4. Brayton, Ericsson, and Space Powercontents.kocw.net/KOCW/document/2015/chungnam/par… · ·...
Transcript of 4. Brayton, Ericsson, and Space Powercontents.kocw.net/KOCW/document/2015/chungnam/par… · ·...
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에너지변환특론Advanced Energy Conversion
Chapter 4. Brayton, Ericsson, and Rankin cycles
교수 박 수 한
Fall semester, 2014
CNU Engine Research Lab.
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브레이튼사이클 (Brayton cycle)
가스터빈기관의열역학적이상사이클로주로항공기추진이나전력생산에응용됨
1 2 (압축기): 가역단열압축 (reversible adiabatic compression, isentropic compression)
2 3 (연소실): 정압가열 (const.‐pr. heat addition)
3 4 (터빈) : 가역단열팽창 (reversible adiabatic expansion, isentropic expansion)
4 1 (배기): 정압방열 (const.‐pr. heat rejection)
Open‐cycle gas‐turbine engine. Closed‐cycle gas‐turbine engine.
Ideal Brayton cycle
브레이튼 사이클
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브레이튼사이클해석
열효율 (thermal efficiency)
)( 23P23in23 TTChhqq
)/(
)/(
)(
)(,
1TTT
1TTT1
TTC
TTC1
q
q1
232
141
23P
14P
in
outOttoth
)( 14P14out41 TTChhqq
)( 12P12c12 TTChhww
)( 43P43t34 TTChhww
4
3k
1k
4
3k
1k
1
2
1
2
T
T
P
P
P
P
T
T
ratiopressureP
P
P
Pr
4
3
1
2P ;
k1kP
Braytonthr
11
/)(, 0%
20%
40%
60%
80%
0 5 10 15 20 25
Thermal efficiency (%)
Pressure ratio, rP
k = 1.4
Typical pressureratios
for gas turbineengines
브레이튼사이클
CNU Engine Research Lab.
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사이클일 (cycle work)
사이클최고온도는터빈블레이드가견딜수있는최대온도로제한되며, 이에따라사이클압력비도결정됨
사이클최고온도(Tmax )와최저온도(Tmin )사이에서압력비, rP에따라브레이튼사이클의정미일은증가하지만,
rP = (Tmax/Tmin )k/2(k‐1) 에서최대에도달한후감소함
k1kP
k
1k
1
23max r
P
PTT /)(
)()(, 12P43PctBraytonnet TTCTTCwww
1
T
TT
T
T1TC
1
21
3
43P
1P
PT
P
P1TC
k1k
1
21
k1k
3
43P
/)(/)(
1rTr
11TCw k1k
P1
k1k
P3PBraytonnet
/)(/)(
,
브레이튼사이클
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역일비(rbw, back work ratio): 터빈일에대한압축기일의비
사이클일 (cycle work)
브레이튼사이클최대일
0rk
1kTr
k
1kT
dr
w 1k
1k
P1
1k
1k
P3P
Braytonnet
,
1k
1k
P1
1k
1k
P3 rk
1kTr
k
1kT
k1k2P
1
3
min
max rT
T
T
T /)(
)( 1k2
k
min
maxP
T
Tr
k1k
P
k
1k
1
23max r
P
PTT /)(
turbine
comprwssorbw
w
wr
브레이튼사이클
CNU Engine Research Lab.
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가스터빈의발달
터빈입구온도의증가 : 소재및코팅기술, 냉각기술
터보기계효율증가 : 터빈(turbine), 압축기(compressor)
기본사이클개선 : 중간냉각(intercooling), 재생(regeneration), 재열(reheating)
실제가스터빈사이클과의차이
터빈, 압축기의비가역성, 압력손실, 단열손실등
a21
s21compressor
hh
hh
s43
a43turbine
hh
hh
브레이튼사이클
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브레이튼 사이클로 작동하는 발전소가 압력비 8을 가지고 있다. 압축기와 터빈 입구에서 가스 온도는 각각 300 K,
1,300 K일때,공기표준사이클로가정할때압축기와터빈의출구에서가스온도,역일비및열효율을구하여라.
Example: 이상브레이튼사이클
Assumption : 1. Steady‐state process
2. Air‐standard cycle
3. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)4. Specific heat is not constant (CP const., k const. )
Solve : T
s
2
1
3
4
dP = 0
dP = 0
qin
qout
wt
wc
1,300 K
300 K
rP = 0
K300T1 @from Table A–17 :
3861P
kgkJ19300h
1r
1
.
/.
P1
2
1r
2r rP
P
P
P 091183861rPP P1r2r ..
from Table A–17 : K540T2
kgkJ35544h2 /.
브레이튼사이클
CNU Engine Research Lab.
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kgkJ03800h3543PK780
kgkJ18778h2739PK760
r
r
/.,.
/.,.@
Solve :
K3001T3 ,@ from Table A–17 : 9330PkgkJ973951h 3r3 .,/.,
P3
4
3r
4r
r
1
P
P
P
P 3641
8
9330
r
PP
P
3r4r .
.
from Table A–17 :
K77076076078027393543
27393641T4
)()..(
)..(
kgkJ3778918778187780380027393543
27393641h4 /..)..(
)..(
)..(
Back work ratio, rbw :
kgkJ162441930035544hhw 12c /...
kgkJ660637789973951hhw 43t /...,
%).(..
.3404030
6606
16244
w
wr
t
cbw
브레이튼사이클
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Thermal efficiency :
kgkJ6285135544973951hhq 23in /...,
Solve :
kgkJ184891930037789hhq 14out /...
%).(..
..6424260
62851
162446606
q
ww
q
w
in
ct
in
netth
%).(..
.6424260
62851
184891
q
q1
in
outth
%).(..)(././)(
84444808
11
r
11cf
4140k1kP
th
브레이튼사이클
CNU Engine Research Lab.
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압축기효율이 80 %이고,터빈효율이 85 %라고가정할때,예제 9‐5에서다룬가스터빈사이클의역일비,열효율및
가스터빈출구온도를구하여라.
Example: 실제가스터빈사이클
Solve :
T
s
2s
1
3
4s
qin
qout
1,300 K
300 K
4a2a
For compressor :
a
sc
w
w
kgkJ230580
16244ww
c
sactc /.
.
..,
kgkJ162441930035544hhw 12thc /....,
kgkJ2305hhw 1a2actc /..,
kgkJ39605230519300whh actc1a2 /....,
kgkJ02607hK600
kgkJ52596hK590
/.
/.@
from Table A–17 :
K5985905906005259602607
5259639605T a2
)()..(
)..(
브레이튼사이클
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Solve :
For turbine :
s
at
w
w
kgkJ615156606850ww stactt /....,
%).(..
.
.,
.,., 2595920
61515
2305
w
wr
actt
actcactbw %).(. 3404030
w
wr
t
cbw
kgkJ660637789973951hhw 43t /...,
kgkJ61515hhw a43actt /..,
kgkJ3688061515973951whh actt3a4 /...,.,
kgkJ27888hK860
kgkJ08866hK840
/.
/.@
from Table A–17 :
K8538208408600886627888
0886636880T a4
)()..(
)..(
kgkJ5879039605973951hhq a23actin /...,.,
kgkJ41210230561515www actcacttactnet /....,.,.,
%).(..
.
.,
.,., 6262660
58790
41210
q
w
actin
actnetactth %).(. 6424260
q
w
in
netth
브레이튼사이클
CNU Engine Research Lab.
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재생브레이튼사이클 (regenerative Brayton cycle)
터빈출구의배기열을이용하여연소기입구의압축공기를가열하는재생기(regenerator)또는회수열교환기
(recuperate)를설치한브레이튼사이클
배기가스에너지의일부가사이클공급열에너지로재사용되기때문에동일출력에대한열효율이증가함
재생브레이튼사이클
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CNU Engine Research Lab.
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재생브레이튼사이클해석
2
1
3
45’
56
T
s
qin
qout
qregen
qsaved = qregen
25actregen hhq .,
2425maxregen hhhhq ,
‐재생열 (regeneration heat) :
‐재생기의유용도 (effectiveness of regenerator) :
24
25regen
hh
hh
)( 45 TT
‐공급열, 방열량및정미일 :
53in hhq
)()( 1253net hhhhw
1216out hhhhq
)(%, 4545regen TTorhh100if
재생브레이튼사이클
CNU Engine Research Lab.
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재생브레이튼사이클해석
34
12
3
1
43
12
TT1
1TT
T
T1
TT
TT1
/
/
)(
)()()()(,
43P
12P43P
43
1243
in
netB Regen.th
TTC
TTCTTC
hh
hh4h
q
w
‐이론열효율 (for regen = 100%) :
2
1
3
45
6
T
s
qin
qout
qregen
qsaved = qregen
k1kP
k1k
1
2
1
2 rP
P
T
T /)(/)(
k1k
P
k1k
3
4
3
4
r
1
P
P
T
T/)(/)(
k1kP
3
1K1k
P
k1kP
3
1 rT
T1
r11
1r
T
T1 /)(
/)(
/)(
)/(
ratiotempT
T
T
Tr
min
max
1
3T .;
k1kP
TBregenth r
r
11 /)(
., 0%
20%
40%
60%
80%
0 5 10 15 20 25
Thermal efficiency (%)
Pressure ratio, rP
k = 1.4
rT = 5
rT = 4
rT = 3
With regeneration
Without regeneration
재생브레이튼사이클
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예제 9‐6에서다룬가스터빈기관에유용도 80 %의재생기가설치할경우의열효율을구하여라.
Example:실제재생가스터빈사이클
Solve :
kgkJ657037825973951hhq 53in /...,
T
s
2s
1
3
4s
qin1,300 K
300 K
4a2a
qsaved = qregen
5
3960536880
39605h
hh
hh 5
a2a4
a25regen
..
.
kgkJ3782539605368808039605
hhhh a2a4regena25
/.)..(..
)(
%).(..
.
.,
.,., 6262660
58790
41210
q
w
actin
actnecactth
%).(..
., 9363690
6570
41210
q
w
in
netregenth
재생브레이튼사이클
CNU Engine Research Lab.
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재열브레이튼사이클 (Brayton cycle with reheating)
터빈출력을증가시키기위해기체를단계적으로팽창시키고그사이에기체를재열시키는브레이튼사이클
Wnet
CompressorTurbine 1
(HP)
Combustionchamber
Reheater
Turbine 2(LP)
1
2 3 a b
4
2
1
3
4a
T
s
qin
qout
qin bTb T3
)()(,, 4ba3LtHtt hhhhwww
)()(
)()()(,
ab23
124ba3
in
netB Reh.th
4h4h
4hhh4h
q
w
재열브레이튼사이클
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CNU Engine Research Lab.
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재열브레이튼사이클 (Brayton cycle with reheating)
터빈일을 최대로하는중간압력
2
1
3
4a
T
s
qin
qout
bTb = T3
)()(,, 4ba3LtHtt hhhhwww
b
4b
3
a3P
T
T1T
T
T1TC
k1k
b
43
k1k
3
a3P
P
P1T
P
P1TC
/)(/)(
b3 TT
iba PPP
0Pk
1kPP
k
1k
P
1TC
dP
w 1k
1k
ik
1k
4
1k
1k
i
k1k
33P
i
reh
)()(/)(
.
k
1k
i
4k
1k
3
i
P
P
P
P
4
b
a
3
P
P
P
P
재열브레이튼사이클
CNU Engine Research Lab.
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중간냉각브레이튼사이클 (Brayton cycle with intercooling)
압축일을감소시키기위해중간냉각이있는다단압축기를사용하는브레이튼사이클
2
1
3
4
a
T
s
qin
qoutb qout
43t hhw )()(,, b21aHcLcc hhhhwww
23in hhq )()( ba14out hhhhq
)( bab
2
1
a PPP
P
P
P
Compressor 1(LP)
Wnet
Combustionchamber
Turbine
Intercooler
Compressor 2(HP)
1 b
2 3
4a
중간냉각브레이튼사이클
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CNU Engine Research Lab.
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중간냉각재열재생브레이튼사이클 (Brayton cycle with intercooling, reheating, and regeneration)
4
3
10
5
2
T
s
qin
qregen
qsaved = qregen
qout1
6 8
97
)()(
)()(,
7856
32110
in
outB regen.‐ehrth
4h4h
4h4h
q
q1
3
4
1
2
P
P
P
P
9
8
7
6
P
P
P
P
6491 PPPP ,
중간냉각재열재생브레이튼사이클
CNU Engine Research Lab.
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2단압축 2단팽창이상가스터빈사이클이전체압력비 8을가지고있다.공기는압축기의각단에 300 K,터빈의각
단에 1,300 K으로들어간다.재생기가없는경우와유용도 100 %의재생기가있는경우에대해이가스터빈사이클의
역일비및열효율을구하여라.
Example: 재열및중간냉각가스터빈
Assumption : 1. Steady‐state process
2. Air‐standard cycle
3. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)4. Specific heat is not constant (CV const., k const. )
Solve :
4
3
10
5
2
T
s
qin
qregen
qsaved = qregen
qout1
6 8
97
1,300 K
300 K
Pressure ratio for minimum compression work :
8328P
P
P
P
3
4
1
2 .
8PP8PPPP 111412 8PP 14 /
Pressure ratio for maximum turbine work :
8328P
P
P
P
9
8
7
6 . 8P8PPPPP 666967 /)/(
중간냉각재열재생브레이튼사이클
11
CNU Engine Research Lab.
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923838618PP 1r2r ..
Solve :
from Table A–17 : 3861PkgkJ19300h 1r1 .,/. K300T1 @
kgkJ12411h1534PK410
kgkJ98400h8063PK400
r
r
/..
/..@
from Table A–17 :
K34034001080631534
8063923T2 .
)..(
)..(
kgkJ3140498400984001241180631534
8063923h2 /..)..(
)..(
)..(
from Table A–17 : 9330PkgkJ973951h 6r6 .,/., K3001T6 ,@
11789330P8P 7r7r /./
kgkJ890681h4123PK0201
kgkJ040461h0114PK0001
r
r
/.,.,
/.,.,@
from Table A–17 :
K400610001201144123
114117T7 .,,
).(
)(
kgkJ3305310404610404618906811144123
114117h7 /.,.,).,.,(
).(
)(
중간냉각재열재생브레이튼사이클
CNU Engine Research Lab.
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Solve :
Compression & turbine work :
kgkJ2420819300314042hh2w 12c /.)..()(
kgkJ286853305319739512hh2w 76t /.).,.,()(
4
3
10
5
2
T
s
qprimary
qregen
qsaved = qregen
qout1
6 8
97
1,300 K
300 K
qreheatkgkJ044772420828685www ctnet /...
Heat addition & rejection :
)()( 7846reheatprimaryin hhhhqqq
kgkJ3334133053197395131404973951 /.,).,.,()..,(
0264931404330531hhq 45regen ...,
kgkJ286850264933341qqq regeninregenin /...,,
%).(..
.4303040
28685
24208
w
wr
t
cbw
%).(..,
., 8353580
33341
04477
q
w
in
netreheatth %).(.
.
.,, 6696960
28685
04477regenrehth
중간냉각재열재생브레이튼사이클
12
CNU Engine Research Lab.
CNU Engine Research Lab.
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랭킨사이클 (Rankine cycle)
증기동력사이클의열역학적이상사이클
1 2 (펌프) : 가역단열(등엔트로피)압축 (reversible adiabatic compression, isentropic compression)
2 3 (보일러) : 정압가열(연소) (const.‐pr. heat addition)
3 4 (터빈) : 가역단열(등엔트로피)팽창 (reversible adiabatic expansion, isentropic expansion)
4 1 (응축기) : 정압방열 (const.‐or. heat rejection)
T
s
2
1
3
4
qin
qout
wpump
wturbine
랭킨사이클
13
CNU Engine Research Lab.
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랭킨사이클해석
: 가역단열압축 (Pump)
: 정압가열 (Boiler)
2323in hhqq
121221
221212 wzzgvv
2
1hhq )()()(
T
s
2
1
3
4
qin
qout
wpump
wturbine
1212p hhww
)()( 21121p vvPPvw
1Pf1 hh @
1Pf1 vv @
: 가역단열팽창 (Turbine)
4334t hhww
: 정압방열 (Condenser)
1441out hhwq
23
14
in
outRth
hh
hh1
q
q1
,
23
1243
in
netRth
hh
hhhh
q
w
)()(
,
랭킨사이클
CNU Engine Research Lab.
29
랭킨사이클로작동하는증기원동소가있다. 수증기가 3 MPa, 350 C 상태로터빈에들어가서 75 kPa의압력으로
응축기에서응축된다. 이사이클의열효율을구하여라.
Example:이상랭킨사이클
Assumption : 1. Steady‐state process
2. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)
Solve :
kPa75P1 @from Table A–5 :
kgm0010370vv
kgkJ44384hh
3f1
f1
/.
/.
P2 = 3 MPa
P4 = 75 kPa
P3 = 3 MPa
T3 = 350 C
P1 = 75 kPa
kgkJ0337500030010370PPvw 121p /.),(.)(
kgkJ4738703344384whh p12 /...
KkgkJ7456sC350T
kgkJ11163hMPa3P
33
33
/.
/.,@from Table A–6 :
랭킨사이클
14
CNU Engine Research Lab.
30
Solve :
from Table A–5 : @ P4 = 75 kPa, sg = 7.4558 kJ/kgK > s4 = s3 = 6.745 kJ/kgK Water vapor
886024266
213217456
s
ssx
fg
f44 .
.
..
T
s
2
1
3
4
qin
qout
wpump
wturbine
kgkJ02782hkgkJ44384h
KkgkJ24266sKkgkJ21321skPa75P
fgf
fgf4
/.,,/.
/.,/.@
kgkJ8402202782886044384hxhh fg4f4 /.,).,.(.
Heat and Work :
kgkJ672824738711163hhq 23in /.,..,
kgkJ401824438484022hhq 14out /.,..,
kgkJ37138402211163hhw 43t /..,.,
kgkJ0334438447387hhw 12c /...
Thermal efficiency :%).(.
.,
.., 0262600
67282
0333713
q
w
in
netRth
랭킨사이클
CNU Engine Research Lab.
31
실제증기사이클과이상증기사이클의차이
보일러와응축기에서배관내에서유체마찰로인한압력강하가존재함
이러한압력강하를보상하기위해실제사이클에서펌프는이상사이클에서필요한압력보다높게가압해야함
또한터빈과펌프는마찰, 주위로의열손실등으로인한비가역성이존재함
1a2
1s2
a
sp
hh
hh
w
w
s43
a43
s
at
hh
hh
w
w
랭킨사이클
15
CNU Engine Research Lab.
32
증기원동소가아래그림에나타낸사이클로작동한다. 펌프의단열효율이 85 %, 터빈의단열효율이 87 %일때이
사이클의열효율과질량유량이 15 kg/s일때정미출력을구하여라.
Example:실제증기동력사이클
For pump :
.
,
act
isenpp
w
w
P2 = 16 MPa
P5 = 15 MPa
T3 = 600 C
P1 = 9 kPa
T1 = 8 C
p = 0.85
P3 = 15.9 MPa
T1 = 35 C
P4 = 15.2 MPa
T4 = 625 C
P6 = 10 kPat = 0.87
Assumption : 1. Steady‐state process
2. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)
Solve :
kgkJ019850
9000160010090
850
PPvww 121
c
isenpactp /.
.
),(.
.
)(,.,
from Table A–5 :
kgm0010100vkPa10P
kgm0010080vkPa57P
3f
3f
/.,@
/.,.@
kgm0010090
0010080001008000101005710
579v
3
1
/.
.)..().(
).(
랭킨사이클
CNU Engine Research Lab.
33
Solve :
For turbine :
KkgkJ67966sC600T
kgkJ15833hMPa15P
55
55
/.
/.,@from Table A–6 :
from Table A–5 : @ P4 = 10 kPa, sg = 8.1488 kJ/kgK > s4 = s3 = 6.6796 kJ/kgK Water vapor
804049967
6492067966
s
ssx
fg
f66 .
.
..
kgkJ13922hkgkJ81191h
KkgkJ49967sKkgkJ64920skPa10P
fgf
fgf6
/.,,/.
/.,/.@
kgkJ1115213922804081191hxhh fg6f6 /.,).,.(.
isen
actt
w
w . kgkJ227711115215833870hh870ww s65isenttactt /.,).,.,(.)(.,.,
랭킨사이클
16
CNU Engine Research Lab.
34
Solve :
For boiler :
kgkJ9397hkgkJ77180hMPa15P C20C40 /.,/.@ @@ from Table A–7 :
kgkJ116093979397771802040
2035h3 /..)..(
)(
)(
kgkJ17123hkgkJ15833hMPa15P C650C600 /.,,/.,@ @@ from Table A–6 :
kgkJ66473158331583317123600650
600625h4 /.,.,).,.,(
)(
)(
Heat and Work :
kgkJ54873116066473hhq 34in /.,..,
Thermal efficiency :
%).(..,
.,, 1363610
54873
22581
q
w
in
netRth
kgkJ2258101922771www ctnet /.,..,
MW918kgkJ22581skg15wmW netnet ./.,/
랭킨사이클
CNU Engine Research Lab.
35
응축기압력을낮추는경우
응축기작동압력을낮추면방출되는열이방출되는온도가낮아지고, 정미일이증가되어열효율이증가함
그러나, 터빈출구에서수분함유량이증가(건도감소)되어터빈효율이감소하고터빈날개의부식문제가생김
사이클최고온도를높이는경우
공급열량도증가하나정미일의증가량이더크기때문에사이클의열효율은증가함
그러나, 터빈재료의기계적인성질로인하여사이클최고온도가제한됨 (약 620 C)
Increase in Wnet
Increase in Wnet
:..
..
avgH
avgLth
T
T1
:.. avgLT
corrosionx4 :
:..
..
avgH
avgLth
T
T1
:.. avgHT
4x
랭킨사이클의열효율향상방법
17
CNU Engine Research Lab.
36
보일러압력을증가시키는경우
보일러 작동압력을증가시키면, 전체적으로사이클의열효율은증가하나, 터빈출구에서수분함유량이
증가(건도감소)함
Increase
in Wnet
Decrease
in Wnet
:..
..
avgH
avgLth
T
T1
:.. avgHT
4x
랭킨사이클의열효율향상방법
CNU Engine Research Lab.
37
이상랭킨사이클로작동하는증기원동소가있다. 수증기가 3 MPa, 350 C의상태로터빈을들어가서 10 kPa의
압력으로응축기에서응축될때, 이원동소의열효율을구하여라. 또한증기가 3 MPa, 600 C로과열될때와 15 MPa,
600 C 로과열될때의열효을구하여라.
Example: 보일러의압력과온도가열효율에미치는영향
Solve :
T
s
2
1
3
4
qin
qout
3
4
kgkJ0231000030010100PPvw 121p /.),(.)(
from Table A–5 : kgkJ81191hhkgm0010100vvkPa10P f13
f1 /.,/.,@
kgkJ8319402381191whh p12 /...
KkgkJ7456sC350T
kgkJ11163hMPa3P
33
33
/.
/.,@from Table A–6 :
KkgkJ51037sC600T
kgkJ86823hMPa3P
33
33
/.
/.,@
kgkJ141510000150010100PPvw 121p /.),(.)(
kgkJ95206141581191whh p12 /...
랭킨사이클의열효율향상방법
18
CNU Engine Research Lab.
38
Solve :
KkgkJ67966sC600T
kgkJ15833hMPa15P
33
33
/.
/.,@from Table A–6 :
from Table A–5 : @ P4 = 10 kPa, sg = 8.1488 kJ/kgK > s4 = s3 = 6.7450 kJ/kgK Water vapor
sg = 8.1488 kJ/kgK > s4 = s3 = 7.5103 kJ/kgK Water vapor
sg = 8.1488 kJ/kgK > s4 = s3 = 6.6796 kJ/kgK Water vapor
8128049967
649207456
s
ssx
fg
f64 .
.
..
kgkJ13922hkgkJ81191h
KkgkJ49967sKkgkJ64920skPa10P
fgf
fgf6
/.,,/.
/.,/.@
kgkJ11362139228128081191h4 /.,).,.(.
from Table A–5 :
8041049967
6492067966
s
ssx
fg
f64 .
.
..
9149049967
6492051037
s
ssx
fg
f64 .
.
..
kgkJ33802139229149081191h4 /.,).,.(.
kgkJ31152139228041081191h4 /.,).,.(.
랭킨사이클의열효율향상방법
CNU Engine Research Lab.
39
Solve :
P3 = 3 MPa, T3 = 350 C : kgkJ392128319411163hhq 23in /.,..,
kgkJ394418319111362hhq 14out /.,..,
%).(..,
.,, 4333340
39212
394411
q
q1
in
outRth
P3 = 3 MPa, T3 = 600 C : kgkJ048838319486823hhq 23in /.,..,
kgkJ518828319133802hhq 14out /.,..,
%).(..,
.,, 3373730
04883
518821
q
q1
in
outRth
P3 = 15 MPa, T3 = 600 C : kgkJ237639520615833hhq 23in /.,..,
kgkJ592318319131152hhq 14out /.,..,
%).(..,
.,, 0434300
23763
592311
q
q1
in
outRth
랭킨사이클의열효율향상방법
19
CNU Engine Research Lab.
40
재열랭킨사이클 (reheat rankine cycle)
랭킨사이클의열효율을향상시키고터빈출구의수분을감소시키기위하여과열증기를 2단의터빈으로
팽창시키고두단사이의증기를재열(reheat)시키는사이클
)()( 4523reheatprimaryin hhhhqqq
)()(,, 6543LtHtt hhhhwww )()(,
4523
16reheatR
hhhh
hh1
재열랭킨사이클
CNU Engine Research Lab.
41
이상재열랭킨사이클로작동하는증기원동소가있다. 증기는 15 MPa, 600 C의압력과온도로고압터빈에
들어가서 10 kPa의압력으로응축기에서응축된다. 저압터빈출구에서증기의수분함유량이 10.4%를초과하지않을
경우, 증기가재열되는압력, 사이클의열효율을구하여라. (단증기는고압터빈의입구온도까지재열된다)
Example:이상재열랭킨사이클
Assumption : 1. Steady‐state process
2. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)
Solve :
T
s
2
1
5
6
15 MPa
3
4
10 kPa
from Table A–5 : kgm0010100vvkPa10P 3f1 /.,@
kgkJ141510000150010100PPvw 121p /.),(.)(
kgkJ95206141581191whh p12 /...
kgkJ81191hh f1 /.
KkgkJ67966sC600T
kgkJ15833hMPa15P
33
33
/.
/.,@from Table A–6 :
재열랭킨사이클
20
CNU Engine Research Lab.
42
Solve :
kgkJ13922hkgkJ81191h8960x
KkgkJ49967sKkgkJ64920skPa10P
fgf6
fgf6
/.,,/..
/.,/.@
from Table A–5 :
kgkJ1335213922896081191h6 /.,).,.(.
KkgkJ3688749967896064920s6 /.)..(.
36687ss
C600T
65
5
.
@
from Table A–6 :
kgkJ96703hKkgkJ31277s
kgkJ96743hKkgkJ37067s
MPa4MPa54
MPa4MPa4
/.,,/.
/.,,/.
@.@
@@
MPa4P5 kgkJ96743h5 /.,
67966ss
MPa4P
34
4
.
@
from Table A–6 :
kgkJ52143hKkgkJ77146s
kgkJ30933hKkgkJ58436s
C400C400
C350C350
/.,,/.
/.,,/.
@@
@@
kgkJ015533093330933521435843677146
5843667966h4 /.,.,).,.,(
)..(
)..(
K53753503504005843677146
5843667966T4 .)(
)..(
)..(
재열랭킨사이클
CNU Engine Research Lab.
43
Solve :kgkJ1896303155967439520615833hhhhq 4523in /.,)..,()..,()()(
kgkJ314328319113352hhq 16out /.,..,
%).(..,
.,, 0454500
18963
314321
q
q1
in
outReheatR
Pin, Pump = 10 kPa,
Discussion :
Pin, turbine = 15 MPa, Tin, turbine = 600 C
kgkJ237639520615833hhq 23in /.,..,
kgkJ592318319131152hhq 14out /.,..,
%).(..,
.,, 0434300
23763
592311
q
q1
in
outRth
kgkJ875213143218963qqw outinReheatnet /.,.,.,,
kgkJ745215923123763qqw outinnet /.,.,.,
8960xReheat .
8040xRankine .
재열랭킨사이클
21
CNU Engine Research Lab.
44
재생랭킨사이클 (reheat rankine cycle)
터빈에서팽창하는증기의일부를추출하여열교환기를통해보일러입구의급수온도를상승시켜사이클의
공급열량을줄임으로써열효율을향상시키는사이클
재생기(regenerator) 또는급수가열기(feedwater heater, FWH) : 급수가재생에의해가열되는장치
개방형 급수가열기 (Open feedwater heater) 밀폐형 급수가열기 (Closed feedwater heater)
재생랭킨사이클
CNU Engine Research Lab.
45
개방형 급수가열기 (open feedwater heater)
y
1 ‐ y
1
765 mmm 5
7
5
6
m
m
m
m1
5
6
m
my
5
7
m
my1
45in hhq
)()( 17out hhy1q
)()()( 7665t hhy1hhw
)()()(,, 34122p1pp hhhhy1www
)(, 1211p PPvw )(, 3432p PPvw
45
17regenR
hh
hhy11
)()(
,
)()()( 2336 hhy1hhy
26
23
hh
hhy
재생랭킨사이클
22
CNU Engine Research Lab.
46
밀폐형 급수가열기 (closed feedwater heater)
56
18regenR
hh
hhy11
)()(
,
)()()( 2937 hhy1hhy
)()( 2937
29
hhhh
hhy
y
1 ‐ y
1
재생랭킨사이클
CNU Engine Research Lab.
47
1개의개방형급수가열기를가지는이상재생랭킨사이클로작동하는증기원동소가있다. 증기는 15 MPa, 600
C의압력과온도로터빈에들어가서 10 kPa의압력으로응축기에서응축되며, 일부증기는 1.2 MPa의압력에서
터빈을떠나서개방형급수가열기로들어간다. 터빈으로부터추출된증기분율과사이클의열효율을구하여라.
Example:이상재생랭킨사이클
Assumption : 1. Steady‐state process
2. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)
Solve :
from Table A–5 : kgm0010100vvkPa10P 3f11 /.,@
kgkJ2011020010010100PPvw 1211p /.),(.)(
kgkJ0119320181191whh 1p12 /...
kgkJ81191hh f1 /.
T
s
2
1
5
7
1
3
4 6
y
1 ‐ yfrom Table A–5 : kgm0011380vvMPa21P 3
f33 /.,.@
kgkJ33798hh f3 /.
재생랭킨사이클
23
CNU Engine Research Lab.
48
Solve : kgkJ70152001000150011380PPvw 3432p /.),,(.)(
kgkJ03814701533798whh 2p34 /...
KkgkJ67966sC600T
kgkJ15833hMPa15P
55
55
/.
/.,@from Table A–6 :
67966ss
MPa21P
56
6
.
.@
from Table A–6 :
kgkJ62935hKkgkJ83136s
kgkJ18162hKkgkJ59096s
C250C250
C200C200
/.,/.
/.,,/.
@@
@@
kgkJ286021816218162629355909683136
5909667966h6 /.,.,).,.(
)..(
)..(
K42182002002505909683136
5909667966T4 .)(
)..(
)..(
8041049967
6492067966
s
ssx
fg
f77 .
.
..
kgkJ13922hkgkJ81191h67966ss
KkgkJ49967sKkgkJ64920skPa10P
fgf57
fgf6
/.,,/..
/.,/.@
kgkJ31152139228041081191h7 /.,).,.(.
from Table A–5 :
재생랭킨사이클
CNU Engine Research Lab.
49
Solve :)()()( 2336 hhy1hhy %).(.
..
..72222700
0119322860
0119333798
hh
hhy
26
23
kgkJ176920381415833hhq 45in /.,..,
kgkJ948618119131152227001hhy1q 17out /.,)..,().()()(
%).(..,
.,, 3464630
17692
948611
q
q1
in
outRegenR
Pin, Pump = 10 kPa,
Discussion :
Pin, turbine = 15 MPa, Tin, turbine = 600 C
kgkJ237639520615833hhq 23in /.,..,
kgkJ592318319131152hhq 14out /.,..,
%).(..,
.,, 0434300
23763
592311
q
q1
in
outRth
kgkJ228219486117692qqw outinRegennet /.,.,.,,
kgkJ745215923123763qqw outinnet /.,.,.,
kgkJ17692q Regenin /.,,
kgkJ23763qin /.,
재생랭킨사이클
24
CNU Engine Research Lab.
50
)()(
)()(,
6745
19regenreheatR
hhhh
hhy11
T
s
2
1
7
9
5
61
3
48
y
1 ‐ y
)()( 6745in hhhhq
)()( 19out hhy1q
)()()()( 988765t hhy1hhhhw
)()()(,, 34122p1pp hhhhy1www
)()()( 2338 hhy1hhy
28
23
hh
hhy
재열‐재생랭킨사이클 (reheat‐regenerative Rankine cycle)
재열-재생랭킨사이클
CNU Engine Research Lab.
51
1개의개방형급수가열기와 1개의밀폐형급수가열기, 1개의재열기를가지는이상재열‐재생랭킨사이클로
작동하는증기원동소가있다. 증기는 15 MPa, 600 C의압력과온도로고압터빈에들어가서 4 MPa까지팽창된후,
일부증기는밀폐형급수가열기로들어가고나머지는같은압력에서 600 C까지재열된다. 한편, 저압터빈의일부
증기는 0.5 MPa의압력에서터빈을떠나서개방형급수가열기로추출되며, 나머지는 10 kPa압력으로응축기에서
응축된다. 각터빈으로부터추출된증기분율과사이클의열효율을구하여라.
Example:이상재열‐재생랭킨사이클
Assumption : 1. Steady‐state process
2. Kinetic and potential energy changes are ignorable (KE = 0, PE = 0)
Solve :
kgm0010100vvkPa10P 3f11 /.,@
kgkJ490105000010100PPvw 1211p /.)(.)(
kgkJ319249081191whh 1p12 /...
kgkJ81191hh f1 /.
T
s
2
1
10
13
y
3
4
12z1 – y ‐ z
87
5 6
9 11
1 kg
1 ‐ y15 MPa
4 MPa
0.5 MPa
10 kPa
재열-재생랭킨사이클
25
CNU Engine Research Lab.
52
Solve :
kgm0010930vvMPa50P 3f33 /.,.@
kgkJ83350000040010930PPvw 3432p /.),(.)(
kgkJ9264383309640whh 2p34 /...
kgkJ09640hh f3 /.
kgm0012520vvMPa4P 3f66 /.,@
kgkJ78130004000150012520PPvw 6763p /.),,(.)(
kgkJ21011781340871whh 3p67 /.,..,
kgkJ40871hh f6 /.,
KkgkJ67966ssC600TMPa15P 10959 /.,@
kgkJ15833h9 /.,
52143h30933h77146s58436sMPa4P C400C350C400C35010 .,,.,,.,.,@
kgkJ015533093330933521435843677146
5843667966h10 /.,.,).,.,(
)..(
)..(
재열-재생랭킨사이클
CNU Engine Research Lab.
53
Solve :
KkgkJ37067sssC600TMPa4P 131211511 /.,@
kgkJ96743h11 /.,
60643h09612h46147s27257sMPa50P C300C250C300C25012 .,,.,,.,.,.@
kgkJ801430961209612606432725746147
2725737067h12 /.,.,).,.,(
)..(
)..(
13922h81191h49967s64920skPa10P fgffgf13 .,,.,..,@
kgkJ733521392249967
649203706781191h13 /.,.,
.
...
)()()( 45610 hhy1hhy
1766092643408714087101553
9264340871
hhhh
hhy
45610
45 .)..,().,.,(
..,
)()(
)()()( 23312 hhzy1hhz
13060319280143
319209640176601
hh
hhy1z
212
23 ...,
)..().()()(
재열-재생랭킨사이클
26
CNU Engine Research Lab.
54
Solve :
T
s
2
1
10
13
y
3
4
12z
1 – y ‐ z
87
5 6
9 11
1 kg
1 ‐ y15 MPa
4 MPa
0.5 MPa
10 kPa
)()()( 101189in hhy1hhq
kgkJ492120155396743823408089115833 /.,).,.,(.).,.,(
kgkJ8089140871823402101117660hy1yhh 578 /.,).,.().,.()(
56410 hy1yhhy1yh )()(
578 hy1yhh )(
kgkJ4087182340
9264392643408710155317660
y1
hhhhyh 445105 /.,
.
.)..,.,(.)(
)()( 113out hhzy1q
kgkJ34851811917335213060176601 /.,)..,()..(
%).(..,
.,, 2494920
49212
348511
q
q1
in
outRegen‐RehR
kgkJ40871hh 65 /.,
재열-재생랭킨사이클
CNU Engine Research Lab.
55
Discussion :
%).(., 2494920Regen‐RehR
%).(., 0434300Rth
%).(., 0454500ReheatR kgkJ87521w Reheatnet /.,,
kgkJ74521wnet /.,kgkJ23763qin /.,
kgkJ18963qin /.,
%).(., 3464630RegenR kgkJ22821w Regennet /.,, kgkJ17692q Regenin /.,,
kgkJ49212q Regen‐Rehin /.,, kgkJ14361w Regen‐Rehnet /.,,
재열-재생랭킨사이클