<?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">
    jamp
   </journal-id>
   <journal-title-group>
    <journal-title>
     Journal of Applied Mathematics and Physics
    </journal-title>
   </journal-title-group>
   <issn pub-type="epub">
    2327-4352
   </issn>
   <issn publication-format="print">
    2327-4379
   </issn>
   <publisher>
    <publisher-name>
     Scientific Research Publishing
    </publisher-name>
   </publisher>
  </journal-meta>
  <article-meta>
   <article-id pub-id-type="doi">
    10.4236/jamp.2024.127143
   </article-id>
   <article-id pub-id-type="publisher-id">
    jamp-134537
   </article-id>
   <article-categories>
    <subj-group subj-group-type="heading">
     <subject>
      Articles
     </subject>
    </subj-group>
    <subj-group subj-group-type="Discipline-v2">
     <subject>
      Physics 
     </subject>
     <subject>
       Mathematics
     </subject>
    </subj-group>
   </article-categories>
   <title-group>
    Thermoelectric Stirling Engine (TEG-Stirling Engine) Based on the Analysis of Thermomechanical Dynamics (TMD)
   </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>
     aNozuta, Machida-City, Tokyo, Japan
    </addr-line> 
   </aff> 
   <pub-date pub-type="epub">
    <day>
     12
    </day> 
    <month>
     07
    </month>
    <year>
     2024
    </year>
   </pub-date> 
   <volume>
    12
   </volume> 
   <issue>
    07
   </issue>
   <fpage>
    2386
   </fpage>
   <lpage>
    2399
   </lpage>
   <history>
    <date date-type="received">
     <day>
      25,
     </day>
     <month>
      May
     </month>
     <year>
      2024
     </year>
    </date>
    <date date-type="published">
     <day>
      13,
     </day>
     <month>
      May
     </month>
     <year>
      2024
     </year> 
    </date> 
    <date date-type="accepted">
     <day>
      13,
     </day>
     <month>
      July
     </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 thermoelectric energy conversion technique by employing the Disk-Magnet Electromagnetic Induction (DM-EMI) is examined in detail, and possible applications to heat engines as one of 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, such as a drinking bird and a low temperature Stirling engine, resulting in thermoelectric energy generation different from conventional heat engines. The current thermoelectric energy conversion with DM-EMI can be applied to wide ranges of machines and temperature differences. The mechanism of DM-EMI energy converter is categorized as the axial flux generator (AFG), which is the reason why the technology is applicable to sensitive thermoelectric conversions. On the other hand, almost all the conventional turbines use the radius flux generator to extract huge electric power, which uses the radial flux generator (RFG). The axial flux generator is helpful for a 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. The technique of DM-EMI will contribute to solving environmental problems to maintain clean and sustainable energy as one of the energy harvesting technologies.
   </abstract>
   <kwd-group> 
    <kwd>
     A Low Temperature Stirling Engine
    </kwd> 
    <kwd>
      Axial Flux Generator
    </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.134537-"></xref>Heat and energy are essential for the prosperity of human society and ecology on the Earth. This is the reason why human societies have 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 the enormous amount of abandoned waste heat and chemical substances. This has caused problems hindering sustainable developmental goals (SDGs).</p>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>On the contrary to MEGs, low temperature heat engines (a drinking bird <xref ref-type="bibr" rid="scirp.134537-1">
     [1]
    </xref> and low temperature Stirling engines <xref ref-type="bibr" rid="scirp.134537-2">
     [2]
    </xref>) are mechanical systems that can use very small amount of heat flows, and we proposed thermoelectric generators to convert the usable mechanical energy into electricity. 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.134537-3">
     [3]
    </xref>-<xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref>. It is possible to activate electric power from abandoned waste heat by the method of DM-EMI with the axial flux electromagnetic induction <xref ref-type="bibr" rid="scirp.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>.</p>
   <p>The traditional mechanoelectric 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. 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. 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.134537-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref>.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></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 a low rotational speed (about 30 - 60 rpm <xref ref-type="bibr" rid="scirp.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>). Therefore, a low temperature, thermoelectric generation Stirling engine (TEG-Stirling engine) can be constructed. In the current paper, 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>
   <p>The method of TMD is explained in Section 2 for self-contained discussion, and the equation of motion for the flywheel of Stirling engine is discussed in Section 3. The solution to the dissipative equation of motion of TEG-Stirling engine is discussed in Section 4. The DM-EMI with TEG-Stirling engine and the relation between electric current and power are explained in Section 5. Conclusion is in Section 6.</p>
  </sec><sec id="s2">
   <title>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>2. The Method of TMD</title>
   <p>The equation of motion and time-dependent physical quantities, such as internal energy 
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       </mo> 
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       </mi> 
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       </mo> 
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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.134537-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref>.</p>
   <p>The method of TMD requires three conditions.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></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.134537-"></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.134537-"></xref>2) The total energy-flow conservation law</p>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>The thermodynamic work 
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    </math>, are related to one another by the energy conservation law:</p>
   <p>
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   <p>Thermodynamic equilibrium is defined by 
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    </math>: no thermodynamic power exists in thermodynamic equilibrium.</p>
   <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>
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    </math>. (3)</p>
   <p>The value of 
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      </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> 
     </mrow> 
    </math>, (4)</p>
   <p>where T<sub>0</sub> 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.134537-7">
     [7]
    </xref>-<xref ref-type="bibr" rid="scirp.134537-9">
     [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="s3">
   <title>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>3. The Equation of Motion for a Stirling Engine</title>
   <p>A theoretical and schematic low temperature Stirling engine is shown in <xref ref-type="fig" rid="fig1">
     Figure 1
    </xref>, and the device consists of following functions:</p>
   <fig id="fig1" position="float">
    <label>Figure 1</label>
    <caption>
     <title>Figure 1. A theoretical and schematic structure of a low temperature Stirling engine <xref ref-type="bibr" rid="scirp.134537-6">
       [6]
      </xref>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1723752-rId44.jpeg?20240716025431" />
   </fig>
   <p>1) Heat source: A homogeneous heat flow from boiled water (40˚C - 100˚C) and geothermal heat, etc. The heat flow coming in 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="fig2">
     Figure 2
    </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 frictional and nonequilibrium thermal fluctuations, and c is a friction constant.</p>
   <fig id="fig2" position="float">
    <label>Figure 2</label>
    <caption>
     <title>Figure 2. 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><xref ref-type="bibr" rid="scirp.134537-#QUOTE"></xref>, starting from the vertical axis.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1723752-rId58.jpeg?20240716025441" />
   </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>
   <p>The jump discontinuities are not avoidable, and they naturally emerge from friction and viscosities of working fluid, sheer stress and machine structure, temperature and thermal fluctuations. 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 no longer determined by the derivative of 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>, though 
    <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 continuous and observable. In TMD, the concept of force is physical, and force only changes directions of motion or velocities of particles, but not associated with mass × acceleration. The angular acceleration is no longer meaningful, shown numerically in the next section.</p>
  </sec><sec id="s4">
   <title>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>4. The Solution to the Dissipative Equation of Motion of TEG-Stirling Engine</title>
   <p>We show 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="fig3">
     Figure 3
    </xref> and <xref ref-type="fig" rid="fig4">
     Figure 4
    </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 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> 
         <mtext>
           1 
         </mtext> 
         <mo>
           / 
         </mo> 
         <mtext>
           s 
         </mtext> 
        </mrow> 
       </mrow> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> for the current simulations.</p>
   <fig id="fig3" position="float">
    <label>Figure 3</label>
    <caption>
     <title>Figure 3. 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><xref ref-type="bibr" rid="scirp.134537-#QUOTE"></xref>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1723752-rId81.jpeg?20240716025522" />
   </fig>
   <fig id="fig4" position="float">
    <label>Figure 4</label>
    <caption>
     <title>Figure 4. The heat flow, <xref ref-type="bibr" rid="scirp.134537-#QUOTE">
       <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>
      </xref>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1723752-rId85.jpeg?20240716025511" />
   </fig>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>The dissipative equation of motion, 
    <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> and 
    <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> with 
    <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> 
      <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 arbitrary 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.134537-"></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="fig5">
     Figure 5
    </xref> and <xref ref-type="fig" rid="fig6">
     Figure 6
    </xref>. One can check that the trajectory of motion, 
    <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>, changes continuously. Thermal force or pressure exerted by heat flows from a cold plate to a hot plate accelerates the angular velocity of rotations in the beginning, but mechanical motions reach a plateau, a relatively stable level of the angular velocity, as shown in <xref ref-type="fig" rid="fig6">
     Figure 6
    </xref>. The maximum angular velocity seems stable and constant, but one can notice that the angular velocity in <xref ref-type="fig" rid="fig6">
     Figure 6
    </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="fig5" position="float">
    <label>Figure 5</label>
    <caption>
     <title>Figure 5. 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><xref ref-type="bibr" rid="scirp.134537-#QUOTE"></xref>, 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/1723752-rId119.jpeg?20240716025511" />
   </fig>
   <fig id="fig6" position="float">
    <label>Figure 6</label>
    <caption>
     <title>Figure 6. 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><xref ref-type="bibr" rid="scirp.134537-#QUOTE"></xref> (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/1723752-rId123.jpeg?20240716025522" />
   </fig>
   <p>The TMD thermomechanical approach to physical phenomena demands fundamental changes regarding the concept of thermodynamic force and 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>. Mechanical work is based on continuity and differentiability of motion, which is integrated in changes of velocity and trajectory of particles. In other words, it is essential to recognize that modifications of mechanical motion caused by friction, wear, deformation and thermal fluctuations generate the fundamental change to the concept of differentiability of physically observable quantities.</p>
   <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="fig7">
     Figure 7
    </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 in a long period of time. Numerical calculations and self-consistency relations are discussed in detail in <xref ref-type="bibr" rid="scirp.134537-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref>.</p>
   <fig id="fig7" position="float">
    <label>Figure 7</label>
    <caption>
     <title>Figure 7. 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><xref ref-type="bibr" rid="scirp.134537-#QUOTE"></xref> (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/1723752-rId135.jpeg?20240716025522" />
   </fig>
   <p>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="fig8">
     Figure 8
    </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.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>.</p>
   <fig id="fig8" position="float">
    <label>Figure 8</label>
    <caption>
     <title>Figure 8. Thermodynamic 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>
  
        <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/1723752-rId142.jpeg?20240716025522" />
   </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.134537-6">
     [6]
    </xref>. We will focus on the technological method DM-EMI (disk-magnet electromagnetic induction) and its applications to TEG-Stirling engine in the following section. The detailed explanations and proposed devices are discussed in detail in the papers <xref ref-type="bibr" rid="scirp.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>.</p>
  </sec><sec id="s5">
   <title>5. The DM-EMI Applied to TEG-Stirling Engine</title>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></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.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>. The NS-pair disk magnet electromagnetic induction in a general schematic image is shown in <xref ref-type="fig" rid="fig9">
     Figure 9
    </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 calculations with ω = 120 (rpm) and ω = 30 (rpm) are respectively compared, which demonstrates the character of electric current and power. 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 a 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="fig9" position="float">
    <label>Figure 9</label>
    <caption>
     <title>Figure 9. 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/1723752-rId152.jpeg?20240716025602" />
   </fig>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>A primitive experiment to show a pulse electric current is shown in <xref ref-type="fig" rid="fig10">
     Figure 10
    </xref>, ω~160 (rpm), which agrees with TMD theoretical calculations. Note that the pulse current direction in <xref ref-type="fig" rid="fig10">
     Figure 10
    </xref> is from down-to-up, which comes from choosing the direction of right- or left-rotations of the flywheel. The 4NS-pair disk-magnet rotor is composed of the pair 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="fig11">
     Figure 11
    </xref> (ω = 120 rpm) and <xref ref-type="fig" rid="fig12">
     Figure 12
    </xref> (ω = 30 rpm).</p>
   <fig id="fig10" position="float">
    <label>Figure 10</label>
    <caption>
     <title>Figure 10. The primitive experiment (left) and pulse electric current (right).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="" />
   </fig>
   <fig id="fig10" position="float">
    <label>Figure 10</label>
    <caption>
     <title>Figure 10. 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/1723752-rId153.jpeg?20240716025602" />
   </fig>
   <fig id="fig10" position="float">
    <label>Figure 10</label>
    <caption>
     <title>Figure 10. 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/1723752-rId154.jpeg?20240716025602" />
   </fig>
   <fig id="fig11" position="float">
    <label>Figure 11</label>
    <caption>
     <title>Figure 11. 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/1723752-rId155.jpeg?20240716025602" />
   </fig>
   <fig id="fig12" position="float">
    <label>Figure 12</label>
    <caption>
     <title>Figure 12. 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/1723752-rId156.jpeg?20240716025602" />
   </fig>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></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>
         E 
       </mi> 
       <mi>
         e 
       </mi> 
      </msub> 
      <mo>
        = 
      </mo> 
      <mstyle displaystyle="true"> 
       <mrow> 
        <msubsup> 
         <mo>
           ∫ 
         </mo> 
         <mrow> 
          <msub> 
           <mi>
             t 
           </mi> 
           <mn>
             0 
           </mn> 
          </msub> 
         </mrow> 
         <mrow> 
          <msub> 
           <mi>
             t 
           </mi> 
           <mn>
             1 
           </mn> 
          </msub> 
         </mrow> 
        </msubsup> 
        <mrow> 
         <mi>
           V 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mi>
            t 
          </mi> 
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            ) 
          </mo> 
         </mrow> 
         <mi>
           I 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
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            t 
          </mi> 
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            ) 
          </mo> 
         </mrow> 
         <mtext>
           d 
         </mtext> 
         <mi>
           t 
         </mi> 
        </mrow> 
       </mrow> 
      </mstyle> 
     </mrow> 
    </math>, (8)</p>
   <p>where 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         E 
       </mi> 
       <mi>
         e 
       </mi> 
      </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 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         E 
       </mi> 
       <mi>
         e 
       </mi> 
      </msub> 
     </mrow> 
    </math> is finite and a constant average value of the time interval 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mo>
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       </mo> 
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          , 
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           1 
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       </mrow> 
       <mo>
         ) 
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      </mrow> 
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    </math>, which is the property of axial flux DM-EMI. It immediately indicates that 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        I 
      </mi> 
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    </math> becomes small when 
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      </mrow> 
     </mrow> 
    </math> is large, and vice versa.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>The electric powers of ω = 120 (rpm) and ω = 30 (rpm) are specifically shown in <xref ref-type="fig" rid="fig13">
     Figure 13
    </xref> and <xref ref-type="fig" rid="fig14">
     Figure 14
    </xref>. The electric energy is shown by the area which is visible in <xref ref-type="fig" rid="fig14">
     Figure 14
    </xref>, but the time interval for 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        I 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mi>
         t 
       </mi> 
       <mo>
         ) 
       </mo> 
      </mrow> 
      <mtext>
        d 
      </mtext> 
      <mi>
        t 
      </mi> 
     </mrow> 
    </math> becomes small in <xref ref-type="fig" rid="fig13">
     Figure 13
    </xref> (ω = 120 rpm). The time interval of <xref ref-type="fig" rid="fig14">
     Figure 14
    </xref> becomes larger than that of <xref ref-type="fig" rid="fig13">
     Figure 13
    </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 (AFG). The results are important for technical applications indicating that a high-speed rotation and special microscopic semiconductors are not necessarily required for extracting usable electricity, though high-speed turbines and semiconductor energy-production devices are surely important as societal infrastructures. The sensitive electric energy extractions using AF-EMI would compensate conventional power-extraction systems. We are currently investigating and proposing new electric power generators based on AF-EMI and hope that other researchers find possible applications with AF-EMI technique.</p>
   <fig id="fig13" position="float">
    <label>Figure 13</label>
    <caption>
     <title>Figure 13. 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/1723752-rId173.jpeg?20240716025532" />
   </fig>
   <fig id="fig14" position="float">
    <label>Figure 14</label>
    <caption>
     <title>Figure 14. 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/1723752-rId174.jpeg?20240716025542" />
   </fig>
   <p>The important property of the 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, which 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.134537-4">
     [4]
    </xref>-<xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref>. It is remarkable that an optimal thermoelectric generation device of a drinking bird is specifically constructed [10] only recently, as we discussed and expected theoretically <xref ref-type="bibr" rid="scirp.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>.</p>
  </sec><sec id="s6">
   <title>6. Conclusions</title>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></xref>The huge power production and consumption of human societies and industries in 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. The DM-EMI technique is for activation of dissipated or discarded waste heat and should not be misunderstood as devices with heavy-duty front-line turbine generators. The results shown in the numerical simulations of DM-EMI technique improve overall thermal efficiency and electric power conversions of thermodynamic cycles. The detailed description of DM-EMI mechanism, including the design and operation of axial flux generators (AFG) and their role in sensitive thermoelectric conversions are shown in the papers <xref ref-type="bibr" rid="scirp.134537-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.134537-4">
     [4]
    </xref>, and the theoretical foundations of TMD and nonequilibrium irreversible thermodynamics are discussed in <xref ref-type="bibr" rid="scirp.134537-5">
     [5]
    </xref> <xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref> in detail.</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), internal combustion engines, a low-temperature TEG-rotary engine, TEG-diesel engines with hydrogen-fuel could be theoretically possible. We are planning to develop optimal devices for electric energy productions and seeking collaborations and an experimental budget to test several types of TEG engines.</p>
   <p>The equations of motion for a low temperature Stirling engine and a drinking bird are solved self-consistently <xref ref-type="bibr" rid="scirp.134537-3">
     [3]
    </xref>-<xref ref-type="bibr" rid="scirp.134537-6">
     [6]
    </xref>. The method of TMD made us integrate very sensitive physical problems of nonequilibrium irreversible thermodynamics with technologies for thermoelectric energy conversions. It helped us understand nonequilibrium irreversible states (NISs) with the time-progress of internal energy 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
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      </mtext> 
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         ( 
       </mo> 
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         t 
       </mi> 
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         ) 
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      </mrow> 
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    </math> and work 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
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        d 
      </mtext> 
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       <mi>
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         ( 
       </mo> 
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         t 
       </mi> 
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         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math>, heat-flow or entropy-flow, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mi>
        T 
      </mi> 
      <mrow> 
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      </mi> 
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         ( 
       </mo> 
       <mi>
         t 
       </mi> 
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         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> and nonequilibrium 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> 
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         t 
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      </mo> 
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        T 
      </mi> 
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      </mi> 
      <mrow> 
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         ( 
       </mo> 
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      </mrow> 
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    </math>, producing testable specific ideas for heat engines.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.134537-"></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 in 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, sustainable environmental goals (SEGs) [11].</p>
  </sec><sec id="s7">
   <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>
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