The rotational energy reaches a maximum stable value, which has a continuous, tiny-wiggly line because of 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msup> 
       <mi>
         θ 
       </mi> 
       <mo>
         ′ 
       </mo> 
      </msup> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>. The dissipative equation of motion is successful for producing thermomechanical flywheel rotations and applied to thermoelectric energy conversions <xref ref-type="bibr" rid="scirp.135246-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.135246-4">
     [4]
    </xref>.</p>
   <fig id="fig12" position="float">
    <label>Figure 12</label>
    <caption>
     <title>Figure 12. The piecewise continuous angular acceleration, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <msup> 
   
         <mi>
          
    θ
   
         </mi> 
   
         <mo>
          
    ″
   
         </mo> 
  
        </msup> 
  
        <mrow>
   
         <mo>
          
    (
   
         </mo> 
   
         <mi>
          
    t
   
         </mi> 
   
         <mo>
          
    )
   
         </mo>
  
        </mrow>
 
       </mrow>

      </math> (rad/s<sup>2</sup>), 0 &lt; t &lt; 1000.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId132.jpeg?20240815031849" />
   </fig>
   <fig id="fig13" position="float">
    <label>Figure 13</label>
    <caption>
     <title>Figure 13. Thermodynamic work, 

      <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
  
        <msub> 
   
         <mi>
          
    Q
   
         </mi> 
   
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          <mi>
           
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          </mi>
    
          <mi>
           
     k
    
          </mi>
   
         </mrow> 
  
        </msub> 
  
        <mrow>
   
         <mo>
          
    (
   
         </mo> 
   
         <mi>
          
    t
   
         </mi> 
   
         <mo>
          
    )
   
         </mo>
  
        </mrow>
  
        <mo>
         
   =
  
        </mo>
  
        <mfrac> 
   
         <mrow> 
    
          <msub> 
     
           <mi>
             I 
           </mi> 
     
           <mn>
             0 
           </mn> 
    
          </msub> 
   
         </mrow> 
   
         <mn>
          
    2
   
         </mn> 
  
        </mfrac> 
  
        <msup> 
   
         <mi>
          
    θ
   
         </mi> 
   
         <mo>
          
    ′
   
         </mo> 
  
        </msup> 
  
        <msup> 
   
         <mrow> 
    
          <mrow>
     
           <mo>
             ( 
           </mo> 
     
           <mi>
             t 
           </mi> 
     
           <mo>
             ) 
           </mo>
    
          </mrow>
   
         </mrow> 
   
         <mn>
          
    2
   
         </mn> 
  
        </msup> 
 
       </mrow>

      </math>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId137.jpeg?20240815031849" />
   </fig>
   <p>The thermomechanical states of the heat engine are in nonequilibrium irreversible states (NISs), and time-dependent thermodynamic work 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         W 
       </mi> 
       <mrow> 
        <mi>
          t 
        </mi> 
        <mi>
          h 
        </mi> 
       </mrow> 
      </msub> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, internal energy 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        ε 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, energy dissipation or entropy 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mrow> 
        <mi>
          T 
        </mi> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          S 
        </mi> 
        <mrow> 
         <mo>
           ( 
         </mo> 
         <mi>
           t 
         </mi> 
         <mo>
           ) 
         </mo> 
        </mrow> 
       </mrow> 
       <mo>
         / 
       </mo> 
       <mrow> 
        <mtext>
          d 
        </mtext> 
        <mi>
          t 
        </mi> 
       </mrow> 
      </mrow> 
     </mrow> 
    </math>, and temperature 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mover accent="true"> 
       <mi>
         T 
       </mi> 
       <mo>
         ˜ 
       </mo> 
      </mover> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, are precisely obtained and computed in TMD, and physical quantities are numerically shown in <xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>. We will focus on the DM-EMI applications to TEG-Stirling engine in the following section.</p>
  </sec><sec id="s6">
   <title>6. The DM-EMI Applied to TEG-Stirling Engine</title>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The computer simulations for the existence of optimal angular velocities (rpm) at low temperature and low heat flows are shown, and the fact is the proof of possibility for a low temperature TEG-Stirling engine as one of the sustainable environmental technologies (SETs). The large parts of technical as well as theoretical discussions are found in papers <xref ref-type="bibr" rid="scirp.135246-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.135246-4">
     [4]
    </xref>. The NS-pair disk magnet electromagnetic induction in a general schematic image is shown in <xref ref-type="fig" rid="fig14">
     Figure 14
    </xref>, and properties of electric current and power produced by the axial flux generator (AFG) are shown by changing angular velocity, ω (rpm). The numerical simulations demonstrate the character of electric current and power. The numerical calculations with ω = 120 (rpm) and ω = 30 (rpm) are respectively compared. The axial magnetic flux of DM-EMI method produces pulse current (PC). The higher angular velocity driven by high temperature exhibits discrete properties of pulse electric current in very short ranges of time, whereas the lower angular velocities driven by a low temperature gradually demonstrate like a character of continuous electric currents. This also indicates one of the properties of AFG appropriate for a low temperature thermoelectric conversion.</p>
   <fig id="fig14" position="float">
    <label>Figure 14</label>
    <caption>
     <title>Figure 14. The image of NS-pair disk magnet electromagnetic induction.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId148.jpeg?20240815031849" />
   </fig>
   <p>A primitive experiment to show a pulse electric current is shown in <xref ref-type="fig" rid="fig15">
     Figure 15
    </xref>, ω~160 (rpm), which is compatible with TMD theoretical calculations. Note that the pulse current direction in <xref ref-type="fig" rid="fig15">
     Figure 15
    </xref> is from down-to-up, which comes from choosing the direction of right- or left-rotations of the flywheel.</p>
   <fig id="fig15" position="float">
    <label>Figure 15</label>
    <caption>
     <title>Figure 15. The primitive experiment (left) and pulse electric current (right).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="" />
   </fig>
   <fig id="fig15" position="float">
    <label>Figure 15</label>
    <caption>
     <title>Figure 15. The primitive experiment (left) and pulse electric current (right).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId149.jpeg?20240815031849" />
   </fig>
   <fig id="fig15" position="float">
    <label>Figure 15</label>
    <caption>
     <title>Figure 15. The primitive experiment (left) and pulse electric current (right).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId150.jpeg?20240815031850" />
   </fig>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The 4NS-pair disk-magnet rotor is composed of some pairs of N and S magnetic poles in a rotor, and numerical simulations produce an alternating pulse current as shown in <xref ref-type="fig" rid="fig16">
     Figure 16
    </xref> (ω = 120 rpm) and <xref ref-type="fig" rid="fig17">
     Figure 17
    </xref> (ω = 30 rpm).</p>
   <fig id="fig16" position="float">
    <label>Figure 16</label>
    <caption>
     <title>Figure 16. The produced pulse electric current, ω = 120 (rpm).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId151.jpeg?20240815031850" />
   </fig>
   <fig id="fig17" position="float">
    <label>Figure 17</label>
    <caption>
     <title>Figure 17. The produced pulse electric current: ω = 30 (rpm).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId152.jpeg?20240815031850" />
   </fig>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The N and S poles respectively induce a reversed pulse-current, examined by the theoretical analysis of electromagnetic induction. The direction of magnetic flux induced in the coils of the stators is completely opposite to the N and S poles, resulting in reversed pulse electric current. The current and voltage produced in a coil are inverse proportional against a produced electric energy in a time interval, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mrow> 
        <msub> 
         <mi>
           t 
         </mi> 
         <mn>
           0 
         </mn> 
        </msub> 
        <mo>
          , 
        </mo> 
        <msub> 
         <mi>
           t 
         </mi> 
         <mn>
           1 
         </mn> 
        </msub> 
       </mrow> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>. It is understood from the relation:</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
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        = 
      </mo> 
      <mstyle displaystyle="true"> 
       <mrow> 
        <msubsup> 
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           ∫ 
         </mo> 
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    </math> (8)</p>
   <p>where 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
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       </mi> 
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      </msub> 
     </mrow> 
    </math> is a finite amount of electric energy produced by a magnet and a coil in the mechanism of axial flux generation. The electric energy 
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    </math> is finite and a constant average value of the time interval 
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    </math>, which is the property of axial flux DM-EMI. It immediately indicates that 
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    </math> is large, and vice versa.</p>
   <p>The electric powers of ω = 120 (rpm) and ω = 30 (rpm) are specifically shown in <xref ref-type="fig" rid="fig18">
     Figure 18
    </xref> and <xref ref-type="fig" rid="fig19">
     Figure 19
    </xref>. The electric energy is shown by the area which is visible in <xref ref-type="fig" rid="fig19">
     Figure 19
    </xref>, but the time interval for 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
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    </math> becomes small in <xref ref-type="fig" rid="fig18">
     Figure 18
    </xref> (ω = 120 rpm). The time interval of <xref ref-type="fig" rid="fig19">
     Figure 19
    </xref> becomes larger than that of <xref ref-type="fig" rid="fig18">
     Figure 18
    </xref>, indicating that electric power can be better extracted in a technical sense in case of ω = 30 (rpm). The result is essential for electric-power conversions, meaning that the electric power may be better extracted from low temperature heat flows (ω ~ 30 rpm) by employing the axial flux generator.</p>
   <fig id="fig18" position="float">
    <label>Figure 18</label>
    <caption>
     <title>Figure 18. The produced pulse electric power: ω = 120 (rpm).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId167.jpeg?20240815031849" />
   </fig>
   <fig id="fig19" position="float">
    <label>Figure 19</label>
    <caption>
     <title>Figure 19. The produced pulse electric power: ω = 30 (rpm).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId168.jpeg?20240815031849" />
   </fig>
   <p>The important property of AFG concludes that an optimal angular velocity to produce electric power exists in a low angular velocity induced by a low temperature heat flow. This is one of the important results in the TMD analysis, which makes the extraction of electric power possible from 50˚C - 100˚C boiled water. That is the reason why the heat-electric power conversion device is proposed by the authors as a thermoelectric generation Stirling engine <xref ref-type="bibr" rid="scirp.135246-4">
     [4]
    </xref>-<xref ref-type="bibr" rid="scirp.135246-6">
     [6]
    </xref>. It is remarkable that an optimal thermoelectric generation device of a drinking bird is specifically constructed <xref ref-type="bibr" rid="scirp.135246-10">
     [10]
    </xref> only recently, as we discussed and expected theoretically <xref ref-type="bibr" rid="scirp.135246-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.135246-4">
     [4]
    </xref>. (<xref ref-type="fig" rid="fig20">
     Figure 20
    </xref>, <xref ref-type="fig" rid="fig21">
     Figure 21
    </xref>)</p>
   <fig id="fig20" position="float">
    <label>Figure 20</label>
    <caption>
     <title>Figure 20. Vertical-axis wind turbines.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="" />
   </fig>
   <fig id="fig20" position="float">
    <label>Figure 20</label>
    <caption>
     <title>Figure 20. Vertical-axis wind turbines.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId169.jpeg?20240815031849" />
   </fig>
   <fig id="fig20" position="float">
    <label>Figure 20</label>
    <caption>
     <title>Figure 20. Vertical-axis wind turbines.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId170.jpeg?20240815031850" />
   </fig>
   <fig id="fig21" position="float">
    <label>Figure 21</label>
    <caption>
     <title>Figure 21. A rotary engine.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1561545-rId171.jpeg?20240815031849" />
   </fig>
  </sec><sec id="s7">
   <title>7. Conclusions</title>
   <p>The huge power production and consumption of human societies and industries in the modern world have affected ecological systems on Earth, and it is imperative to develop clean energy and energy harvesting technologies. The DM-EMI technique proves that there exists an optimal speed of rotation (rpm) to extract electric power, even in a low temperature heat flow. The property of a low-(rpm) electric-power conversion and applications of the axial flux generator are one of the new findings and should be investigated further.</p>
   <p>The new types of heat-electricity conversion devices are possible but have not been constructed nor applied sufficiently. The applications to compensate electricity productions for macroscopic energy generators (MEGs), vertical-axis wind turbines (VAWTs), internal combustion engines, a low-temperature TEG-rotary engines, TEG-diesel engines with hydrogen-fuel could be theoretically possible. We are planning to develop optimal devices for electric energy production and seeking collaborations and an experimental budget to test several types of TEG engines.</p>
   <p>The method of TMD helped us integrate very sensitive physical problems of nonequilibrium irreversible thermodynamics with technologies for thermoelectric energy conversions and understand the time-progress of internal energy 
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    </math>, heat-flow or entropy-flow, 
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       </mo> 
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    </math> and nonequilibrium temperature 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
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    </math>, producing testable specific ideas for heat engines.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.135246-"></xref>The TMD analysis of heat engines suggests that energy can be more efficiently produced and used so that waste of energy should be dramatically decreased. The very high-temperature pressurized steam required in a traditional RFG is not necessary for AFG for thermoelectric energy conversions. The electricity should be directly used for sustainable social infrastructure, such as electrolysis to produce basic chemicals, such as H<sub>2</sub>, O<sub>2</sub>, C, COOH, CH<sub>3</sub>COOH, etc., which supports biological stability, symbiosis and ecology in nature, and sustainable environmental goals (SEGs) [11].</p>
  </sec><sec id="s8">
   <title>Acknowledgements</title>
   <p>The authors acknowledge that the research is supported by Japan Keirin Autorace (JKA) Foundation, Grant No. 2024M-423. The TMD and DM-EMI energy conversion research is partly supported by Kansai Research Foundation for Technology Promotion (KRF), Osaka, Japan.</p>
  </sec><sec id="s9">
   <title>NOTES</title>
   <p>*This is a review article of the presentation at 10th World Congress of Advanced Materials 2024, May 20-22; Osaka, Japan.</p>
  </sec>
 </body><back>
  <ref-list>
   <title>References</title>
   <ref id="scirp.135246-ref1">
    <label>1</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Uechi, S.T., Uechi, H. and Nishimura, A. (2019) The Analysis of Thermomechanical Periodic Motions of a Drinking Bird. World Journal of Engineering and Technology, 7, 559-571. &gt;https://doi.org/10.4236/wjet.2019.74040 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref2">
    <label>2</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Senft, J.R. (1996) An Introduction to Low Temperature Differential Stirling Engines. Moriya Press.
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref3">
    <label>3</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Uechi, H. and Uechi, S.T. (2020) Thermoelectric Energy Conversion of a Drinking Bird by Disk-Magnet Electromagnetic Induction. World Journal of Engineering and Technology, 8, 204-216. &gt;https://doi.org/10.4236/wjet.2020.82017 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref4">
    <label>4</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Uechi, H. and Uechi, S.T. (2022) The Disk-Magnet Electromagnetic Induction Applied to Thermoelectric Energy Conversions. World Journal of Engineering and Technology, 10, 179-193. &gt;https://doi.org/10.4236/wjet.2022.102010 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref5">
    <label>5</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Uechi, H., Uechi, L. and Uechi, S.T. (2021) Thermodynamic Consistency and Thermomechanical Dynamics (TMD) for Nonequilibrium Irreversible Mechanism of Heat Engines. Journal of Applied Mathematics and Physics, 9, 1364-1390. &gt;https://doi.org/10.4236/jamp.2021.96093 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref6">
    <label>6</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Uechi, H., Uechi, L. and Uechi, S.T. (2023) The Application of Thermomechanical Dynamics (TMD) to the Analysis of Nonequilibrium Irreversible Motion and a Low-Temperature Stirling Engine. Journal of Applied Mathematics and Physics, 11, 332-359. &gt;https://doi.org/10.4236/jamp.2023.111019 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref7">
    <label>7</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Zhang, D., Zheng, X. and Di Ventra, M. (2019) Local Temperatures Out of Equilibrium. Physics Reports, 830, 1-66. &gt;https://doi.org/10.1016/j.physrep.2019.10.003 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref8">
    <label>8</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Lieb, E.H. and Yngvason, J. (1999) The Physics and Mathematics of the Second Law of Thermodynamics. Physics Reports, 310, 1-96. &gt;https://doi.org/10.1016/s0370-1573(98)00082-9 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref9">
    <label>9</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Jiménez de Cisneros, B. and Hernández, A.C. (2008) Coupled Heat Devices in Linear Irreversible Thermodynamics. Physical Review E, 77, Article ID: 041127. &gt;https://doi.org/10.1103/physreve.77.041127
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref10">
    <label>10</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Wu, H., Zheng, H., Qin, X., Jin, Y., Li, Y., Yang, S., et al. (2024) Drinking-Bird-Enabled Triboelectric Hydrovoltaic Generator. Device, 2, Article 100318. &gt;https://doi.org/10.1016/j.device.2024.100318 
    </mixed-citation>
   </ref>
   <ref id="scirp.135246-ref11">
    <label>11</label>
    <mixed-citation publication-type="other" xlink:type="simple">
     Uechi, H., Uechi, L. and Uechi, S.T. (2021) The Lynx and Hare Data of 200 Years as the Nonlinear Conserving Interaction Based on Noether’s Conservation Laws and Stability. Journal of Applied Mathematics and Physics, 9, 2807-2847. &gt;https://doi.org/10.4236/jamp.2021.911181
    </mixed-citation>
   </ref>
  </ref-list>
 </back>
</article>