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Efficiency at the maximum power output for simple two-level heat engine Sang Hoon Lee School of Physics, Korea Institute for Advanced Study http://newton.kias.re.kr/~lshlj82 in collaboration with Jaegon Um (CCSS, CTP and Department of Physics and Astronomy, SNU) and Hyunggyu Park (School of Physics & Quantum Universe Center, KIAS) 2016 Workshop on Special Topics in Statistical Physics & Complex Systems (SPnCS) @ Chosun Univ., Gwangju, 22 December, 2016. SHL, J. Um, and H. Park, e-print arXiv:1612.00518.
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Efficiency at the maximum power output for simple two-level heat engine

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  • Efficiency at the maximum power output for simple two-level heat engine

    Sang Hoon Lee School of Physics, Korea Institute for Advanced Study

    http://newton.kias.re.kr/~lshlj82

    in collaboration with Jaegon Um (CCSS, CTP and Department of Physics and Astronomy, SNU) and Hyunggyu Park (School of Physics & Quantum Universe Center, KIAS)

    2016 Workshop on Special Topics in Statistical Physics & Complex Systems (SPnCS) @ Chosun Univ., Gwangju, 22 December, 2016.

    SHL, J. Um, and H. Park, e-print arXiv:1612.00518.

  • Carnot engine

    source: http://web2.uwindsor.ca/courses/physics/high_schools/2013/SteamEngine/images/PVgraph.jpg

    S. Carnot, Rflexions Sur La Puissance Motrice Du Feu Et Sur Les Machines Propres Dvelopper Cette Puissance (Bachelier Libraire, Paris, 1824).

    the

    Sadi Carnot (1796-1832)

    http://web2.uwindsor.ca/courses/physics/high_schools/2013/SteamEngine/images/PVgraph.jpg

  • Carnot engine

    source: http://web2.uwindsor.ca/courses/physics/high_schools/2013/SteamEngine/images/PVgraph.jpg

    S. Carnot, Rflexions Sur La Puissance Motrice Du Feu Et Sur Les Machines Propres Dvelopper Cette Puissance (Bachelier Libraire, Paris, 1824).

    the

    Sadi Carnot (1796-1832)

    the Carnot eciency C =Weng|Qh|

    =

    |Qh| |Qc||Qh|

    = 1 TcTh

    quasi-static(the 1st law of thermodynamics)

    http://web2.uwindsor.ca/courses/physics/high_schools/2013/SteamEngine/images/PVgraph.jpg

  • the Carnot eciency C =Weng|Qh|

    =

    |Qh| |Qc||Qh|

    = 1 TcTh

    quasi-static(the 1st law of thermodynamics)

  • the Carnot eciency C =Weng|Qh|

    =

    |Qh| |Qc||Qh|

    = 1 TcTh

    quasi-static(the 1st law of thermodynamics)

    0: cyclic process

    the 2nd law of thermodynamics: Stot

    = Seng

    +Sres

    = QhTh

    +

    QcTc 0

    (per cycle)

    ! |Qc||Qh| Tc

    Th! = 1 |Qc||Qh|

    1 TcTh

    = C

    ) C in general, and C is the theoretically maximum eciency.

    quasi-static

  • the Carnot eciency C =Weng|Qh|

    =

    |Qh| |Qc||Qh|

    = 1 TcTh

    quasi-static(the 1st law of thermodynamics)

    0: cyclic process

    the 2nd law of thermodynamics: Stot

    = Seng

    +Sres

    = QhTh

    +

    QcTc 0

    (per cycle)

    ! |Qc||Qh| Tc

    Th! = 1 |Qc||Qh|

    1 TcTh

    = C

    ) C in general, and C is the theoretically maximum eciency.

    Weng reaches the maximum value for given |Qh| in the Carnot engine,but the power P = Weng/ ! 0 where is the operating time !1

    quasi-static

  • Th

    Tc

    hot reservoir

    cold reservoir

    Thw

    Tcw

    Endoreversible engine P. Chambadal, Les Centrales Nuclaires (Armand Colin, Paris, 1957). I. I. Novikov, Efficiency of an atomic power generating installation, At. Energy 3, 1269 (1957);

    The efficiency of atomic power stations, J. Nucl. Energy 7, 125 (1958). F. L. Curzon and B. Ahlborn, Efficiency of a Carnot engine at maximum power output, Am. J. Phys. 43, 22 (1975).

  • endoreversibility

    Th

    Tc

    hot reservoir

    cold reservoir

    Thw

    Tcw

    during t1

    irreversible heat conduction

    the input energy (linear heat conduction) Qh = t1(Th Thw)

    the reversible engine

    operated at Thw and Tcw!QhThw

    =QcTcw

    during t2

    irreversible heat conduction

    the heat rejected (linear heat conduction) Qc = t2(Tcw Tc)

    Endoreversible engine P. Chambadal, Les Centrales Nuclaires (Armand Colin, Paris, 1957). I. I. Novikov, Efficiency of an atomic power generating installation, At. Energy 3, 1269 (1957);

    The efficiency of atomic power stations, J. Nucl. Energy 7, 125 (1958). F. L. Curzon and B. Ahlborn, Efficiency of a Carnot engine at maximum power output, Am. J. Phys. 43, 22 (1975).

  • endoreversibility

    the (Chambadal-Novikov-)Curzon-Ahlborn eciency CA = 1r

    TcTh

    Th

    Tc

    hot reservoir

    cold reservoir

    Thw

    Tcw

    during t1

    irreversible heat conduction

    the input energy (linear heat conduction) Qh = t1(Th Thw)

    the reversible engine

    operated at Thw and Tcw!QhThw

    =QcTcw

    during t2

    irreversible heat conduction

    the heat rejected (linear heat conduction) Qc = t2(Tcw Tc)

    maximizing power P =Qh Qct1 + t2

    with respect to t1 and t2

    Endoreversible engine P. Chambadal, Les Centrales Nuclaires (Armand Colin, Paris, 1957). I. I. Novikov, Efficiency of an atomic power generating installation, At. Energy 3, 1269 (1957);

    The efficiency of atomic power stations, J. Nucl. Energy 7, 125 (1958). F. L. Curzon and B. Ahlborn, Efficiency of a Carnot engine at maximum power output, Am. J. Phys. 43, 22 (1975).3/31/16, 12:03Endoreversible thermodynamics - Wikipedia, the free encyclopedia

    Page 2 of 3https://en.wikipedia.org/wiki/Endoreversible_thermodynamics

    Power Plant (C) (C) (Carnot) (Endoreversible) (Observed)West Thurrock (UK) coal-fired power

    plant 25 565 0.64 0.40 0.36

    CANDU (Canada) nuclear power plant 25 300 0.48 0.28 0.30Larderello (Italy) geothermal power

    plant 80 250 0.33 0.178 0.16

    As shown, the endoreversible efficiency much more closely models the observed data. However, such anengine violates Carnot's principle which states that work can be done any time there is a difference intemperature. The fact that the hot and cold reservoirs are not at the same temperature as the working fluidthey are in contact with means that work can and is done at the hot and cold reservoirs. The result istantamount to coupling the high and low temperature parts of the cycle, so that the cycle collapses.[7] In theCarnot cycle there is strict necessity that the working fluid be at the same temperatures as the heat reservoirsthey are in contact with and that they are separated by adiabatic transformations which prevent thermalcontact. The efficiency was first derived by William Thomson [8] in his study of an unevenly heated body inwhich the adiabatic partitions between bodies at different temperatures are removed and maximum work isperformed. It is well known that the final temperature is the geometric mean temperature so that

    the efficiency is the Carnot efficiency for an engine working between and .

    Due to occasional confusion about the origins of the above equation, it is sometimes named theChambadal-Novikov-Curzon-Ahlborn efficiency.

    See alsoHeat engine

    An introduction to endoreversible thermodynamics is given in the thesis by Katharina Wagner.[4] It is alsointroduced by Hoffman et al.[9][10] A thorough discussion of the concept, together with many applications inengineering, is given in the book by Hans Ulrich Fuchs.[11]

    References1. I. I. Novikov. The Efficiency of Atomic Power Stations. Journal Nuclear Energy II, 7:125128, 1958. translated from

    Atomnaya Energiya, 3 (1957), 409.2. Chambadal P (1957) Les centrales nuclaires. Armand Colin, Paris, France, 4 1-583. F.L. Curzon and B. Ahlborn, American Journal of Physics, vol. 43, pp. 2224 (1975)4. M.Sc. Katharina Wagner, A graphic based interface to Endoreversible Thermodynamics, TU Chemnitz, Fakultt fr

    Naturwissenschaften, Masterarbeit (in English). http://archiv.tu-chemnitz.de/pub/2008/0123/index.html5. A Bejan, J. Appl. Phys., vol. 79, pp. 11911218, 1 Feb. 1996 http://dx.doi.org/10.1016/S0035-3159(96)80059-66. Callen, Herbert B. (1985). Thermodynamics and an Introduction to Thermostatistics (2nd ed. ed.). John Wiley &

    Sons, Inc.. ISBN 0-471-86256-8.7. B. H. Lavenda, Am. J. Phys., vol. 75, pp. 169-175 (2007)8. W. Thomson, Phil. Mag. (Feb. 1853)

  • the (Chambadal-Novikov-)Curzon-Ahlborn eciency CA = 1r

    TcTh

  • the (Chambadal-Novikov-)Curzon-Ahlborn eciency CA = 1r

    TcTh

    Q. Is this a universal formula for power-maximizing efficiency, or does endoreversibility guarantee it?

  • the (Chambadal-Novikov-)Curzon-Ahlborn eciency CA = 1r

    TcTh

    Q. Is this a universal formula for power-maximizing efficiency, or does endoreversibility guarantee it?

    A. No. The linear heat conduction is essential.

    Q = (Th Tc)

    We introduce a different type of engine with non-(CN)CA optimal efficiency.

    L. Chen and Z. Yan, J. Chem. Phys. 90, 3740 (1988): F. Angulo-Brown and R. Pez-Hernndez, J. Appl. Phys. 74, 2216 (1993):

    (Dulong-Petit law of cooling)Q = (Th Tc)n

    Q = (Tnh Tnc )

  • our simple two-level heat engine model

    R1

    R2

    relaxation with

    relaxation with

    Q1

    Q2

    E1

    E2

    T1

    T2

    q

    t1

    t2

    during t1

    during t2

    W = E1 E2W 0 = E1 E2

    q/(1 q) = exp(E1/T1)

    /(1 ) = exp(E2/T2)

    0

    E1

    q(setting the Boltzmann constant

    kB 1 for notational convenience)

  • our simple two-level heat engine model

    R1

    R2

    relaxation with

    relaxation with

    Q1

    Q2

    E1

    E2

    T1

    T2

    q

    t1

    t2

    during t1

    during t2

    W = E1 E2W 0 = E1 E2

    q/(1 q) = exp(E1/T1)

    /(1 ) = exp(E2/T2)

    0

    E2

    (setting the Boltzmann constant

    kB 1 for notational convenience)

  • our simple two-level heat engine model

    R1

    R2

    relaxation with

    relaxation with

    Q1

    Q2

    E1

    E2

    T1

    T2

    q

    t1

    t2

    during t1

    during t2

    W = E1 E2W 0 = E1 E2

    q/(1 q) = exp(E1/T1)

    /(1 ) = exp(E2/T2)

    0

    E2

    (setting the Boltzmann constant

    kB 1 for notational convenience)

  • our simple two-level heat engine model

    R1

    R2

    relaxation with

    relaxation with

    Q1

    Q2

    E1

    E2

    T1

    T2

    q

    t1

    t2

    during t1

    during t2

    W = E1 E2W 0 = E1 E2

    q/(1 q) = exp(E1/T1)

    /(1 ) = exp(E2/T2)

    0

    q

    E1

    (setting the Boltzmann constant

    kB 1 for notational convenience)

  • our simple two-level heat engine model

    R1

    R2

    relaxation with

    relaxation with

    Q1

    Q2

    E1

    E2

    T1

    T2

    q

    t1

    t2

    during t1

    during t2

    W = E1 E2W 0 = E1 E2

    q/(1 q) = exp(E1/T1)

    /(1 ) = exp(E2/T2)

    0

    q

    E1

    (setting the Boltzmann constant

    kB 1 for notational convenience)

  • our simple two-level heat engine model

    R1

    E1T1

    q

    R2

    E2

    T2

    0

    q

    0

    during duringstochastic Markov processes

    1 2

    |P1i(t1 = 0) |P1i(t1 = 1) = |P2i(t2 = 0) |P2i(t2 = 2)

    |P2i(t2 = 2) = |P1i(t1 = 0)

    W = E1 E2

    W 0 = E1 E2

    Q1 Q2

    hWnetiT1

    sh =T2T1

    sc +hWnetiT1

    sh =E1T1

    scG1 (sc)

    sc

    sh

  • hW i = (E1 E2)P1 and hW 0i = (E1 E2)P2where P1 (P2) is the population in E1 (E2) at R1 (R2), respectively

    independent of t1

    and t2

    (no P1

    and P2

    dependency)

    and ! Carnot

    = 1 T2

    /T1

    when ' q

    total entropy change S = Q1T1

    +

    Q2T2

    hQ1i = (P1 P2)T1 ln[(1 q)/q], hQ2i = (P1 P2)T2 ln[(1 )/]

    hWneti = hW i hW 0i = (P1 P2)(E1 E2)= (P1 P2){T1 ln[(1 q)/q] T2 ln[(1 )/]}

    eciency =hWnetihQ1i

    =hW i hW 0i

    hQ1i= 1 T2

    T1

    ln[(1 )/]ln[(1 q)/q]

    0

    = (P1 P2)E1 = (P1 P2)E2(from the Schnakenberg entropy formula, or equivalently, the 1st law:

    hEi = hQi hW i for each half of the cycle)

  • hWneti = hW i hW 0i = (P1 P2)(E1 E2)= (P1 P2){T1 ln[(1 q)/q] T2 ln[(1 )/]}

    eciency =hWnetihQ1i

    =hW i hW 0i

    hQ1i= 1 T2

    T1

    ln[(1 )/]ln[(1 q)/q]

    P1(t1 !1, t2 !1) = q and P2(t1 !1, t2 !1) = , as expected

    meaningful only for q > , or hWneti > 0P1 = (1 q)P1 + q(1 P1)P2 = (1 )P2 + (1 P2)

    ! P1 = q A1et01 , P2 = A2et

    02

    (0 t01 t1 and 0 t02 t2)P1(t

    01 = 0, t2) = P2(t1, t2) and P2(t1, t

    02 = 0) = P1(t1, t2)

    ! A1 = q P2, A2 = P1 and let t01 = t1, t02 = t2

    ! P1 =q(1 et1) + (1 et2)et1

    1 e(t1+t2)

    P2 =(1 et2) + q(1 et1)et2

    1 e(t1+t2)

  • Let t1 = t2 = /2, then

    in terms of , the maximum power is achieved for ! 0, asPower ! hWneti/4 and the power is monotonically decreased as is increased.

    hWneti = (q )(1 e/2)2

    1 e

    {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    time: decoupled overall factor

    hWneti( !1) = (q ) {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    Power hP i = hWneti

    =

    q

    (1 e/2)2

    1 e

    {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    (still decoupled even when t1 6= t2)

  • Let t1 = t2 = /2, then

    in terms of , the maximum power is achieved for ! 0, asPower ! hWneti/4 and the power is monotonically decreased as is increased.

    hWneti = (q )(1 e/2)2

    1 e

    {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    time: decoupled overall factor

    hWneti( !1) = (q ) {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    Power hP i = hWneti

    =

    q

    (1 e/2)2

    1 e

    {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    our goal: to find (q, ) = (q, ) maximizing hP i@hP i@q

    q=q,=

    =@hP i@

    q=q,=

    = 0

    (still decoupled even when t1 6= t2)

    hWneti = hW i hW 0i = (P1 P2)(E1 E2)= (P1 P2){T1 ln[(1 q)/q] T2 ln[(1 )/]}

    eciency =hWnetihQ1i

    =hW i hW 0i

    hQ1i= 1 T2

    T1

    ln[(1 )/]ln[(1 q)/q]

    substitute (q, ) = (q, ) here,then

    op

    (q, ) is the eciencyat the maximum power output

  • ! T2q(1 q)

    T1(1 )= 1

    at (q, ) (global optimum)

    3

    equation system for given q and values,

    dP1

    dt

    = (1 q)P1 + q(1 P1) ,dP2

    dt

    = (1 )P2 + (1 P2) .(7)

    With the circular boundary condition P1(t01 = 0, t02 = t2) =

    P2(t01 = t1, t02 = t2) and P2(t

    01 = t1, t

    02 = 0) = P1(t

    01 = t1, t

    02 =

    t2) where the primed variables describe intermediate time, thesolution at t01 = t1 and t

    02 = t2 is

    P1 =q(1 et1 ) + (1 et2 )et1

    1 e(t1+t2) ,

    P2 =(1 et2 ) + q(1 et1 )et2

    1 e(t1+t2) ,(8)

    and limt1,t2!1 P1 = q and limt1,t2!1 P2 = as expected.

    Let t1 = t2 = /2 (each reservoir contacts with the systemduring the equal time), then

    hWneti = (q )(1 e/2)2

    1 e"T1 ln

    1 q

    q

    ! T2 ln

    1

    !#,

    (9)so the monotonically increasing factor (1 e/2)2/(1 e)for the time scale is decoupled from the rest of the formulaand only plays the role of overall factor. The amount of network is increased up to

    lim!1hWneti = (q )

    "T1 ln

    1 q

    q

    ! T2 ln

    1

    !#. (10)

    The average power output hPi, which is the amount of network per unit time, is given by

    hPi = (q )(1 e/2)2

    (1 e)"T1 ln

    1 q

    q

    ! T2 ln

    1

    !#.

    (11)In terms of , the maximum power is achieved forlim!0hPi = hWneti/4 and the power is monotonically de-creased as is increased. Therefore, from now on, we discard

    the time dependence altogether and focus on other parame-ters, i.e., denoting hWneti = hPi without considering the over-all factor involving for notational convenience. Numerically,we obtain the net work and eciency for (q, ) combination,as shown in Fig. 2. In Sec. III B, we derive the condition forthe eciency at the maximum power output.

    B. Eciency at the maximum power output

    1. The condition for the maximum power output

    For a given T2/T1 value, the maximum power output con-dition for the two-variable function is

    @hPi@q

    q=q,=

    =@hPi@

    q=q,=

    = 0 , (12)

    which leads to

    1 T2T1

    ln[(1 )/]ln[(1 q)/q] =

    q

    q

    (1 q) ln[(1 q)/q] , (13a)

    and

    1 T2T1

    ln[(1 )/]ln[(1 q)/q] =

    (T2/T1)(q )(1 ) ln[(1 q)/q] , (13b)

    from Eq. (11). By eliminating the left-hand side of Eqs. (13a)and (13b), we obtain the following simple relation

    T2q(1 q)

    T1(1 ) = 1 , (14a)

    or

    =12

    2666641

    r1 4T2

    T1q

    (1 q)377775 , (14b)

    because 0 < < q < 1/2. By substituting as a function ofq

    in Eq. (14b) to Eq. (13a) or Eq. (13b), we get the optimumcondition f (T2/T1, q) = 0, which is explicitly

    f (T2/T1, q) = ln

    1 qq

    ! T2

    T1ln

    26666666666666664

    1 +r

    1 4T2T1

    q

    (1 q)

    1 r

    1 4T2T1

    q

    (1 q)

    37777777777777775

    q

    12+

    12

    r1 4T2

    T1q

    (1 q)q

    (1 q)

    = ln

    1 qq

    ! (1

    C

    ) ln

    266666666664

    1 +q

    (1 2q)2 + 4C

    q

    (1 q)1

    q(1 2q)2 + 4

    C

    q

    (1 q)

    377777777775

    q

    12+

    12

    q(1 2q)2 + 4

    C

    q

    (1 q)q

    (1 q) = 0 .

    (15)

    Furthermore, the condition in Eq. (15) leads to the followingform of op from Eq. (6),

    op =q

    12+

    12

    r1 4T2

    T1q

    (1 q)q

    (1 q) ln[(1 q)/q] (16a)

    or in terms of C

    = 1 T2/T1,

    op =q

    12+

    12

    q(1 2q)2 + 4

    C

    q

    (1 q)q

    (1 q) ln[(1 q)/q] . (16b)

  • 4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    quadratic form

    FIG. 3. Numerically found q and values satisfying Eq. (15), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The quadratic form indicates Eq. (19).

    We verify that the (q, ) is indeed the maximum point byusing the relations of second derivatives

    0BBBBB@@2hPi@q2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@q@

    q=q,=

    1CCCCCA

    2

    =

    T

    21(1 )q

    (1 q) (2q q )2 4T 21 2(1 )2

    2(1 )2q2(1 q)2

    = T1(q )2

    (1 )q3(1 q)3 > 0 ,(17)

    where we use the relation in Eq. (14a), and

    @2hPi@q2

    q=q,=

    = T1[q + (1 2q)]q

    2(1 q)2 < 0 ,

    @2hPi@2

    q=q,=

    = T2[q + (1 2q)]2(1 )2 < 0 .

    (18)

    Therefore, the procedure to calculate the eciency forgiven T2/T1 at the maximum power output seems straight-forward now. First, find the q value satisfying Eq. (15) andsubstitute the q value to Eq. (16a). The only (but very crucial)problem is that f (T2/T1, q) = 0 is a transcendental equationwhose closed-form solution is unattainable.

    2. Asymptotic behaviors for extreme cases

    The upper bound for q is given by the condition T2/T1 = 0,satisfying ln[(1 q)/q] = 1/(1 q) and q(T2/T1 = 0) '0.217 811 705 719 800 found numerically and (T2/T1 =0) = 0 exactly from Eq. (14b). T2/T1 = 1 always satisfiesf (T2/T1, q) = 0 regardless of q values, but the T2/T1 ' 1asymptotic case yields the lower bound for q(T2/T1 ' 1) =(T2/T1 ' 1) ' 0.083 221 720 199 517 7 found numerically.

    schematically . . .

    q

    = q

    no net work

    q(T2/T1 1) 0.0832217201995177= (T2/T1 1)

    q(T2/T1 = 0) 0.217811705719800(T2/T1 = 0) = 0

    as T2/T1 (C) is decreased (increased),respectively

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    0

    0.2

    0.4

    0.6

    0.8

    1

    0 0.2 0.4 0.6 0.8 1

    op

    c = 1 T2 / T1

    at (q*, *)CA = 11c

    c/(2c)c/2

    FIG. 5. The eciency at the maximum power op as the functionof the Carnot eciency

    C

    in Eq. (16b) using numerically found op-timal q values, along with various asymptotic cases: the Curzon-Ahlborn eciency CA in Eq. (21), the upper bound C/(2 C) andthe lower bound

    C

    /2 in Ref. [19].

    Figure 3 shows the numerical solution (q, ) as a functionof

    C

    = 1 T2/T1, where the asymptotic behaviors derivedabove hold when T2/T1 ' 0 and T2/T1 ' 1. It seems thatq

    is monotonically decreased and is monotonically in-creased, as T2/T1 is increased, i.e., qmin = q

    (T2/T1 ' 1),q

    max = q

    (T2/T1 = 0), min = 0, and max =

    (T2/T1 ' 1).Figure 4 illustrates the situation on the (q, ) plane. We numer-ically obtain the quadratic function q(

    C

    ) = qmin + aC + b2C

    by fitting it to the numerical solution near C

    = 0, in the range

    C

    2 [0, 0.05] in this case, which isq

    (C

    ) ' qmin + 0.0457524C + 0.02767322C . (19)To proceed further, we have to take into account that q

    is also a function of C

    . Unfortunately, it is not possible toobtain the closed form solution for q(

    C

    ), so we rely on the

    ! T2q(1 q)

    T1(1 )= 1

    at (q, ) (global optimum)

    ! T2q(1 q)

    T1(1 )= 1

  • ! T2q(1 q)

    T1(1 )= 1

    at (q, ) (global optimum)

    ) = 12

    1

    r1 4T2

    T1q(1 q)

    !

    substituting (q) to

    1 T2T1

    ln[(1 )/]ln[(1 q)/q]

    =

    T2T1

    q

    (1 ) ln[(1 q)/q]

    Finding the global maximum theoretically

    1 T2T1

    ln[(1 )/]ln[(1 q)/q]

    =

    q

    q(1 q) ln[(1 q)/q] or

    ! f(T2

    /T1

    , q) = 0 ! q(T1

    , T2

    ) ! (T1

    , T2

    ) ! (hWnet

    imax

    , op

    )

  • ! f(T2

    /T1

    , q) = 0 ! q(T1

    , T2

    ) ! (T1

    , T2

    ) ! (hWnet

    imax

    , op

    )

    f(T2/T1, q) = ln

    1 q

    q

    T2

    T1ln

    0

    BB@1 +

    r1 4T2

    T1q(1 q)

    1r

    1 4T2T1

    q(1 q)

    1

    CCAq 1

    2+

    1

    2

    r1 4T2

    T1q(1 q)

    q(1 q)

    numerically found q(C) and (C)

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q*(c0) = *(c0)

    q*(c=1)

    optim

    al tr

    ansi

    tion

    rate

    s

    c

    q**

    c0 and 1 asymptotes

  • schematically . . .

    q

    = q

    net power < 0

  • schematically . . .

    q

    = q

    net power < 0

    C from 0 to 1(T2/T1 from 1 to 0)

    ( ), T1 = 1, T2 = 1/100

    0.1 0.2 0.3 0.4 0.5q

    0.1

    0.2

    0.3

    0.4

    0.5

    0

    0.05

    0.1

    0.15

    0.2

    0.25

    0.3

    ( ), T1 = 1, T2 = 1/10

    0.1 0.2 0.3 0.4 0.5q

    0.1

    0.2

    0.3

    0.4

    0.5

    0 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2

    ( ), T1 = 1, T2 = 1/2

    0.1 0.2 0.3 0.4 0.5q

    0.1

    0.2

    0.3

    0.4

    0.5

    0 0.005 0.01 0.015 0.02 0.025 0.03 0.035 0.04

    ( ), T1 = 1, T2 = 9/10

    0.1 0.2 0.3 0.4 0.5q

    0.1

    0.2

    0.3

    0.4

    0.5

    0

    0.0002

    0.0004

    0.0006

    0.0008

    0.001

    0.0012

    P (T2/T1 = 9/10)

    P (T2/T1 = 1/2)

    P (T2/T1 = 1/10)

    P (T2/T1 = 1/100)

    q

    q

    q

    q

    hWneti( !1) = (q ) {T1 ln[(1 q)/q] T2 ln[(1 )/]}

    q(C ! 0) = (C ! 0) ' 0.083 221 720 199 517 7 q0

    the root of

    2

    1 2q = ln1 q

    q

    q(C = 1) ' 0.217 811 705 719 800(C = 1) = 0

    the root of

    1

    1 q = ln1 q

    q

  • ) = 12

    1

    r1 4T2

    T1q(1 q)

    !

    ) op

    = 1 T2T1

    ln[(1 )/]ln[(1 q)/q]

    =

    q 12+

    1

    2

    r1 4T2

    T1

    q(1 q)

    q(1 q) ln[(1 q)/q]

    =q 1

    2+

    1

    2

    p(1 2q)2 + 4Cq(1 q)

    q(1 q) ln[(1 q)/q]

    = ln

    1 q

    q

    (1 C) ln

    1 +

    p(1 2q)2 + 4Cq(1 q)

    1p

    (1 2q)2 + 4Cq(1 q)

    !q 1

    2+

    1

    2

    p(1 2q)2 + 4Cq(1 q)

    q(1 q)

    f(T2/T1, q) = ln

    1 q

    q

    T2

    T1ln

    0

    BB@1 +

    r1 4T2

    T1q(1 q)

    1r

    1 4T2T1

    q(1 q)

    1

    CCAq 1

    2+

    1

    2

    r1 4T2

    T1q(1 q)

    q(1 q)

    ! f(T2

    /T1

    , q) = 0 ! q(T1

    , T2

    ) ! (T1

    , T2

    ) ! (hWnet

    imax

    , op

    )

    the series expansion at C ! 0

  • 0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q*(c0) = *(c0)

    q*(c=1)

    optim

    al tr

    ansi

    tion

    rate

    s

    c

    q**

    c0 and 1 asymptotes

    the numerically found functional form of

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    quadratic form near c=0

    FIG. 3. Numerically found q and values satisfying Eq. (16), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The quadratic form indicates Eq. (21).

    We verify that the (q, ) is indeed the maximum point byusing the relations of second derivatives

    0BBBBB@@2hPi@q2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@q@

    q=q,=

    1CCCCCA

    2

    =

    T

    21(1 )q

    (1 q) (2q q )2 4T 21 2(1 )2

    2(1 )2q2(1 q)2

    = T1(q )2

    (1 )q3(1 q)3 > 0 ,(18)

    where we use the relation in Eq. (15a), and

    @2hPi@q2

    q=q,=

    = T1[q + (1 2q)]q

    2(1 q)2 < 0 ,

    @2hPi@2

    q=q,=

    = T2[q + (1 2q)]2(1 )2 < 0 .

    (19)

    Therefore, the procedure to calculate the eciency forgiven T2/T1 at the maximum power output seems straight-forward now. First, find the q value satisfying Eq. (16) andsubstitute the q value to Eq. (17a). The only (but very crucial)problem is that f (T2/T1, q) = 0 is a transcendental equationwhose closed-form solution is unattainable.

    2. Asymptotic behaviors based on series expansion

    If we treat q as constant for a moment (which is clearly notthe case, of course, as q is also a function of T2/T1 to satisfy

    schematically . . .

    q

    = q

    no net work

    q(T2/T1 1) 0.0832217201995177= (T2/T1 1)

    q(T2/T1 = 0) 0.217811705719800(T2/T1 = 0) = 0

    as T2/T1 (C) is decreased (increased),respectively

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    f = 0), the function f has the expansion form

    f (T2/T1, q) ="ln

    1 q

    q

    ! 1

    1 q#+

    (1 ln

    T2

    T1

    !+ ln

    q

    (1 q))

    T2

    T1

    !

    + O2666664

    T2

    T1

    !23777775

    (20a)

    when T2/T1 ' 0, and

    f (T2/T1, q) ="ln

    1 q

    q

    ! 2

    1 2q#

    1 T2T1

    !+

    12(1 2q)

    1 T2

    T1

    !2

    + O2666664

    1 T2

    T1

    !33777775

    (20b)

    when T2/T1 ' 1. The upper bound for q is given by the con-dition T2/T1 = 0, satisfying ln[(1 q)/q] = 1/(1 q) andq

    (T2/T1 = 0) ' 0.217 811 705 719 800 found numericallyand (T2/T1 = 0) = 0 exactly from Eq. (15b). T2/T1 = 1always satisfies f (T2/T1, q) = 0 regardless of q values, butthe T2/T1 ' 1 asymptotic case yields the lower bound forq

    (T2/T1 ' 1) = (T2/T1 ' 1) ' 0.083 221 720 199 517 7found numerically. Figure 3 shows the numerical solution(q, ) as a function of

    C

    = 1 T2/T1, where the asymp-totic behaviors derived above hold when T2/T1 ' 0 andT2/T1 ' 1. It seems that q is monotonically decreasedand is monotonically increased, as T2/T1 is increased, i.e.,q

    min = q

    (T2/T1 ' 1), qmax = q(T2/T1 = 0), min = 0, andmax = (T2/T1 ' 1). For later, we numerically obtain thefunctional form of q(

    C

    ) up to the quadratic term by fitting aquadratic function near

    C

    = 0, in the range C

    2 [0, 0.05] inthis case, which is

    q

    (C

    ) ' qmin + 0.0457524C + 0.02767322C . (21)

  • 0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q*(c0) = *(c0)

    q*(c=1)

    optim

    al tr

    ansi

    tion

    rate

    s

    c

    q**

    c0 and 1 asymptotes

    the numerically found functional form of

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    quadratic form near c=0

    FIG. 3. Numerically found q and values satisfying Eq. (16), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The quadratic form indicates Eq. (21).

    We verify that the (q, ) is indeed the maximum point byusing the relations of second derivatives

    0BBBBB@@2hPi@q2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@q@

    q=q,=

    1CCCCCA

    2

    =

    T

    21(1 )q

    (1 q) (2q q )2 4T 21 2(1 )2

    2(1 )2q2(1 q)2

    = T1(q )2

    (1 )q3(1 q)3 > 0 ,(18)

    where we use the relation in Eq. (15a), and

    @2hPi@q2

    q=q,=

    = T1[q + (1 2q)]q

    2(1 q)2 < 0 ,

    @2hPi@2

    q=q,=

    = T2[q + (1 2q)]2(1 )2 < 0 .

    (19)

    Therefore, the procedure to calculate the eciency forgiven T2/T1 at the maximum power output seems straight-forward now. First, find the q value satisfying Eq. (16) andsubstitute the q value to Eq. (17a). The only (but very crucial)problem is that f (T2/T1, q) = 0 is a transcendental equationwhose closed-form solution is unattainable.

    2. Asymptotic behaviors based on series expansion

    If we treat q as constant for a moment (which is clearly notthe case, of course, as q is also a function of T2/T1 to satisfy

    schematically . . .

    q

    = q

    no net work

    q(T2/T1 1) 0.0832217201995177= (T2/T1 1)

    q(T2/T1 = 0) 0.217811705719800(T2/T1 = 0) = 0

    as T2/T1 (C) is decreased (increased),respectively

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    f = 0), the function f has the expansion form

    f (T2/T1, q) ="ln

    1 q

    q

    ! 1

    1 q#+

    (1 ln

    T2

    T1

    !+ ln

    q

    (1 q))

    T2

    T1

    !

    + O2666664

    T2

    T1

    !23777775

    (20a)

    when T2/T1 ' 0, and

    f (T2/T1, q) ="ln

    1 q

    q

    ! 2

    1 2q#

    1 T2T1

    !+

    12(1 2q)

    1 T2

    T1

    !2

    + O2666664

    1 T2

    T1

    !33777775

    (20b)

    when T2/T1 ' 1. The upper bound for q is given by the con-dition T2/T1 = 0, satisfying ln[(1 q)/q] = 1/(1 q) andq

    (T2/T1 = 0) ' 0.217 811 705 719 800 found numericallyand (T2/T1 = 0) = 0 exactly from Eq. (15b). T2/T1 = 1always satisfies f (T2/T1, q) = 0 regardless of q values, butthe T2/T1 ' 1 asymptotic case yields the lower bound forq

    (T2/T1 ' 1) = (T2/T1 ' 1) ' 0.083 221 720 199 517 7found numerically. Figure 3 shows the numerical solution(q, ) as a function of

    C

    = 1 T2/T1, where the asymp-totic behaviors derived above hold when T2/T1 ' 0 andT2/T1 ' 1. It seems that q is monotonically decreasedand is monotonically increased, as T2/T1 is increased, i.e.,q

    min = q

    (T2/T1 ' 1), qmax = q(T2/T1 = 0), min = 0, andmax = (T2/T1 ' 1). For later, we numerically obtain thefunctional form of q(

    C

    ) up to the quadratic term by fitting aquadratic function near

    C

    = 0, in the range C

    2 [0, 0.05] inthis case, which is

    q

    (C

    ) ' qmin + 0.0457524C + 0.02767322C . (21)f(T2/T1 = 0, q

    ) = ln

    1 q

    q

    1

    1 q = 0

    ! q ' 0.217 811 705 719 800

  • 0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q*(c0) = *(c0)

    q*(c=1)

    optim

    al tr

    ansi

    tion

    rate

    s

    c

    q**

    c0 and 1 asymptotes

    the numerically found functional form of

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    quadratic form near c=0

    FIG. 3. Numerically found q and values satisfying Eq. (16), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The quadratic form indicates Eq. (21).

    We verify that the (q, ) is indeed the maximum point byusing the relations of second derivatives

    0BBBBB@@2hPi@q2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@2

    q=q,=

    1CCCCCA

    0BBBBB@@2hPi@q@

    q=q,=

    1CCCCCA

    2

    =

    T

    21(1 )q

    (1 q) (2q q )2 4T 21 2(1 )2

    2(1 )2q2(1 q)2

    = T1(q )2

    (1 )q3(1 q)3 > 0 ,(18)

    where we use the relation in Eq. (15a), and

    @2hPi@q2

    q=q,=

    = T1[q + (1 2q)]q

    2(1 q)2 < 0 ,

    @2hPi@2

    q=q,=

    = T2[q + (1 2q)]2(1 )2 < 0 .

    (19)

    Therefore, the procedure to calculate the eciency forgiven T2/T1 at the maximum power output seems straight-forward now. First, find the q value satisfying Eq. (16) andsubstitute the q value to Eq. (17a). The only (but very crucial)problem is that f (T2/T1, q) = 0 is a transcendental equationwhose closed-form solution is unattainable.

    2. Asymptotic behaviors based on series expansion

    If we treat q as constant for a moment (which is clearly notthe case, of course, as q is also a function of T2/T1 to satisfy

    schematically . . .

    q

    = q

    no net work

    q(T2/T1 1) 0.0832217201995177= (T2/T1 1)

    q(T2/T1 = 0) 0.217811705719800(T2/T1 = 0) = 0

    as T2/T1 (C) is decreased (increased),respectively

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    f = 0), the function f has the expansion form

    f (T2/T1, q) ="ln

    1 q

    q

    ! 1

    1 q#+

    (1 ln

    T2

    T1

    !+ ln

    q

    (1 q))

    T2

    T1

    !

    + O2666664

    T2

    T1

    !23777775

    (20a)

    when T2/T1 ' 0, and

    f (T2/T1, q) ="ln

    1 q

    q

    ! 2

    1 2q#

    1 T2T1

    !+

    12(1 2q)

    1 T2

    T1

    !2

    + O2666664

    1 T2

    T1

    !33777775

    (20b)

    when T2/T1 ' 1. The upper bound for q is given by the con-dition T2/T1 = 0, satisfying ln[(1 q)/q] = 1/(1 q) andq

    (T2/T1 = 0) ' 0.217 811 705 719 800 found numericallyand (T2/T1 = 0) = 0 exactly from Eq. (15b). T2/T1 = 1always satisfies f (T2/T1, q) = 0 regardless of q values, butthe T2/T1 ' 1 asymptotic case yields the lower bound forq

    (T2/T1 ' 1) = (T2/T1 ' 1) ' 0.083 221 720 199 517 7found numerically. Figure 3 shows the numerical solution(q, ) as a function of

    C

    = 1 T2/T1, where the asymp-totic behaviors derived above hold when T2/T1 ' 0 andT2/T1 ' 1. It seems that q is monotonically decreasedand is monotonically increased, as T2/T1 is increased, i.e.,q

    min = q

    (T2/T1 ' 1), qmax = q(T2/T1 = 0), min = 0, andmax = (T2/T1 ' 1). For later, we numerically obtain thefunctional form of q(

    C

    ) up to the quadratic term by fitting aquadratic function near

    C

    = 0, in the range C

    2 [0, 0.05] inthis case, which is

    q

    (C

    ) ' qmin + 0.0457524C + 0.02767322C . (21)f(T2/T1 = 0, q

    ) = ln

    1 q

    q

    1

    1 q = 0

    ! q ' 0.217 811 705 719 800

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(12q0)4{2a21+[(12q0)a212(1q0)q0a2] ln[(1q0)/q0]}}/[(1q

    20)

    2q

    20]. Using Eqs. (24), (25) and (26), Eq. (27) becomes sim-

    ply

    op =12

    C

    +182

    C

    +7 24q0 + 24q20

    96(1 2q0)2 3C

    + O 4C

    . (28)

  • 4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(12q0)4{2a21+[(12q0)a212(1q0)q0a2] ln[(1q0)/q0]}}/[(1q

    20)

    2q

    20]. Using Eqs. (24), (25) and (26), Eq. (27) becomes sim-

    ply

    op =12

    C

    +182

    C

    +7 24q0 + 24q20

    96(1 2q0)2 3C

    + O 4C

    . (28)

  • = ln

    1 q

    q

    (1 C) ln

    1 +

    p(1 2q)2 + 4Cq(1 q)

    1p

    (1 2q)2 + 4Cq(1 q)

    !q 1

    2+

    1

    2

    p(1 2q)2 + 4Cq(1 q)

    q(1 q)0 = f(C , q)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(12q0)4{2a21+[(12q0)a212(1q0)q0a2] ln[(1q0)/q0]}}/[(1q

    20)

    2q

    20]. Using Eqs. (24), (25) and (26), Eq. (27) becomes sim-

    ply

    op =12

    C

    +182

    C

    +7 24q0 + 24q20

    96(1 2q0)2 3C

    + O 4C

    . (28)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    asymptotic form

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0(the horizontal axis). The asymptotic form on the right side indicatesEq. (31).

    schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + O 3C

    . (22)

    0

    0.2

    0.4

    0.6

    0.8

    1

    0 0.2 0.4 0.6 0.8 1

    op

    c = 1 T2 / T1

    at (q*, *)CA = 11c

    c/(2c)c/2

    1+a[ln(1c)b](1c)

    FIG. 5. The eciency at the maximum power op as the function ofthe Carnot eciency

    C

    in Eq. (19) using numerically found optimalq

    values, along with various asymptotic cases: the Curzon-Ahlborneciency CA in Eq. (28), the upper bound C/(2C) and the lowerbound

    C

    /2 in Ref. [19], and the function in Eq. (32) for C

    0.65.

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 a0)a0(1 2a0)32

    C

    +O 3C

    = 0 .

    (23)

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =a0(1 a0)2(1 2a0) . (25)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + O 3C

    .

    (26)

    Using Eqs. (24) and (25), Eq. (26) becomes simply

    op =12

    C

    +182

    C

    + O 3C

    , (27)

    which has exactly the same coecients up to the quadraticterm to those of the Curzon-Ahlborn eciency [35] definedas

    CA = 1 p

    T2/T1 = 1 p

    1 C

    , (28)

    with the expansion form

    CA =12

    C

    +182

    C

    +1

    163

    C

    +5

    1284

    C

    + O(5C

    ) , (29)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(1

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(1

  • 0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q*(c0) = *(c0)

    q*(c=1)

    optim

    al tr

    ansi

    tion

    rate

    s

    c

    q**

    c0 and 1 asymptotes

    = ln

    1 q

    q

    (1 C) ln

    1 +

    p(1 2q)2 + 4Cq(1 q)

    1p

    (1 2q)2 + 4Cq(1 q)

    !q 1

    2+

    1

    2

    p(1 2q)2 + 4Cq(1 q)

    q(1 q)0 = f(C , q)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    asymptotic form

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0(the horizontal axis). The asymptotic form on the right side indicatesEq. (31).

    schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + O 3C

    . (22)

    0

    0.2

    0.4

    0.6

    0.8

    1

    0 0.2 0.4 0.6 0.8 1

    op

    c = 1 T2 / T1

    at (q*, *)CA = 11c

    c/(2c)c/2

    1+a[ln(1c)b](1c)

    FIG. 5. The eciency at the maximum power op as the function ofthe Carnot eciency

    C

    in Eq. (19) using numerically found optimalq

    values, along with various asymptotic cases: the Curzon-Ahlborneciency CA in Eq. (28), the upper bound C/(2C) and the lowerbound

    C

    /2 in Ref. [19], and the function in Eq. (32) for C

    0.65.

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 a0)a0(1 2a0)32

    C

    +O 3C

    = 0 .

    (23)

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =a0(1 a0)2(1 2a0) . (25)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    0

    q(C ! 0) = q0 = (C ! 0) ' 0.083 221 720 199 517 7

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(12q0)4{2a21+[(12q0)a212(1q0)q0a2] ln[(1q0)/q0]}}/[(1q

    20)

    2q

    20]. Using Eqs. (24), (25) and (26), Eq. (27) becomes sim-

    ply

    op =12

    C

    +182

    C

    +7 24q0 + 24q20

    96(1 2q0)2 3C

    + O 4C

    . (28)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    asymptotic form

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0(the horizontal axis). The asymptotic form on the right side indicatesEq. (31).

    schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + O 3C

    . (22)

    0

    0.2

    0.4

    0.6

    0.8

    1

    0 0.2 0.4 0.6 0.8 1

    op

    c = 1 T2 / T1

    at (q*, *)CA = 11c

    c/(2c)c/2

    1+a[ln(1c)b](1c)

    FIG. 5. The eciency at the maximum power op as the function ofthe Carnot eciency

    C

    in Eq. (19) using numerically found optimalq

    values, along with various asymptotic cases: the Curzon-Ahlborneciency CA in Eq. (28), the upper bound C/(2C) and the lowerbound

    C

    /2 in Ref. [19], and the function in Eq. (32) for C

    0.65.

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 a0)a0(1 2a0)32

    C

    +O 3C

    = 0 .

    (23)

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =a0(1 a0)2(1 2a0) . (25)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + O 3C

    .

    (26)

    Using Eqs. (24) and (25), Eq. (26) becomes simply

    op =12

    C

    +182

    C

    + O 3C

    , (27)

    which has exactly the same coecients up to the quadraticterm to those of the Curzon-Ahlborn eciency [35] definedas

    CA = 1 p

    T2/T1 = 1 p

    1 C

    , (28)

    with the expansion form

    CA =12

    C

    +182

    C

    +1

    163

    C

    +5

    1284

    C

    + O(5C

    ) , (29)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(1

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    c1 asymptote

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0 (thehorizontal axis). The

    C

    ! 1 asymptote indicates Eq. (34).schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + a33C

    + O 4C

    . (22)

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 q0)q0(1 2q0)32

    C

    + c3(q0, a1, a2)3C

    + O 4C

    = 0 ,

    (23)

    where c3(q0, a1, a2) = [10q60 + 3a21 6q0(a21 + a2) 6q50(5 +

    6a1+8a2)12q30(1+6a1+16a21+9a2)+q20(1+18a1+132a21+42a2)+q40(31+90a1+96a

    21+120a2)]/[6(12q0)5(1q0)2q20].

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =q0(1 q0)2(1 2q0) . (25)

    Similarly, the coecient a2 in Eq. (22) can also be written interms of q0 alone, by letting c3(q0, a1, a2) = 0 in Eq. (23) andusing the relations in Eqs. (24) and (25), as

    a2 =7q0(1 q0)24(1 2q0) . (26)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    C

    in Eq. (22). Then,

    op =1

    (1 2q0) ln[(1 q0)/q0]C

    +

    a1q03q20+2q30

    +[q20+2a1q0(1+4a1)] ln[(1q0)/q0]

    (12q0)3

    ln2[(1 q0)/q0]2

    C

    + d3(q0, a1, a2)3C

    + O 4C

    ,

    (27)

    where d3(q0, a1, a2) = {2(1 2q0)2a1[q20 + 2a1 q0(1 +4a1)] ln[(1q0)/q0]+2[2q40+a14a212a2+4q0(4a21+3a2)+4q30(1+a1+4a2)2q20(1+3a1+8a21+12a2)] ln2[(1q0)/q0]+(1

  • 0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q*(c0) = *(c0)

    q*(c=1)

    optim

    al tr

    ansi

    tion

    rate

    s

    c

    q**

    c0 and 1 asymptotes

    = ln

    1 q

    q

    (1 C) ln

    1 +

    p(1 2q)2 + 4Cq(1 q)

    1p

    (1 2q)2 + 4Cq(1 q)

    !q 1

    2+

    1

    2

    p(1 2q)2 + 4Cq(1 q)

    q(1 q)0 = f(C , q)

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    asymptotic form

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0(the horizontal axis). The asymptotic form on the right side indicatesEq. (31).

    schematically . . .

    q

    = q

    no net work

    as C is increased

    q(C 0) = (C 0) 0.083 221 720 199 517 7

    q(C = 1) 0.217 811 705 719 800(C = 1) = 0

    FIG. 4. Illustration of the optimal transition rates (q, ) for the max-imum power output as the T2/T1 value varies.

    2. Asymptotic behaviors obtained from series expansion

    The upper bound for q is given by the condition C

    = 1,satisfying ln[(1 q)/q] = 1/(1 q) and q(

    C

    = 1) '0.217 811 705 719 800 found numerically and (

    C

    = 1) = 0exactly from Eq. (16b).

    C

    = 0 always satisfies Eq. (18) re-gardless of q values, so finding the optimal q is meaningless(in fact, when

    C

    = 0, the operating regime for the engineis shrunk to the line q = and there cannot be any positivework). Therefore, let us examine the case

    C

    ' 0 using theseries expansion of q with respect to

    C

    , as

    q

    = q0 + a1C + a22C

    + O 3C

    . (22)

    0

    0.2

    0.4

    0.6

    0.8

    1

    0 0.2 0.4 0.6 0.8 1

    op

    c = 1 T2 / T1

    at (q*, *)CA = 11c

    c/(2c)c/2

    1+a[ln(1c)b](1c)

    FIG. 5. The eciency at the maximum power op as the function ofthe Carnot eciency

    C

    in Eq. (19) using numerically found optimalq

    values, along with various asymptotic cases: the Curzon-Ahlborneciency CA in Eq. (28), the upper bound C/(2C) and the lowerbound

    C

    /2 in Ref. [19], and the function in Eq. (32) for C

    0.65.

    Substituting Eq. (22) into Eq. (18) and expanding the left-handside with respect to

    C

    again, we obtain

    2 (1 2q0) ln[(1 q0)/q0]2q0 1 C

    +q0(1 q0) 2a1(1 2q0)

    2(1 a0)a0(1 2a0)32

    C

    +O 3C

    = 0 .

    (23)

    Letting the linear coecient to be zero yields

    21 2q0 = ln

    1 q0

    q0

    !, (24)

    from which the lower bound for q(C

    ! 0) = q0 =(

    C

    ! 0) ' 0.083 221 720 199 517 7 found numerically[lim

    C

    !0 U(C , q) = 1 2q, thus (C ! 0) = q(C ! 0)by Eq. (16b)]. Figure 3 shows the numerical solution (q, )as a function of

    C

    , where the asymptotic behaviors derivedabove hold when

    C

    ' 0 and C

    ' 1. It seems that q ismonotonically increased and is monotonically decreased,as

    C

    is increased, i.e., qmin = q(

    C

    ! 0), qmax = q(C = 1),min = 0, and

    max =

    (C

    ! 0). Figure 4 illustrates the situ-ation on the (q, ) plane. The linear coecient a1 in Eq. (22)can be written in terms of q0 when we let the coecient of thequadratic term in Eq. (23) to be zero, as

    a1 =a0(1 a0)2(1 2a0) . (25)

    With the relations of coecients in hand, we find theasymptotic behavior of op in Eq. (19) by expanding it withrespect to

    C

    after substituting q as the series expansion of

    0 0

    4

    0

    0.05

    0.1

    0.15

    0.2

    0 0.2 0.4 0.6 0.8 1

    q* a

    nd

    *

    c = 1 T2 / T1

    q**

    q*(c0) = *(c0)q*(c=1)

    asymptotic form

    FIG. 3. Numerically found q and values satisfying Eq. (18), as afunction of

    C

    = 1T2/T1, along with the q(C ! 0) = (C ! 0)and q(

    C

    = 1) values presented in Sec. III B 2. (C

    = 1) = 0(the horizon