Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
OTTO CYCLE The Otto cycle is the theoretical cycle for the spark-ignition (SI) engine
0-1 suction stroke
1-2 compressed isentropically
3-4 isentropic expansion
4-1 the heat is rejected
Consider 1 kg of air. Heat added during process 2-3 = cv (T3 - T2) Heat rejected during process 4-1 = cv(T4 – T1) ∴ Work done = heat added – heat rejected = cv (T4 – T2) – cv(T4 – T1) Thermal efficiency, η = Or
η=
work done heat supplied
c v ( T3 − T2 ) − c v (T4 − T1 ) c v (T3 − T2 )
=1−
(T4 − T1 ) (T3 − T2 )
Now compression ratio
v4 v1 =r = Expansion ratio v3 v2
For ideal gas pv = RT and pv γ = cons tan t. These equations yield T2 v1 = T1 v 2
γ −1
v = 4 v3
γ −1
=
T3 = r γ −1 T4
21
2-3 heat is added at constant volume
Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
∴ T3 = T4 r γ −1 and T2 = T1 r γ −1 Hence, substituting
η =1−
(
T − T1 T4 − T1 1 =1− = 1 − γ −1 γ −1 γ −1 ( T4 − T1 ) r T4 r − T1r r 4 γ −1
)
The efficiency can also be expressed in terms of temperatures T3 and T4. Now, since
v1 v 3 = , it follows that v2 v4 T2 T3 T T = or 2 = 1 T1 T4 T3 T 4
T2 T1 = T3 T 4
-1
and hence, 1−
T2 T = 1− 1 T3 T4
or
T3 − T2 T4 − T1 = T3 T4
Therefore, T4 − T1 T4 = T3 − T2 T3 Hence, substituting, in (a) we get
η = 1−
T4 T = 1− 1 T3 T2
Otto cycle efficiency at different compression ratios and γ
Helium (γ = 1.66) monoatomic gas Argon (γ = 1.97) monoatomic gas
22
Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
Mean effective pressure (mep) of Otto cycle Let clearance volume be unity, i.e, V2 = V3 = 1, and V1 – V4 = r and
p3 =α p2
Now
p2 p = rγ = 3 p1 p4 ∴
p3 p 4 = =α p 2 p1
Work done = area of the p-v diagram =
p 3 v 3 − p 4 v 4 p 2 v 2 − p1 v1 − γ −1 γ −1
=
p 1 p3 − 1 − p1 r 2 − 1 p 4 r γ −1 p4r p1 r
=
r p 4 r γ −1 − 1 − p1 r γ −1 − 1 γ −1
=
r r γ −1 − 1 ( p 4 − p1 ) γ −1
=
p1 r ( α − 1)( p 4 − p1 ) γ −1
[ ( (
)
(
)]
)
Length of the diagram = r − 1 23
Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
area of the diagram length of the diagram
∴ mep = =
(
)
p1 r ( α − 1) r γ −1 − 1 ( γ − 1)( r − 1)
1. Two Stroke
Spark plug
Deflector
Transfer port
Inlet valve
Crankcase Scavenging
Exhaust blow down
P
3
P
Piston travel in uncovering port
2 4 5 VC
VS Ideal diagram
1 V
24 Actual diagram
V
Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
2. The Diesel Cycle T
s
Work done in compression
1-2 = area 1256
Heat supplied in 2-3 = area 2365
Work done in expansion
3-4 = area 23456
heat rejected in 4-1 = area 4156
Net work done
= area 1234
The thermal efficiency of the ideal Diesel cycle is given by η= =
heat added − heat rejected heat added c p ( T3 − T2 ) − c v ( T4 − T1 ) c p ( T3 − T2 )
1 T − T1 = 1 − 4 γ T3 − T2 T4 −1 T T =1− 1 1 γ T2 T3 −1 T2
:
=1−
c v ( T4 − T1 ) 1 ( T4 − T1 ) =1− c p ( T3 − T2 ) c p ( T3 − T2 ) cv
T1 T2
For isentropic compression and expansion process T1 v 2 = T2 v1
γ −1
and
T4 v 3 = T3 v 4
For constant pressure heat addition 2-3, Also
γ −1
T3 v 3 = T2 v 2
v4 = v1 25
Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
T4 T3 v3 / v 4 = T1 T2 v 2 / v1
Thus
γ −1
v v = 3 3 v2 v2
γ −1
v = 3 γ v2
Substituting these values in Eq.(the thermal efficiency), we get v2 −1 1 η = 1− γ −1 γ ( v1 / v 2 ) T3 − 1 T2
η = 1−
1 ρ γ −1 r γ −1 γ ( ρ − 1)
Note that the efficiency of the Diesel cycle differs from that of Otto cycle only by the bracketed term, which is always greater than unity (except when ρ = 1 and there is no heat addition).Thus the Diesel cycle always has a lower efficiency than the Otto cycle of the same compression ratio.
Fig ..Efficiency of the Diesel cycle for various cut-off ratios and compression ratios.
Mean Effective Pressure (mep) of Diesel cycle. Work done = area of the p-v diagram = p2 ( v3 − v2 ) + = p 2 ( ρ − 1) +
p 3 v 3 − p 4 v 4 p 2 v 2 − p1 v1 − γ −1 γ −1
p 3 ρ − p 4 r − ( p 2 − p1 r ) γ −1
(
)
(
)
p 2 ( ρ − 1)( γ − 1) + p 2 ρ − ρ γ r 1−γ − p 2 1 − r γ −1 p = − 2 γ ( ρ − 1) − r 1−γ ρ γ − 1 γ −1 γ −1 mep = =
area of the indicator diagram length of the indicator diagram
[
(
)]
p 2 γ ( ρ − 1) − r 1−γ ρ γ − 1 ( γ − 1)( r − 1)
26
[
(
)]
Ir. TRI TJAHJONO, MT/INTERNAL COMBUSTION ENGINE
=
[
(
)]
p1 r γ γ ( ρ − 1) − r 1−γ ρ γ − 1 ( γ − 1)( r − 1)
27