EBK THERMODYNAMICS: AN ENGINEERING APPR
EBK THERMODYNAMICS: AN ENGINEERING APPR
8th Edition
ISBN: 8220100257056
Author: CENGEL
Publisher: YUZU
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Chapter 15.7, Problem 108RP

A steam boiler heats liquid water at 200°C to superheated steam at 4 MPa and 400°C. Methane fuel (CH4) is burned at atmospheric pressure with 50 percent excess air. The fuel and air enter the boiler at 25°C and the products of combustion leave at 227°C. Calculate (a) the amount of steam generated per unit of fuel mass burned, (b) the change in the exergy of the combustion streams, in kJ/kg fuel, (c) the change in the exergy of the steam stream, in kJ/kg steam, and (d) the lost work potential, in kJ/kg fuel. Take T0 = 25°C.

(a)

Expert Solution
Check Mark
To determine

The amount of steam generated per unit of fuel mass burned.

Answer to Problem 108RP

The amount of steam generated per unit of fuel mass burned is 18.72kgsteam/kgfuel_.

Explanation of Solution

Write the energy balance equation using steady-flow equation.

EinEout=ΔEsystem (I)

Here, the total energy entering the system is Ein, the total energy leaving the system is Eout, and the change in the total energy of the system is ΔEsystem.

Substitute 0 for Ein, Qout for Eout, and ΔU for ΔEsystem in Equation (I)

(0)Qout=ΔUQout=NP(h¯f°+h¯h¯°)PNR(h¯f°+h¯h¯°)RQout=NP(h¯f°+h¯500Kh¯298K°)PNR(h¯f°)R (II)

Here, the enthalpy of formation for product is h¯f,P°, the enthalpy of formation for reactant is h¯f,R°, the mole number of the product is NP, and the mole number of the reactant is NR.

Calculate the molar mass of the CH4.

MCH4=[(NC)(MC)+(NH)(MH)] (III)

Here, the number of carbon atoms is NC, the molar mass of the carbon is MC, the number of hydrogen atoms is NH, the molar mass of the hydrogen is MH.

Determine the amount of steam generated per unit mass of fuel burned from an energy balance.

msmf=QoutΔhs (IV)

Here, the mass of the steam is ms, the mass of the fuel burned is mf, and the change in the enthalpy of the steam.

Conclusion:

Perform unit conversion of temperature at state 1 from degree Celsius to Kelvin.

For air temperature enter in the machine,

Tenter=25°C=(25+273)K=298K

For air temperature exit from the machine,

Tleave=227°C=(227+273)K=500K

Write the combustion equation of 1 kmol for CH4.

{CH4+3(O2+3.76N2)}{CO2+2H2O+O2+11.28N2} (V)

Here, liquid methane is CH4, stoichiometric coefficient of air is ath, oxygen is O2, nitrogen is N2, carbon dioxide is CO2 and water is H2O.

Refer Appendix Table A-18, A-19, A-20, and A-23, obtain the enthalpy of formation, at 298 K , and 500 K for CH4, O2, N2, H2O, and CO2 is given in a table (I) as:

Substanceh¯f°kJ/kmolh¯298KkJ/kmolh¯500KkJ/kmol
CH4-74,850------
O20868214,770
N20866914,581
H2O(g)-241820990416,828
CO2-393,520936417,678

Refer Equation (V), and write the number of moles of reactants.

NR,CH4=1kmolNR,O2=3kmolNR,N2=11.28kmol

Here, number of moles of reactant methane, oxygen and nitrogen is NR,CH4,NR,O2andNR,N2 respectively.

Refer Equation (V), and write the number of moles of products.

NP,CO2=1kmolNP,H2O=2kmolNP,O2=1kmolNP,N2=11.28kmol

Here, number of moles of product carbon dioxide, water, oxygen and nitrogen is NP,CO2,NP,H2O,NP,O2andNN,N2 respectively.

Substitute the value of substance in Equation (II).

Qout=[(1)(393,520kJ/kmol+17,678kJ/kmol9364kJ/kmol)+(2)(241,820kJ/kmol+16,828kJ/kmol9904kJ/kmol)+(1)(0+14,770kJ/kmol8682kJ/kmol)+(11.28)(0+14,581kJ/kmol8669kJ/kmol)(1)(74,850kJ/kmol)]=707,373kJ/kmoloffuel

Therefore the heat transfer for CH4 is 707,373kJ/kmoloffuel.

Substitute 1 for NC, 12kg/kmol for MC, 4 for NH, 1kg/kmol for MH in Equation (III).

MCH4=[(12)+(1)(4)]kg/kmol=[(12)+(4)]kg/kmol=16kg/kmol

Calculate the heat loss per unit mass of the fuel.

Qout=707,373kJ/kmolof fuel16kg/kmolof fuel=44,211kJ/kg

From the table A-4, “Saturated water-Temperature” obtain the value of the saturated enthalpy and entropy of liquid at the 200°C temperature as 852.26kJ/kg and 2.3305kJ/kgK.

From the table A-6, “Superheated water” obtain the value of the enthalpy and entropy at the 400°C temperature and 4 MPa pressure as 3214.5kJ/kg and 6.7714kJ/kgK.

Substitute 44,211kJ/kgfuel for Qout, 3214.5kJ/kg for h2, and 852.26kJ/kg for h1 in Equation (IV).

msmf=44,211kJ/kgfuel(3214.5852.26)kJ/kgsteam=44,211kJ/kgfuel2362.24kJ/kgsteam=18.715kgsteam/kgfuel18.72kgsteam/kgfuel

Thus, the amount of steam generated per unit of fuel mass burned is 18.72kgsteam/kgfuel_.

(b)

Expert Solution
Check Mark
To determine

The change in the exergy of the combustion steams, in kJ/kgfuel.

Answer to Problem 108RP

The change in the exergy of the combustion steams, in kJ/kgfuel is 49,490kJ/kgfuel_.

Explanation of Solution

Write the expression for entropy generation during this process.

Sgen=SPSR+QoutTsurr (VI)

Write the combustion equation of Equation (VI)

Sgen=SPSR+QoutTsurrSgen=NPs¯PNRs¯R+QoutTsurr (VII)

Here, the entropy of the product is s¯P, the entropy of the reactant is s¯R, the heat transfer for C8H18 is Qout, and the surrounding temperature is Tsurr.

Determine the entropy at the partial pressure of the components.

Si=Nis¯i(T,Pi)=Nis¯i°(T,P0)Ruln(yiPm) (VIII).

Here, the partial pressure is Pi, the mole fraction of the component is yi, the total pressure of the mixture is Pm, and the universal gas constant is Ru.

Write the expression for exergy change of the combustion steam is equal to the exergy destruction.

ΔXgases=Xdes=T0Sgen (IX)

Here, the thermodynamic temperature of the surrounding is T0.

Conclusion:

Refer Equation (VIII) for reactant and product to calculation the entropy in tabular form as:

For reactant entropy,

SubstanceNiyi

s¯i°

(T, 1 atm)

Ruln(yiPm)Nis¯i
CH41---186.16---186.16
O230.21205.04-12.98654.06
N211.280.79191.61-1.9602183.47
SR=3023.69kJ/K

For product entropy,

SubstanceNiyi

s¯i°

(T, 1 atm)

Ruln(yiPm)Nis¯i
CH410.0654234.814-22.67257.48
H2O(g)20.1309206.413-16.91446.65
O210.0654220.589-22.67243.26
N211.280.7382206.630-2.5242359.26
SP=3306.65kJ/K

Substitute 3306.65kJ/K for SP, 3023.69kJ/K for SR, 298K for Tsurr, and 707,373kJ/kmol for Qout in Equation (VI).

Sgen=(3306.653023.69)kJ/K+707,373kJ/kmolK298K=(282.96)kJ/K+(2373.735)kJ/kmol=2656.695kJ/kmolK

Substitute 2657kJ/kg for Sgen and 298K for T0 in Equation (IX).

ΔXgases=(298K)×(2657kJ/kg)=791,786kJ/kmolfuel

Calculate the exergy destruction per unit mass of the basis.

Qout=791,786kJ/kmolof fuel16kg/kmolof fuel=49,490kJ/kg

Thus, the change in the exergy of the combustion steams, in kJ/kgfuel is 49,490kJ/kgfuel_.

(c)

Expert Solution
Check Mark
To determine

The exergy change of the steam, in kJ/kgsteam.

Answer to Problem 108RP

The exergy change of the steam, in kJ/kgsteam is 1039kJ/kgsteam_.

Explanation of Solution

Determine the exergy change of the steam stream.

ΔXsteam=ΔhT0Δs=(h2h1)T0(s2s1) (X)

Here, the final enthalpy is h2, the initial enthalpy is h1, the final entropy is s2, and the initial entropy is s1.

Conclusion:

Substitute 3214.5kJ/kg for h2, 852.26kJ/kg for h1, 6.7714kJ/kgK for s2, and 2.3305kJ/kgK for s1 in Equation (X).

ΔXsteam=(3214.5852.26)kJ/kg(298K)(6.77142.3305)kJ/kgK=2362.24kJ/kg(298K)×4.4409kJ/kgK=1038.85kJ/kgsteam1039kJ/kgsteam

Thus, the exergy change of the steam, in kJ/kgsteam is 1039kJ/kgsteam_.

(d)

Expert Solution
Check Mark
To determine

The lost work potential, in kJ/kgfuel.

Answer to Problem 108RP

The lost work potential, in kJ/kgfuel is 30,040kJ/kgfuel_.

Explanation of Solution

Determine the lost work potential is the negative of the net exergy change both streams.

Xdest=[msmfΔXsteam+ΔXgases] (XI)

Conclusion:

Substitute 18.72kgsteam/kgfuel for ms/mf, 1039kJ/kgsteam for ΔXsteam, and 49,490kJ/kgsteam for ΔXgases in Equation (XI).

Xdest=[(18.72kgsteam/kgfuel)×(1039kJ/kgsteam)+(49,490kJ/kgfuel)]=[(19450.08kJ/kgfuel)+(49,490kJ/kgfuel)]=30,039.9kJ/kgfuel30,040kJ/kgfuel

Thus, the lost work potential, in kJ/kgfuel is 30,040kJ/kgfuel_.

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Chapter 15 Solutions

EBK THERMODYNAMICS: AN ENGINEERING APPR

Ch. 15.7 - What are the causes of incomplete combustion?Ch. 15.7 - Which is more likely to be found in the products...Ch. 15.7 - Methane (CH4) is burned with the stoichiometric...Ch. 15.7 - Prob. 14PCh. 15.7 - n-Butane fuel (C4H10) is burned with the...Ch. 15.7 - Prob. 16PCh. 15.7 - Prob. 17PCh. 15.7 - 15–18 n-Octane (C8H18) is burned with 50 percent...Ch. 15.7 - In a combustion chamber, ethane (C2H6) is burned...Ch. 15.7 - Prob. 20PCh. 15.7 - Prob. 21PCh. 15.7 - 15–22 One kilogram of butane (C4H10) is burned...Ch. 15.7 - 15–23E One lbm of butane (C4H10) is burned with 25...Ch. 15.7 - Prob. 24PCh. 15.7 - A fuel mixture of 60 percent by mass methane (CH4)...Ch. 15.7 - A certain natural gas has the following volumetric...Ch. 15.7 - Prob. 27PCh. 15.7 - A gaseous fuel with a volumetric analysis of 45...Ch. 15.7 - Prob. 30PCh. 15.7 - 15–31 Octane (C8H18) is burned with dry air. The...Ch. 15.7 - Prob. 32PCh. 15.7 - Prob. 33PCh. 15.7 - Prob. 34PCh. 15.7 - Prob. 35PCh. 15.7 - Prob. 36PCh. 15.7 - Prob. 37PCh. 15.7 - Prob. 38PCh. 15.7 - Prob. 39PCh. 15.7 - Prob. 40PCh. 15.7 - Prob. 41PCh. 15.7 - Prob. 42PCh. 15.7 - Prob. 44PCh. 15.7 - Repeat Prob. 1546 for liquid octane (C8H18).Ch. 15.7 - Ethane (C2H6) is burned at atmospheric pressure...Ch. 15.7 - Reconsider Prob. 1550. What minimum pressure of...Ch. 15.7 - Calculate the HHV and LHV of gaseous n-octane fuel...Ch. 15.7 - Prob. 49PCh. 15.7 - Prob. 50PCh. 15.7 - Consider a complete combustion process during...Ch. 15.7 - Prob. 53PCh. 15.7 - Prob. 54PCh. 15.7 - Propane fuel (C3H8) is burned with an airfuel...Ch. 15.7 - 15–56 Hydrogen (H2) is burned completely with the...Ch. 15.7 - Prob. 57PCh. 15.7 - Prob. 58PCh. 15.7 - Octane gas (C8H18) at 25C is burned steadily with...Ch. 15.7 - Prob. 61PCh. 15.7 - Liquid ethyl alcohol [C2H5OH(l)] at 25C is burned...Ch. 15.7 - Prob. 63PCh. 15.7 - Prob. 64PCh. 15.7 - A constant-volume tank contains a mixture of 120 g...Ch. 15.7 - Prob. 67PCh. 15.7 - Prob. 68PCh. 15.7 - Prob. 69PCh. 15.7 - A fuel is completely burned first with the...Ch. 15.7 - Prob. 71PCh. 15.7 - Acetylene gas (C2H2) at 25C is burned during a...Ch. 15.7 - Octane gas (C8H18) at 25C is burned steadily with...Ch. 15.7 - Express the increase of entropy principle for...Ch. 15.7 - Prob. 81PCh. 15.7 - What does the Gibbs function of formation gf of a...Ch. 15.7 - Liquid octane (C8H18) enters a steady-flow...Ch. 15.7 - Benzene gas (C6H6) at 1 atm and 77F is burned...Ch. 15.7 - Prob. 87PCh. 15.7 - Prob. 88PCh. 15.7 - A steady-flow combustion chamber is supplied with...Ch. 15.7 - Prob. 91RPCh. 15.7 - 15–92 A gaseous fuel with 80 percent CH4, 15...Ch. 15.7 - Prob. 93RPCh. 15.7 - Prob. 94RPCh. 15.7 - Prob. 95RPCh. 15.7 - Prob. 96RPCh. 15.7 - Prob. 97RPCh. 15.7 - Prob. 98RPCh. 15.7 - Prob. 99RPCh. 15.7 - Prob. 100RPCh. 15.7 - A 6-m3 rigid tank initially contains a mixture of...Ch. 15.7 - Prob. 102RPCh. 15.7 - Propane gas (C3H8) enters a steady-flow combustion...Ch. 15.7 - Determine the highest possible temperature that...Ch. 15.7 - Prob. 106RPCh. 15.7 - Prob. 107RPCh. 15.7 - A steam boiler heats liquid water at 200C to...Ch. 15.7 - Repeat Prob. 15112 using a coal from Utah that has...Ch. 15.7 - Liquid octane (C8H18) enters a steady-flow...Ch. 15.7 - Prob. 111RPCh. 15.7 - Prob. 112RPCh. 15.7 - Prob. 113RPCh. 15.7 - Consider the combustion of a mixture of an...Ch. 15.7 - A fuel is burned steadily in a combustion chamber....Ch. 15.7 - A fuel is burned with 70 percent theoretical air....Ch. 15.7 - Prob. 123FEPCh. 15.7 - One kmol of methane (CH4) is burned with an...Ch. 15.7 - An equimolar mixture of carbon dioxide and water...Ch. 15.7 - The higher heating value of a hydrocarbon fuel...Ch. 15.7 - Acetylene gas (C2H2) is burned completely during a...Ch. 15.7 - Prob. 129FEPCh. 15.7 - A fuel is burned during a steady-flow combustion...
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