Man B&W S50ME-B9.3-TII - Exhaust Gas Amount and Temperature

MAN B&W 6.04
Page 8 of 12
MAN Diesel
MAN B&W MC/MC-C/ME/MEC/ME-B/GI engines 198 43 181.3
Exhaust Gas Amount and Temperature
Influencing factors
The exhaust gas data to be expected in practice
depends, primarily, on the following three factors:
a) The specified MCR point of the engine (point M):
P
M
: power in kW at specified MCR point
n
M
: speed in r/min at specified MCR point
b) The ambient conditions, and exhaust gas
backpressure:
T
air
: actual ambient air temperature, in °C
p
bar
: actual barometric pressure, in mbar
T
CW
: actual scavenge air coolant temperature,
in °C
∆p
M
: exhaust gas backpressure in mm WC at
specified MCR
c) The continuous service rating of the engine
(point S), valid for fixed pitch propeller or control-
lable pitch propeller (constant engine speed):
P
S
: continuous service rating of engine, in kW
Calculation Method
To enable the project engineer to estimate the ac-
tual exhaust gas data at an arbitrary service rating,
the following method of calculation may be used.
The partial calculations based on the above influ-
encing factors have been summarised in equations
[4] and [5].
Fig. 6.04.06: Summarising equations for exhaust gas amounts and temperatures
The partial calculations based on the influencing
factors are described in the following:
a) Correction for choice of specified MCR point
When choosing a specified MCR point ‘M’ other
than the nominal MCR point ‘L
1
’, the resulting
changes in specific exhaust gas amount and
temperature are found by using as input in dia-
grams the corresponding percentage values (of
L
1
) for specified MCR power P
M%
and speed n
M%
:
P
M%
= P
M
/P
L1
x 100%
n
M%
= n
M
/n
L1
x 100%
M
exh
= M
L1
x
P
M
___
P
L1
x 1 +
∆m
M%
______
100
x 1 +
∆M
amb%
_______
100
x 1 +
∆m
s%
_____
100
x
P
S%
____
100
kg/h +/5% [4]
T
exh
= T
L1
+ ∆T
M
+ ∆T
amb
+ ∆T
S
°C /+15 °C [5]
where, according to ‘List of capacities’, i.e. referring to ISO ambient conditions and 300 mm WC
backpressure and specified in L
1
:
M
L1
: exhaust gas amount in kg/h at nominal MCR (L
1
)
T
L1
: exhaust gas temperature after turbocharger in °C at nominal MCR (L
1
)


















M
exh
: exhaust gas amount in kg/h, to be found
T
exh
: exhaust gas temperature in °C, to be found