Upload
felix-ws
View
218
Download
0
Embed Size (px)
Citation preview
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 1/11
Ministry of Science and Technology
Department of Technical and Vocational Education
Promotion Examination for A.G.T.I. Year I
Date: 26.10.06 Time: 12:30-
15:30
Met-04011 Metallurgical Thermodynamics I
Answer any five.
1 (a) The combustion of acetylene fuel with nitrous oxide as oxidant at 25ºC, is
widely performed in flame emission spectrometry. Calculate the maximum
temperature attained if the best mixture corresponds to the reaction:
(C2H2) + 3 (N2O) = 2(CO) + (H2O) + 3 (N2)
Assume that water is undissociated.
ΔHº298 (C2H2) = 54.23 kcal/mole, ΔHº298 (N2O) = 19.70 kcal/mole,
ΔHº298 (CO) = -26.42 kcal/mole, ΔHº298 (H2O) = -57.80 kcal/mole,
Cp for (CO) = 6.8 + 1.0 x 10-3T – 0.11 x 105T-2 cal/deg/mole
Cp for (H2O) = 7.17 + 2.56 x 10-3T – 0.08 x 105T-2 cal/deg/mole
Cp for (N2) = 6.5 + 1.0 x 10-3T cal/deg/mole
Ans: (C2H2) + 3 (N2O) = 2(CO) + (H2O) + 3 (N2)
ΔHº298 (Reaction) = 2 ΔHºCO + ΔHºH2O + 3 ΔHº N2 – (ΔHºC2H2 + ΔHº N2O)
= (2 x -26.42) + (-57.80) + (0) – (54.23) – (3x19.70)
= -223.97 Kcal
Heat evolved = dTpC product
Tm
∫ ∑298
223970 = ( )∫ ++Tm
NOHCO dTCpCpCp298
2232
=
( )( ) ( )
dTTx..Tx.Tx..
Tx.Tx..Tm
∫
++++
+−+−−−
−−
2983253
253
10035191008010562177
102201002613
= ( )dTTx.Tx..Tm
∫ −− −+298
253 10140105672740
= [ ]Tm298Tx.Tx.T. 1523 10140107832740 −− ++
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 2/11
223970 = 40.27 (Tm – 298) + 3.78 x 10-3 (Tm2 – 2982) + 0.14 x 105
−
298
11
Tm
Neglecting Tm-1
223970 = 3.78 x 10-3 Tm2 + 40.27 Tm – 12383
3.78 x 10-3 Tm2 + 40.27 Tm – 236353 = 0
Tm = 4207 K
Maximum temperature = 4207 – 273 = 3934ºC
The enthalpy changes for the following reactions are as follows:
2B + 2 H2 + 3 O2 + aq = 2 H3BO3 (dil solution) ΔHº298 = - 512.8 kcal
B2O3 + 3 H2O (l) + aq = 2 H3BO3 (dil solution) ΔHº298 = - 4.12 kcalH2 + ½ O2 = H2O ΔHº298 = - 68.73 kcal
I (b) Calculate the standard heat of formation of B2O3 in terms of per mole of B2O3,
and per gram of B2O3. Atomic weight of B and O are 10.82 and 16.0 respectively.
Ans: 2B + 2 H2 + 3 O2 + aq = 2 H3BO3 (dil solution) ΔHº298 = - 512.8 kcal
B2O3 + 3 H2O (l) + aq = 2 H3BO3 (dil solution) ΔHº298 = - 4.12 kcal
2B + 3 H2 + 3 O2 + = 2BO3 ΔHº298 = - 508.68 kcal
3H2 + 3/2O2 = 3H2O ΔHº298 = - 206.19 kcal
2B + 3/2O2 = B2O3
ΔHº298 = - 302.49 kcal
Relative molecular mass of B2O3 = 2 x 10.82 + 16 x 3= 69.64 gm/mole
Standard ht of formation of B2O3 = - 302.49 Kcal/mole
= - gm/Kcal.
.
6469
49302
= - 4.3436 Kcal/gm
2 (a) Calculate the entropy change of the system and surroundings for the
isothermal freezing of one mole of super cooled liquid silver at 850ºC, when the
surroundings are also at the same temperature.
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 3/11
Heat of fusion at the melting point of 1234ºK is 2690 cal/mole.
Cp for solid silver is 5.09 + 2.04 x 10 -3T cal/deg/mole and liquid copper is 7.3
cal/deg/mole.
{Cu}850 + 273 = 1123 <Cu>1123
ΔSsys = ?, ΔSsyr = ?
ΔFfus = 2690 cal/mole , Tfus = 1234K
Cp(s) = 5.09 + 2.04x10-3T , Cp(l) = 7.3 cal/deg/mole
Ans: {Cu}1123 <Cu>1123 ΔS1 = ∫ 1124
1123T
dTCpl
{Cu}1124 <Cu>1124 ΔS2 =t
t
T
∆Η
<Cu>1124 <Cu>1123 ΔS3 = dTCps∫ 1123
1124
{Cu}1123 <Cu>1124
ΔSsys = ΔS1+ ΔS2 +ΔS3 =
( )dT
T
Tx..dT
T
.∫ ∫
−++
−+
1123
1234
31234
1123
10042095
1234
269037
= ( )1234112310021
1234
1123095
1234
2690
1123
123437 3 −++− −x.ln.ln.
= 0.688 – 2.1799 – 0.479769 – 0.11322= - 2.084789
∫ ∫ −++−=∆Η =∆Η −1234
1123
1123
1234
310042095269037 TdTx..dT.syssur
=7.3(1234-1123)-2690+5.09(1123-1234)+1.02x10-3(11232-12342)
= 810.3-2690-564.99-266.859
= -2711.549 cal
deg/cal..THSsys
sur 1973621234
5492711 +=+=∆−=∆
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 4/11
0847892197362 ..SSS sursystotal −+=∆+∆=∆
= 0.1125769 cal/deg
2 (b) Calculate the standard enthalpy and entropy change at 298 K for the
following reaction
2<Cu> + ½ O2 = <Cu2O> ΔGº = -400,500 – 3.92T log T + 29.5 T cal.
Ans: 2<Cu> + ½ O2 = <Cu2O>
ΔGº = -400,500 – 3.92T log T + 29.5 T cal
529923500400
.Tlog.T
,
T
G+−−=
∆
T.T
,
T
T/G 1
7021
5004002 −=∂
∆∂
T
.
T
,
T
702150040022
−=∆Η
−
T., 7021500400 +−=∆Η
= - 400,500 + 1.702x298
= - 400,500+507
= - 399993 cal
= - 399.993Kcal
52970217021 .Tln..T
G+−−=
∂∆∂
Tln..S 702179827 −=∆
298702179827298 ln..S −=∆
= - 18.10 cal/ deg
3.(a) The melting point of gallium is 303K at 1atm. The densities of solid and
liquid gallium are 5.885 g/cc and 6.08 g/cc. the heat of fusion of gallium is 18.5
cal/g. Calculate the change in melting point of gallium for an increase of pressure of
1 atm.
Ans: ( )sl
fus
V V TdT
dP
−∆Η
=
Let atomic wt. Of gallium=x
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 5/11
ρ
−ρ
×=
sl
xx
.x.
dT
dP
303
29341518
,cc/g.,cc/g. sl 8855086 =ρρ1cal=41.293cc atm
dP=1atm, dT=?
−
×=
8855086303
29341518
.
x
.
x
.x.
dT
dP
= -462.7atm/deg
atmdeg/x.dP
dT 310162 −−=
dT= - 2.16x10-3 deg at dP= 1 atm
∴melting point of gallium will be decreased by 2.16x10-3 deg
3.(b) In an investigation for the thermodynamic properties of a managanese, the
following heat contents were determined:
Hº700 -Hº298 = 2895cal/g-atom
Hº1000 -Hº298 = 2895cal/g-atom
Find applications suitable equation for
298HHT − and also for Cp as
function of temperature in the form (a+ bT). Assume that no structural
transformation takes place in the given temperature range.
Ans: atomg/calH −=−Η 2895298700
( )
700
298
2
700
298
298700
2981000
22895
5450
+=
+=−
+=−=−Η
∫
bTaT
bTaHH
bTaCp
atomg/calH
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 6/11
( ) ( )
( ) ( )
( ) ( )
( ) ( )
761753325451087831
761753108783132545
2982
107566329832545
2982
298
32545
107566321
276357649
4555987025450
29810002
2981000
127499
2005984022895
2987002
2987002895
23
23
22
3
22
298
3
22
2981000
22
.T.Tx.
.Tx.T.
Tx.
T.
T b
TaHH
.a
x. b)(x)(
)......(........... ba
ba
baHH
).......(........... ba
ba
ba
T
−+=
−+=
−+−=
−+−=−∴
=
=⇒
=+
+=
−+−=−
=+
+=
−+−=
−
−
−
−
4.(a) Calculate the vaccum needed for obtaining molybdenum metal according to
the reaction
MoS2 = Mo + S2 at 800ºC and 1000ºC.
MoS2 + 2H2 = Mo + 2H2S; K 1
2H2S = 2H2 + S2; K 2
At temperature 800ºC K 1 is 7.3x10-6 and K 2 is 2.2x10-4 and at temperature
1000ºC K 1 is 1.439x10-3 and K 2 is 5.6x 10-3.
Solution
MoS2 + 2H2 = Mo + 2H2S , K 1
2H2S = 2H2 + S2 , K 2
MoS2 = Mo + S2, K = K 1K 2
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 7/11
22
2s
MoS
sMoP
a
paK ==
at 800C K 1 = 7.3x10-6, K 2 = 2.2x10-4
K = K 1K 2 = 7.3x10-6
x 2.2x10-4
K = Ps2 = 1.606x10-9
at 1000C K 1 = 1.439x10-3, K 2 = 5.6x10-3
K = K 1K 2 = 1.439x10-3 x 5.6x10-3
K = Ps2 = 8.0584x10-6
4.(b) Calculate the mean of vaporization of palladium and vapor pressure at
1568C from the following vapor pressure data :7.516x10-7
mmHg at temperature1314C and 1.164x10-6mmHg at 1351C.
Ans: ΔHv = ?, T = 1568+273 = 1814K → P = ?
T1= 1341+ 273 = 1597K, p1= 7.516x10-7mmHg
T2= 1351+ 273 = 1624K, p2= 1.614x10-6mmHg
4
7
7
6
121
2
103046
731986
1597
1
1841
1
9871
145871
105167
145871
15971
16241
9871105167106141
11
−
−
−
−
=
=
−
−=
=∆
−∆−=
−
∆−=
x.P
.
.x.
Pln
calH
.H
x.x.ln
TTR
H
P
Pln
v
v
v
5.(a) Determine the lowest temperature at which copper oxide (Cu2O)can
dissociate in a vaccum of 10-5mmHg.
Ans: Cu2O(s) = 2Cu(s) + 1/2 O2 ΔG = 40500+3.92T log T – 29.5T
Solution
Cu2O(s) = 2Cu(s) +1/2 O2
ΔG = 40500 + 3.92T log T -29.5T
21
2
2
221
2 5754 oOCu
Cuo PlogT.a
a.PlnRTG −=−=∆
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 8/11
In a vaccum of 10-5mmHg, taking Po2 in air as 0.2 atm
( )
092314940500
61952992340500
6191063525754
106352760
11020
21
9
952
=+−=−+
=−=∆
==
−
−−
ddd
o
TlogT.T.
T..TlogT.
T.x.logT.G
atmx.xx.P
T 500 1000
Eqn 21240 3160
by graphically→
The lowest temperature = 1085 K
5.(b) Calculate the equilibrium constant an equilibrium partial pressure of oxygen
for the reaction Zr + O2 = Zr O2 ΔG = 259940 + 2.33T logT –
59.12T
at 2000K. Also predict the possibility of decomposing a pure zirconia crucible
under a vaccum of 10-5mmHg.
Zr + O2 = Zr O2 ΔG = 259940 + 2.33T logT – 59.12T
ΔG = 259940 + 2.33 x 2000 log 2000 – 59.12 x 20000
- RT ln K = 156885
lefttoRightactionReK Q
PQ
mmHgx.k
P
PP.a
aK
x.K
.x.
K ln
O
O
OOZr
ZrO
∴⟩
==
==
==
=
−=−
=
−
5
2
17
2
22
2
18
101
10385811
1
102177
473920009871
156885
Zirconia crucible will be decomposed.
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 9/11
6.(a) In separate experiments, pure nitrogen at atmospheric pressure is passed
over either mercury or a mercury-thallium amalgam(68.4 atom percent thallium).
At temperature less than 100C the vapor pressure of thallium is negligible, relative
to that of mercury. The flow rate of nitrogen is controlled such that the gas is just
saturated with mercury vapor as it passes over the pure mercury or the amalgam.
The vapor carried over in the gas stream is condensed in a cold trapped an
weighted. In experiments with the samples at 26 C, the weight of mercury trapped
from the pure mercury an the amalgam were respectively 2.20 and 0.75mg per
hundred liter of nitrogen, the nitrogen volume being measured at 20 C and 1
atmosphere pressure. Assuming that equilibrium is continuously maintained over
the samples, calculate the partial pressure of mercury over the amalgam and the
activity coefficient of mercury in the amalgam at 26 C. (atomic weight of Hg =
200.6 g / mole)
Ans: Hg(pure,l)=Hg(g,in N2)
K P=HgpureHg
Hg
a
ρ………….(1)
= PHg(pure Hg)Hg(l,amalgam)=Hg(g,in N2)
K P=amlgamaHg
Hg
a
P
…………….(2)
Assuming Hg vapor behave ideally, (1) = (2)
PHg(pureHg)=
amlgamaHg
Hg
a
p
AHg=)pureHg(Hg
)amlgama(Hg
P
P…………….(3)
Volume of (100liter at 20C) at 26 C = literx 102273
299100 =
.NTPatcc..x.
.occupiesmgHg.,mole/g.MHg 239022
6200
422226200 =
=
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 10/11
Catccx. 26273
2992390=
= 0.262 cc at 26 C
∴ partial pressure of Hg over pure Hg = 7601020002620 x.
mmHgx.PHg40 10519 −=
at NTP 0.75mg Hg occupies = cc..x.
.0820750
6200
422=
at 26 C 0.75mg Hg occupies =0.082x cc.0890273
299=
∴ partial pressure of Hg over amalgam = 760102000
0890 x.
PHg=6.65x10-4mmHg
(3)
0813160
340
34010519
106564
4
0
..
.
N
a
.x.
x.
P
Pa
Hg
HgHg
Hg
HgHg
===ρ
=== −
−
6.(b) Chromium plates are bright annealed at 1000K in a wet hydrogen
atmosphere. The pressure of wet hydrogen is 1atm. (i) Calculate the permissible
water content in the hydrogen if there is to be no oxidation at 1000K (ii) Will
annealed chromium plates be oxidized when cooled to 500K in the furnace
atmosphere, as calculated in (i)? neglect the possibility of dissolution of hydrogen
in chromium.
Given: 2<Cr>+3(H2O) = <Cr 2O3>+3(H2) ΔGº= - 91050+22.8Tcal.
Ans: 2<Cr>+3(H2O) = <Cr 2O3>+3(H2) ΔGº= - 91050+22.8Tcal
68250
100082291050
82291050
1000
−=−+−=∆
+−=∆
K lnRT
x.G
T.GT
7/29/2019 MEt04011MetThermodynamicsI(1)
http://slidepdf.com/reader/full/met04011metthermodynamicsi1 11/11
RighttoLeft.QK
K Q
x.K ln
K lnRT
x.G
x.P
.P
P
.PP
x.P
PK
.K ln
OH
OH
OH
OH
H
OH
H
>==
=
−=−+−=∆
=
=−
=
=
=
=
−
16533
5009871
9650
9650
50082291050
10061
27938361
2793836
102658
34834
500
500
5
2
2
2
2
2
14
3
2
21000
Cr. Plate will be oxidized at 500 ºK