production efficiency, environmental sustainability, and...

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Production efficiency, environmental sustainability, and glass quality – a thermodynamic optimization of three conflicting objectives Reinhard Conradt Department of Mineral Engineering and Chair of Glass and Ceramic Composites RWTH Aachen, Germany Tel. +49-241-809-4966, Fax +49-241-8092-129, E-mail [email protected] ABSTRACT Glass producers aim at using their installed melting aggregates at full capacity. At the same time, they aim at minimizing the specific energy consumption, and maximizing glass quality. Obviously, non of the above individual goals can be reached to full extent without impairing the remaining two. In other words: The mentioned objectives constitute the corners of an optimization task. This task is accomplished by evaluating conventional heat balances, taking into account the aspect of availability (or: exergy), applying the fundamentals of heat transfer, and finally making use of the method of so-called finite-time thermodynamics. As a result of this treatment, a performance diagram is presented displaying a distinct curve for a given furnace in a pull rate vs. thermal efficiency diagram. The obtained graph displays two characteristic working points. These are (1) a working point of maximum pull rate (i. e., production efficiency), and (2) a working point of maximum heat exploitation efficiency (i. e., environmental sustainability). These working points clearly distinguish between wasteful and potentially optimal

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  • Production efficiency, environmental sustainability, and glass quality –

    a thermodynamic optimization of three conflicting objectives

    Reinhard Conradt

    Department of Mineral Engineering and Chair of Glass and Ceramic Composites

    RWTH Aachen, Germany

    Tel. +49-241-809-4966, Fax +49-241-8092-129,

    E-mail [email protected]

    ABSTRACT

    Glass producers aim at using their installed melting aggregates at full capacity. At

    the same time, they aim at minimizing the specific energy consumption, and

    maximizing glass quality. Obviously, non of the above individual goals can be

    reached to full extent without impairing the remaining two. In other words: The

    mentioned objectives constitute the corners of an optimization task. This task is

    accomplished by evaluating conventional heat balances, taking into account the

    aspect of availability (or: exergy), applying the fundamentals of heat transfer, and

    finally making use of the method of so-called finite-time thermodynamics. As a

    result of this treatment, a performance diagram is presented displaying a distinct

    curve for a given furnace in a pull rate vs. thermal efficiency diagram. The obtained

    graph displays two characteristic working points. These are (1) a working point of

    maximum pull rate (i. e., production efficiency), and (2) a working point of

    maximum heat exploitation efficiency (i. e., environmental sustainability). These

    working points clearly distinguish between wasteful and potentially optimal

  • 2

    configurations, with the term “optimal” referring to the specific optimization target.

    The lowest pull rate which is still located within the potentially optimal range marks

    a “quality point”. For a given furnace, glass quality enhancement beyond this point

    can be reached under extremely wasteful conditions only.

    INTRODUCTION

    The efficiency of energy utilization of the conventional glass melting process

    seems to have reached its technological limits. According to a recent energy

    benchmarking report [1], the end-port fired horseshoe flame furnace with

    regenerative flue gas heat recovery represents kind of an optimum configuration.

    Yet there is a worldwide quest for further improvement. This quest is driven by the

    continued increase of energy costs as well as by the commitment of individual

    countries to reduce CO2 emission in accordance with the Kyoto protocol. New

    concepts are discussed and tested, among which are conventional ones (like batch

    pre-heating, enhanced combustion technology, use of top burners) and most

    unconventional ones, like submerged combustion, jet melting, or segmentation of

    the entire process. In view of these efforts, it seems necessary to reconsider the

    theoretical basis of the glass melting process and to point out its physical limits as

    derived from the 1rst and 2nd law of thermodynamics. This is done in terms of zero-

    dimensional models yieldings general guidelines of optimization – irrespective of

    their potential realization by technological means. In doing this, we must keep in

    mind that optimization is an ambiguous target. It may be referred to power output, i.

    e., to the maximum pull rate achieved with a given furnace, or to environmental

  • 3

    sustainability, i. e., to the minimum energy required to melt a given amount of

    glass, or to maximum glass quality. None of the mentioned individual targets can

    be reached to full extent without impairing the remaining two.

    The paper starts with a 1rst law treatment, i.e., with a conventional heat balance.

    Quantification of the balance is achieved by combustion calculations, as well as by

    an assessment of the heat involved in the batch-to-melt conversion and the heat

    content of the melt leaving the basin. The suggestions for optimization derived from

    this treatment comprise the use of low-enthalpy batches, the enhancement of heat

    recovery from the hot stream, and heat insulation measures. Such measures have

    been applied with success in the past. However, from a principle point of view,

    none of these measures provide a sufficient condition to push efficiencies beyond

    the practical limits already reached.

    In the second part of the paper, the issue of energy availability is briefly addressed.

    This leads to a time-independent 2nd law treatment of the glass melting process

    resulting in a quite different view of its efficiency. It is shown that the most severe

    loss of availability is involved in the combustion process itself. From the point of

    view of availability, it is an advantage to aim at the highest possible adiabatic flame

    temperature, and to cool down the offgas to the possibly lowest temperature even

    within the process. A later heat recovery is second-best choice only. Another

    suggestion derived from this approach, however, may turn out to be quite

    ambivalent if considered from the point of view of finite-time heat transfer. This is

  • 4

    the suggestion to realize heat transfer across the smallest possible temperature

    gradients, which is equivalent to minimizing the increase of entropy.

    The ambivalence is resolved when the process is treated in its time dependence,

    first by applying the fundamentals of heat transfer, finally by applying the paradigm

    of finite-time thermodynamics. Finite-time process thermodynamics was “invented”

    by a number of theorists [2-3] as an answer to the first world oil crisis during the

    early 70ties. The approach, nowadays used for the optimal configuration of power

    plants, has hardly found access to the glass community. Yet, it provides some

    interesting insights not obtainable by earlier approaches.

    An editorial remark: Temperatures are given in units of K throughout this paper,

    either as absolute temperatures T, or as temperature differences ∆T = T – T0 to the

    environment; T0 = 298 K.

    FIRST LAW HEAT AND POWER BALANCE

    The glass melting process is a high-temperature process converting a batch of

    primary or secondary raw materials to a homogeneous and workable melt. The

    melt has to be made available

    - at a certain temperature Tex (pull temperature),

    - at a certain production rate mG given in t/h; the pull rate r, given in t/(m2⋅h), is

    obtained by r = mG/A; A = melting area.

  • 5

    For a given glass composition, this corresponds to an amount of heat ∆HG =

    cG·∆Tex physically stored in the melt at T = Tex relative to the environment at

    T0 = 298 K. ∆HG is given in kWh/t, the heat capacity of the glass cG in Wh/(t·K).

    ∆HG corresponds, in turn, to a power qG,

    GGG mHq ⋅∆= , (1)

    with qG given in kW. No matter what actually happens inside the furnace, or how it

    is constructed, its ultimate objective as a thermal reactor consists in generating an

    amount of useful thermal power qG. Its objective as a chemical reactor consists in

    bringing about the conversion batch → glass + batch gases characterized by the

    chemical heat demand ∆H°chem (referred to 298 K). As the final steps of chemical

    conversion (i. e., quartz dissolution, fining and refining) involve comparatively small

    amounts of energy only, the time required to reach a desired degree of conversion

    (i. e., a desired quality level) is not directly related to the constraints of heat

    transfer. Thus, as Nemec pointed out [4], the aspect of glass quality yields its own

    constraints for the process. For a given glass, ∆HG is a fixed quantity while ∆H°chem

    is still open to manipulation by the choice of raw materials. If ∆H°chem is referred to

    cullet-free batch, then ∆HG and ∆H°chem may be summarized like

    GochemCex HHyH ∆+∆⋅−= )1( , (2)

  • 6

    where Hex denotes the so-called exploited heat and yC the cullet fraction (per t of

    glass) used in the batch. The corresponding specific power is qex = Hex⋅mG. The

    furnace requires an amount of energy input Hin > Hex made available at a

    temperature TH. When provided by fossile or synthetic fuel, then TH is identical with

    the so-called adiabatic combustion temperature Tad (see table 1).

    Figure 1 illustrates the heat balance of a typical glass melting tank furnace with an

    offgas heat exchanger system. The individual quantities are explained in the figure

    itself. They may be read in an equivalent way as amounts of heat H in kWh/t, or as

    power terms q in kW; amounts of t always refer to the quantity of melted glass. The

    relative proportions of the individual terms in figure 1 depend on: the production

    rate, the furnace age, the type of batch, the type of fuel and oxygen supply. They

    thus represent a momentary production situation (a snap shot) or alternatively, an

    average over a given time interval. Form figure 1, five principal balance equations

    are derived describing the amounts of heat set free in the combustion space,

    exchanged with the furnace body, transferred to the basin, conveyed to the heat

    exchanger, and exchanged within the heat exchanger, respectively. Presented in

    the quoted sequence and in terms of heat amounts, they read

    Hsf = Hin + Hre = Hoff + Hwo + Hwu + Hex , (3)

    Hfire = Hsf - Hoff = Hwo + Hwu + Hex , (4)

    Hht = Hwu + Hex , (5)

    Hoff = Hstack + Hwx + Hre , (6)

    Hexch = Hoff - Hstack = Hwx + Hre . (7)

  • 7

    The meaning of the subscripts is explained in figure 1. The quantities Hin, Hoff, Hre,

    and Hstack related to the hot stream entering or leaving the combustion space or the

    heat exchanger, respectively, can be calculated via combustion calculations (as

    explained in many textbooks) in a fully quantitative way. Likewise, based on own

    work [5-6], the individual heat terms ∆H°chem and ∆HG in eq. (2), and hence, the

    exploited heat, can be calculated in a fully quantitative way for a given pull

    temperature Tex and any batch composition. Thus, by using eqs. (3) to (7), the

    exact values of Hsf, Hfire, Hwx, and the sum of Hwo + Hwu can be derived, too.

    Unfortunately, the individual wall losses Hwo and Hwu and the amount of heat Hht

    transferred to the basin cannot be assessed by this approach. Nevertheless, a few

    meaningful conclusions may be drawn from figure 1 and eqs. (3) to (7). Let us

    express the heat input by the amount MF of fuel (kg per t of glass) and its net

    calorific value HNCV (kWh per kg fuel),

    ,· NCVFin HMH = (8)

    introduce the efficiency ηre of the heat exchanger system ηre = Hre/Hoff, and express

    Hoff in terms of the volume VFH of the offgas, of the air demand VFair, both given in

    m3 (at 298 K and 1 bar) per kg fuel, their heat capacities cH and cair, respectively,

    and the air excess factor λ; T0 = 298 K. Then eq. (3) may be rearranged as

    )T(T)cV1)(?c(V)?(1HHHH

    M0offair

    FairH

    FHreNCV

    exwuwoF −⋅⋅⋅−+⋅⋅−−

    ++= (9)

  • 8

    reflecting the significant influence of ηre and λ on the amount of fuel required.

    According to eq. (9), energy utilization is optimized by a number of conventional

    measures, i.e., by enhancing ηre, by minimizing λ ≥ 1, and by improving the heat

    insulation of the furnace (i.e., by decreasing Hwo and Hwu). As the offgas volume

    always exceeds the air volume, and always has a higher heat capacity than air,

    approx. 75 % is a true physical upper limit of ηre even for an infinitely large heat

    exchanger. Real heat exchangers nowadays approach 65 %. The option to

    minimize Hex by using cullet - see eq. (2) – is also well established. One might also

    think of minimizing ∆H°chem via the choice of raw materials, e.g., by replacing

    alkaline earth carbonates by calcined products or by silicates. Such measures are,

    however, effective only in batches with low cullet content. All above optimization

    suggestions are valid for constant – and moderate – production rates. They may

    not work at all if a furnace already operates in the vicinity of its performance limit

    and are of little use to push the energy utilization efficiency beyond the practical

    limits already reached.

    SECOND LAW TREATMENT OF TIME-INDEPENDENT HEAT TRANSFER

    The energy balance based on 1rst law principles has an essential weakness: It

    counts energy amounts without taking into account their respective values relative

    to the environment at T0 = 298 K. It is quite obvious that an amount of energy Hin

    by itself is not sufficient to melt glass. Hin must be made available at a suitable

    temperature level; otherwise it is useless for the purpose. In general terms, an

  • 9

    amount of heat Hin made available at a temperature level TH can be exploited to at

    most

    Ain = Hin ⋅ (1 – T0 / TH) , (10)

    where Ain is termed „availability“ or „exergy“. Ain is smaller than Hin by the efficiency

    ηC of the generalized Carnot heat engine, which is a direct 2nd law consequence

    under the boundary condition of instantaneous (or time-independent) heat transfer.

    TH determines how valuable Hin is. Transferring Hin to a lower temperature level

    means depreciating it. During a process, energy is conserved but availability is lost.

    From this point of view, optimizing energy utilization does not necessarily mean

    reducing Hin, but minimizing availability losses. In this respect, availability balances

    focus on the aspect of sustainability rather than efficiency. The corresponding

    optimization task focuses on minimizing the entropy increase. The availability

    approach, which is standard in energy conversion technology (see, e.g., [7]) has

    found entry to the glass community in a few cases only [8-11]. Availability may be

    presented in a way complementary to eq. (11) by

    A = H1 – H0 – T0 (S1 – S0) , (11)

    with 1 = state of influx, 0 = state of equilibrium with the environment, H = enthalpy

    (heat), S = entropy. For pure CH4 as fuel, the difference H1 – H0 is equal to the net

    calorific value HNCV = 802.3 kJ/mol (offgas water dissipates as atmospheric

    humidity, not as liquid). The entropy term, by contrast, amounts to only 1.6 kJ/mol.

  • 10

    Consequently, the availability of energy chemically stored in the fuel is almost

    equal to HNCV. This changes the very moment the fuel is ignited. Then

    .11 00

    −⋅

  • 11

    subscripts have the same meaning as in figure 1. As stated before, eqs. (1) to (3)

    also hold for the heat fluxes q. The heat fluxes related to the hot stream passing

    the combustion space are presented in terms of the mass flow rate mH and heat

    capacity cH, respectively, of the offgas. Temperatures T are given in terms of

    temperature differences ∆T = T – T0 to the environment (T0 = 298 K):

    ,offHHoff Tcmq ∆⋅⋅= (13)

    ,oadHHin Tcmq ∆⋅⋅= (14)

    ,adHHoffrein Tcmqq ∆⋅⋅=⋅+η (15)

    where ∆Tad and ∆T°ad refer to the adiabatic combustion temperature with

    preheated and ambient air, respectively. The term qwo is not taken into

    consideration at this stage. Wall losses through the upper structure are non-

    essential (avoidable) losses; they have no role for the function of the process. By

    contrast, the wall losses through the basin are essential losses, at least in part.

    They are not only necessary to promote convective stirring of the glass melt, but

    also to establish a sufficient drain for qht. In this respect, a glass furnace is in no

    way different form any other heat engine drawing heat form an upper reservoir,

    rejecting heat to a lower one, thereby generating a useful power output. This

    aspect has been addressed in earlier literature already [12]. Rearrangement of

    eq. (1), expressed in terms of heat fluxes q, and combination with eqs. (13 – 15)

    yields

  • 12

    ;11

    ∆⋅−−== wuo

    ad

    offre

    oex

    in

    ex wT

    T

    qq

    ηη (16)

    η°ex is the overall efficiency of heat exploitation in the absence of wall losses qwo,

    wwu = qwu/qin is a basin wall loss ratio. The unknown quantity ∆Toff is given by

    ( ) ( ) .exp htexadexoff NTUTTTT −⋅∆−∆+∆=∆ (17)

    Here, in agreement with eqs. (14 – 15),

    .offreo

    adad TTT ∆⋅+∆=∆ η (18)

    NTUht is the so-called number of transfer units related to the flux qht. NTUht may be

    approximated by NTUht = αht/(cG·r); αht is a heat transfer number given in

    W/(m2·K), cG is the heat capacity of the glass melt in Wh/(t·K) and r ist the pull

    rate in t/(m2·h). The ratio b = αht/cG may be interpreted as a reference pull rate.

    Inserting eq. (18) into (17), resolving for ∆Toff, and inserting ∆Toff in eq. (16) yields

    the following relation between efficiency η°ex and pull rate r:

    ( )( ) .)exp()exp(1

    11

    00

    0wuhto

    ad

    exo

    ado

    ad

    ex

    htre

    reoex wNTUTT

    TTTTTT

    NTU−

    −⋅

    −−

    +−−

    ⋅−⋅−

    −−=

    ηη

    η (19)

  • 13

    The effect of the wall losses qwo through the upper structure is taken into account

    by multiplying η°ex with wwo = qin/(qin + qwo). Since qin depends on the pull rate r

    while qwo does not, wwo assumes a form like wwo = (1 + w/r)-1. Like b, w has the

    meaning of a reference pull rate. Typically, b and w assume values of b = 2 to 8

    and w = 0.5 to 2 t/(m2·d), respectively. For a given production situation

    characterized by a given batch (see eq. (2)) and a given pull temperature Tex, the

    actual heat demand Hin = Hex/ηex can be calculated as a function of the pull rate.

    This is shown in figure 3 for Hex = 500 kWh/t, Tad = 3000 K (2700 °C), Tex = 1523 K

    (1250 °C) and wwu = 0.2. The results feature the behavior actually found in

    industry. The combination b = 8, w = 0.5 represents a large furnace with good

    internal heat transfer and low wall losses. Such a furnace is especially efficient at

    high pull rates. It reacts, however, to changes of the internal heat transfer in a very

    sensitive way. Small furnaces typically exhibit high wall losses (here represented

    by w = 2). Beyond this, with their small basin volumes resulting in short dwell times

    of the melt, they do not reach the high-pull regime. They react very sensitive to

    even moderate under-pull, but are less sensitive to changes of the internal heat

    transfer than large furnaces.

    FINITE-TIME THERMODYNAMICS

    The approach presented in the previous section is helpful in predicting the

    characteristic variation of the actual energy demand Hin with the pull rate for a

    given furnace. The approach may be refined by using more sophisticated

    expressions for NTUht, wwu, and wwu than done in the present paper. The

  • 14

    shortcoming of the approach consists in the fact that no constraint is put on the pull

    rate r itself. Rather, r is treated as an independent variable. This makes sense for

    simple heat exchangers in which the flow of cooling agent can be increased, in

    principle, without limits. The limits related to glass quality have been pointed out by

    [4]. But there are thermal constraints involved, too, which are not related to glass

    quality. Therefore, let us complement the previous approach by the so-called finite-

    time thermodynamics. In this approach, the glass furnace is treated as heat engine

    generating an output qex of useful power. Thus, qex itself becomes the target of

    optimization. In other words: Since qex is directly proportional to the pull rate r, the

    approach focuses on the optimal and extremal points of r. Finite-time thermo-

    dynamics has been developed earlier [2-3]; it has been used with success to

    configure, e. g., power plants. The principle idea is sketched in figure 4: A

    reversible heat conversion machine operates between a limited upper reservoir

    and TH and an unlimited lower reservoir at T0 (i.e., the environment). The restricted

    heat fluxes between the reservoir at TH and the machine, and between the

    machine and the environment, respectively, decrease the temperature difference

    Tht - Twu across which the machine operates. For simplicity, let us consider

    Twu → TL (no heat resistance towards the environment). While the heat flux

    ( )htHht TTq −≈ (20)

    increases with decreasing Tht, the power output

  • 15

    Chtht

    Lht qT

    Tqp η⋅=

    −⋅= 1 (21)

    decreases, and vice versa. As shown in literature [2-3, 13], the power output

    depends on the actual value of Tth, which may be expressed by a dependence on

    the Carnot type efficiency ηC (where pmax is found by the condition ∂p/∂Tht = 0):

    ( )2max1

    1

    /LH

    LH

    TT

    TTpp

    −−⋅

    η

    (22)

    yielding the well-known Curzon-Ahlborn efficiency

    H

    LAC T

    T−= 1..η (23)

    at the point of maximum power output p = pmax. The heat leak qwo is introduced in

    the same was done in the previous section. Figure 5 shows the results for a zero, a

    low, and a high heat leak qwo. It is interesting to note that in the realistic case of a

    non-zero heat leak, the curves display two distinctly different optimal points, i.e.,

    one referring to minimum entropy production (i. e., maximum sustainability), and

    one to maximum power output. With increasing heat leak, both points approach

    each other.

  • 16

    It has been debated whether or not the discussed scenario may be transferred to a

    glass furnace. After all, glass melting obviously is a heat transfer process, not a

    heat conversion process; beyond this, the endoreversibility of the processes in the

    basin may be doubted. The latter point is resolved easily: The pull of hot glass and

    its continuous replacement by a corresponding amount of batch constitutes a cycle

    in the same way as the continuous supply of fuel and release of exhaust gas does

    for an Otto engine. In fact, it has been shown [14] that endoreversibility is not a

    prerequisite for the application of the method. The former point is by far more

    difficult to resolve: The efficiency related to the intrinsic cycle must have a Carnot

    type form; otherwise p(η) displays a steady decrease or increase only, but no

    maximum. For the time being, let us lean on a general result from a theoretical

    investigation [15] justifying the above approach in a most general way. The

    justification is based on a common expression for the maximum entropy source

    which is the same for operations with and without work. Thus, for a large number of

    processes in which linear approximations are acceptable, models and optimization

    results in both kinds of operations are identical [15]. Therefore, let us apply the

    results from figure 5 to glass furnaces in general and interpret them accordingly.

    This is done in figure 6. A furnace yielding 3.5 t/(m2·d) as upper limit of the pull

    rate is taken as example. Again, two distinct optimal points appear, referring to pull

    rates of 2.5 and 3,5 t/(m2·d) at heat exploitation efficiencies of 53 and 63 %,

    respectively. The bold part of the curve marks the range within which the objectives

    of production efficiency and energy exploitation efficiency can be optimized.

    Operations aiming at high glass quality as the primary optimization target apply low

  • 17

    pull rates only. For these cases, the plot in figure 6 allows to define yet another

    optimal point. It corresponds to the position on the lower branch of the curve at the

    efficiency corresponding to maximum power output. This point shall be termed

    “quality point”. At the quality point, maximum glass quality is obtained under the

    constraint of an optimized energy utilization efficiency. Lowering the pull rate below

    this point, however, leads to an extremely wasteful under-pull of the furnace. The

    left part of the upper branch of the curve is of limited practical interest only. It

    corresponds to an overdriven combustion space, is eventually entered in the

    attempt to drive a furnace towards high pull due to economic pressure, and should

    be avoided by any means.

    CONCLUSION

    A hierarchy of theoretical approaches was presented yielding an increasingly

    distinct description of the thermal performance of glass furnaces. For the time

    being, this is done on a quite abstract level only. Verification against a sufficiently

    large number of data obtained from real furnaces will follow in a future paper. The

    starting point of a numerical quantification of all approaches presented is the

    conventional heat balance. It can be established in a fully quantitative way for

    individual furnaces by retrospectively evaluating factory data typically recorded on

    a day-by-day routine by every producer, and by calculating the intrinsic heat

    demand ∆H°chem for the batch used in a most accurate way. The observation time

    span should be extended over sufficiently long time spans comprising significant

    changes of the pull rate. Based on such quantification, the more sophisticated

  • 18

    approaches can be quantified for individual furnaces, too. This means in detail, that

    the conflicting optimization targets of production efficiency, heat exploitation

    efficiency, and glass quality can be optimized for individual cases. For the latter

    aspect of quality, a model as presented in [4] is implemented, balancing the

    chemical versus the thermal constraints of an operation. In a situation where glass

    industry is exposed to increasing pressure by economy and by environmental

    regulations, a clear understanding of the achievable limits of individual operations

    may be of great help.

  • 19

    REFERENCES

    [1] R. G. C. Beerkens, J. van Limpt: Energy efficiency benchmarking of glass

    furnaces. 62nd Conference on Glass Problems, Illinois 2001.

    [2] F. L. Curzon, B. Ahlborn: Efficiency of a Carnot engine at maximum power

    output. Am. J. Phys. 43 (1975), 22-24.

    [3] B. Andresen, R. S. Berry, M. J. Ondrechen, P. Salamon: Thermodynamics

    for processes in finite time. Acc. Chem. Res. 17 (1984), 266-271.

    [4] L. Nemec: Energy consumption in the glass melting process. Pt. 1.

    Theoretial relations. Pt. 2. Results of calculations. Glastechn. Ber. Glass Sci.

    Technol. 68, (1995), 1-20, 39-50.

    [5] R. Conradt, P. Pimkhaokham: An easy-to-apply method to estimate the heat

    demand for melting technical silicate glasses. Glastechn. Ber. 63K (1990),

    134-143.

    [6] R. Conradt: Chemical structure, medium range order, and crystalline

    reference state of multicomponent oxide liquids and glasses. J. Non-Cryst.

    Solids 345 & 346 (2004), 16-23.

    [7] K. Lucas: Thermodynamik – Die Grundgesetze der Energie- und

    Stoffumwandlungen. Springer-Verlag, Berlin 2006.

    [8] F. Bosnjakovic: The meaning of the second theorem of thermodynamics for

    the heat balance of furnaces. (German). Glastechn. Ber. 32 (1959), 6-47.

    [9] I. Huhmann-Kotz: Untersuchung und Beurteilung von Glasschmelzwannen

    durch Exergiebilanzen. Glastechn. Ber. 51 (1959), 47-53.

  • 20

    [10] W. Trier: Glasschmelzöfen. Konstruktion und Betriebsverhalten. Kap.

    5.1.5.5. Exergiebilanzen, Springer-Verlag, Berlin (1984), 91-93.

    [11] S. Chengxu, X. Jianming: The exergy analysis of a glass tank furnace.

    Glass Technol. 32 (1991), 217-218.

    [12] D. Aufhäuser: The glass melting furnace as heat engine. (German).

    Glastech. Ber. 6 (1928-29), 372-379.

    [13] P. Salamon, K. H. Hoffmann, S. Schubert, R. S. Berry, B. Andresen: What

    conditions make minimum entropy production equivalent to maximum power

    production? J. Non-Eq. Thermodynamics 26 (2001), 78-83.

    [14] J. Chen, Z. Yan, G. Lin, B. Andresen: On the Curzon-Ahlborn efficiency and

    its connection with the efficiencies of real heat engines. Energy Concersion

    & Management 42 (2001, 173-181.

    [15] S. Sieniutycz: A synthesis of thermodynamic models unifying traditional and

    work-driven operations with heat and mass exchange. Open Systems &

    Information Dyn. 10 (2003), 31-49.

  • 21

    Table 1. Adiabatic combustion temperatures Tad in K for CH4 in different

    combustion scenarios; λ = oxygen excess factor (lambda factor)

    adiabatic temperature Tad in K

    air-fuel,

    ambient air (298 K)

    air-fuel,

    air pre-heated to1500 K

    oxy-fuel

    λ = 1.00 2332 3125 4746

    λ = 1.02 2303 3102 4718

    λ = 1.08 2221 3036 4634

  • 22

    heat exchanger melting tank

    stack losses (stack)

    recovered (re)

    set free (sf)exchanged (fire)transferred (ht)

    exploited heat (ex)

    wall losses,basin (wu)

    wall losses,upper structure (wo)

    wall losses,heat exchanger (wx)

    exchanged in theheat exchanger (exch)

    heat input

    (in)

    offgas(off)

    q = H·mG[kW] = [kWh/t]·[t/h]

    Figure 1. Heat balance of a conventional glass furnace with offgas heat recovery;

    the balance is valid for amounts of heat H per t of melted glass, or

    power terms q = H⋅mG ; mG = production rate in t/h

  • 23

    qre = ηre·qoff, Tre

    qin + qre, Tad qoff, Toff

    qex, Tex

    qwo, Two

    qwu, Twu

    qht, Tht

    Figure 2 Heat flux balance of a glass furnace showing both heat fluxes and

    corresponding temperature levels; ηre is the efficiency of the heat

    exchanger; subscripts have the same meaning as in figure 1

  • 24

    0 1 2 3 41000

    1500

    2000

    2500

    3000

    Hin in

    kW

    h/t

    r in t/(m²·d)

    w = 2

    w = 0.5

    b = 2

    4

    8

    b = 4

    8

    Figure 3. Modeled dependence of the required heat input Hin as a function of

    the pull rate r for the case: intrinsic heat demand Hex = 500 kWh/t,

    adiabatic offgas temperature Tad = 3000 K (2700 °C), pull

    temperature Tex = 1523 K (1250 °C), and basin wall loss ratio

    wwu = 0.2; w is a parameter related to qwo presenting the wall losses

    through the upper structure: b is a parameter presenting the heat

    transfer rate qht from the combustion space to the basin; both w and b

    are given in dimensions of a pull rate

  • 25

    TH

    Tht

    Twu

    TL

    (limited) upper heat reservoir

    (unlimited) lower heat reservoir

    endo-reversibleprocess

    finite time heat transfer

    exploitedpower p

    qht

    qL finite time heat transfer

    heatleak qwo

    Figure 4. Sketch of an endoreversible heat engine operating between two heat

    reservoirs at TH and TL involving constrained heat transfer rates qht

    and qL, respectively (so-called Curzon-Ahlborn machine [2]); the

    actual temperature difference across which the machine operates

    thus becomes Tht – Twu; in addition, a heat leak qwo is employed

  • 26

    0.0 0.2 0.4 0.6 0.8 1.0

    1.0

    0.0

    low heatleak

    high heat leak

    no heat leak

    efficiency η

    maximumsustain-ability

    maximum power output

    p/p m

    ax

    Figure 5. Result for the Curzon-Ahlborn machine (see figure 4) with heat leak,

    presented as a plot of relative power output p/pmax vs. thermal

    efficiency η

  • 27

    0.0 0.2 0.4 0.6 0.8 1.00.0

    0.5

    1.0

    1.5

    2.0

    2.5

    3.0

    3.5

    4.0

    pull r

    ate

    in t/

    (m²·d

    )

    efficiency ηex

    maximum power output

    maximumsustain-ability

    sustainabilityvs. efficiency

    quality vs.sustainability

    efficiency vs. sustainability

    under -pu

    ll throug

    h basin

    over -d

    riven c

    ombu

    stiom

    space

    wasteful configurations optimal configurations

    „quality point“

    Figure 6. Interpretation of the performance of a glass melting furnace in terms

    of a Curzon-Ahlborn type behavior, presented as a plot of pull rate vs.

    the efficiency of heat exploitation ηex = Hex/Hin; the bold part of the

    curve marks the range within which the three optimization targets of

    production efficiency, heat exploitation efficiency (environmental

    sustainability), and glass quality can be balance against each other