s90mec7
.pdf
MAN B&W |
15.04 |
|
|
Exhaust gas silencer
The typical octave band sound pressure levels from the diesel engine’s exhaust gas system – at a distance of one meter from the top of the exhaust gas uptake – are shown in Fig.15.04.02.
The need for an exhaust gas silencer can be decided based on the requirement of a maximum permissible noise level at a specific position.
The exhaust gas noise data is valid for an exhaust gas system without boiler and silencer, etc.
The noise level is at nominal MCR at a distance of one metre from the exhaust gas pipe outlet edge at an angle of 30° to the gas flow direction.
For each doubling of the distance, the noise level will be reduced by about 6 dB (far field law).
When the noise level at the exhaust gas outlet to the atmosphere needs to be silenced, a silencer can be placed in the exhaust gas piping system after the exhaust gas boiler.
The exhaust gas silencer is usually of the absorption type and is dimensioned for a gas velocity of approximately 35 m/s through the central tube of the silencer.
An exhaust gas silencer can be designed based on the required damping of noise from the exhaust gas given on the graph.
In the event that an exhaust gas silencer is required – this depends on the actual noise level requirement on the bridge wing, which is normally maximum 60 70 dB(A) – a simple flow silencer of the absorption type is recommended. Depending on the manufacturer, this type of silencer normally has a pressure loss of around 20 mm WC at specified MCR.
Page of 2
D" |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
.2 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|||
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
K |
K |
K |
K(Z |
|
|
#ENTREæFREQUENCIESæOFæOCTAVEæBANDS |
|
||||||
D"æ !
3-#ç#-%ç# 3-#ç#-%ç#
178 51 16-6.1
Fig. 15.04.02: ISO’s NR curves and typical sound pressure levels from the engine’s exhaust gas system. The noise levels at nominal MCR and a distance of 1 metre from the edge of the exhaust gas pipe opening at an angle of 30 degrees to the gas flow and valid for an exhaust gas system – without boiler and silencer, etc. Data for a specific engine and cylinder no. is available on request.
Spark arrester
To prevent sparks from the exhaust gas being spread over deck houses, a spark arrester can be fitted as the last component in the exhaust gas system.
It should be noted that a spark arrester contributes with a considerable pressure drop, which is often a disadvantage.
It is recommended that the combined pressure loss across the silencer and/or spark arrester should not be allowed to exceed 100 mm WC at specified MCR. This depends, of course, on the pressure loss in the remaining part of the system, thus if no exhaust gas boiler is installed, 200 mm WC might be allowed.
MAN B&W S90MC-C/ME-C7/8
MAN Diesel |
198 40 81-7.1 |
|
MAN B&W |
15.05 |
|
|
|
Page of 3 |
Calculation of Exhaust Gas Back Pressure
The exhaust gas back pressure after the turbo charger(s) depends on the total pressure drop in the exhaust gas piping system.
The components, exhaust gas boiler, silencer, and spark arrester, if fitted, usually contribute with a major part of the dynamic pressure drop through the entire exhaust gas piping system.
The components mentioned are to be specified so that the sum of the dynamic pressure drop through the different components should, if possible, approach 200 mm WC at an exhaust gas flow volume corresponding to the specified MCR at tropical ambient conditions. Then there will be a pressure drop of 100 mm WC for distribution among the remaining piping system.
Fig. 15.05.01 shows some guidelines regarding resistance coefficients and back pressure loss calculations which can be used, if the maker’s data for back pressure is not available at an early stage of the project.
The pressure loss calculations have to be based on the actual exhaust gas amount and temperature valid for specified MCR. Some general formulas and definitions are given in the following.
Exhaust gas data
M: exhaust gas amount at specified MCR in kg/sec. T: exhaust gas temperature at specified MCR in °C
Please note that the actual exhaust gas temperature is different before and after the boiler. The exhaust gas data valid after the turbocharger may be found in Chapter 6.
Exhaust gas velocity (v)
In a pipe with diameter D the exhaust gas velocity is:
v = Mρ x π x4D2in m/s
Pressure losses in pipes (∆p)
For a pipe element, like a bend etc., with the resistance coefficient ζ, the corresponding pressure loss is:
∆p = ζ x ½ ρ v2 x 9.811 in mm WC
where the expression after ζ is the dynamic pressure of the flow in the pipe.
The friction losses in the straight pipes may, as a guidance, be estimated as :
1 mm WC per 1 diameter length
whereas the positive influence of the up draught in the vertical pipe is normally negligible.
Pressure losses across components (∆p)
The pressure loss ∆p across silencer, exhaust gas boiler, spark arrester, rain water trap, etc., to be measured/ stated as shown in Fig. 15.05.01 (at specified MCR) is normally given by the relevant manufacturer.
Total back pressure (∆pM)
The total back pressure, measured/stated as the static pressure in the pipe after the turbocharger, is then:
∆pM = Σ ∆p
Mass density of exhaust gas (ρ)
ρ 1.293 x 273273+ T x 1.015 in kg/m3
The factor 1.015 refers to the average back pressure of 150 mm WC (0.015 bar) in the exhaust gas system.
where ∆p incorporates all pipe elements and components etc. as described:
∆pM has to be lower than 350 mm WC.
(At design stage it is recommended to use max. 300 mm WC in order to have some margin for fouling).
MAN B&W MC/MC C, ME/ME C/ME GI/ME-B engines
MAN Diesel |
198 40 94 9.3 |
|
MAN B&W |
15.05 |
|
|
|
Page of 3 |
Measuring Back Pressure |
|
At any given position in the exhaust gas system, |
|
the total pressure of the flow can be divided into |
|
dynamic pressure (referring to the gas velocity) |
|
and static pressure (referring to the wall pressure, |
|
where the gas velocity is zero). |
|
At a given total pressure of the gas flow, the |
|
combination of dynamic and static pressure may |
|
change, depending on the actual gas velocity. The |
|
measurements, in principle, give an indication of |
|
the wall pressure, i.e., the static pressure of the |
|
gas flow. |
|
It is, therefore, very important that the back pres- |
|
sure measuring points are located on a straight |
|
part of the exhaust gas pipe, and at some dis- |
|
tance from an ‘obstruction‘, i.e. at a point where |
|
the gas flow, and thereby also the static pressure, |
|
is stable. Taking measurements, for example, in a |
|
transition piece, may lead to an unreliable meas- |
|
urement of the static pressure. |
|
In consideration of the above, therefore, the total |
|
back pressure of the system has to be measured |
|
after the turbocharger in the circular pipe and not |
|
in the transition piece. The same considerations |
|
apply to the measuring points before and after the |
|
exhaust gas boiler, etc. |
|
MAN B&W MC/MC C, ME/ME C/ME GI/ME-B engines
MAN Diesel |
198 40 94 9.3 |
|
MAN B&W |
15.05 |
|
|
Pressure losses and coefficients of resistance in exhaust pipes
a |
|
a |
90 |
|
60 b Change over valves |
|
|
|
c |
|
Change over valve |
|
|
of type with con- |
|
|
stant cross section |
|
|
ζa = 0.6 to 1.2 |
20 |
|
ζb = 1.0 to 1.5 |
a |
b |
ζc = 1.5 to 2.0 |
Change over valve of type with volume
ζa = ζb = about 2.0
90
D
R
60
D
R
30
D
|
M |
|
90 |
|
|
|
|
|
p |
Spark |
D |
|
|
arrester |
|
|
|
|
|
|
M |
|
R |
|
|
|
|
|
p2 |
Silencer |
45 |
|
|
|
|
ptc |
M |
|
|
|
|
|
|
|
|
|
D |
|
|
M |
|
|
p3 |
Exhaust |
|
|
gas boiler |
|
|
|
|
M |
|
|
|
Mtc |
Mtc |
|
|
T/C |
|
M: Measuring points |
|
|
|
|
|
|
178 32 09 1.0 |
Fig. 15.05.01: Pressure losses and coefficients of resistance in exhaust pipes
Page of 3
R = D |
ζ = 0.28 |
R = 1.5D |
ζ = 0.20 |
R = 2D |
ζ = 0.17 |
R = D |
ζ = 0.16 |
R = 1.5D |
ζ = 0.12 |
R = 2D |
ζ = 0.11 |
ζ = 0.05
R = D |
ζ = 0.45 |
R = 1.5D |
ζ = 0.35 |
R = 2D |
ζ = 0.30 |
ζ = 0.14
Outlet from |
ζ = 1.00 |
top of exhaust |
|
gas uptake |
|
Inlet (from |
|
turbocharger) |
ζ = – 1.00 |
178 06 85 3.0
MAN B&W MC/MC C, ME/ME C/ME GI/ME-B engines
MAN Diesel |
198 40 94 9.3 |
|
MAN B&W |
15.06 |
|
|
Page of 2
Forces and Moments at Turbocharger
$!



$"
$" |
$# |
DA: Max. movement of the turbocharger flange in the vertical direction
DB: Max. movement of the turbocharger flange in the transversal direction
DC: Max. movement of the turbocharger flange in the longitudinal direction
|
|
|
|
|
|
|
|
|
|
078 87 11-1.0.0b |
Fig. 15.06.01: Vectors of thermal expansion at the turbocharger exhaust gas outlet flange |
|
|
||||||||
|
|
|
|
|
|
|
|
|
|
|
No. of cylinders |
|
|
6-9 |
6 |
7 |
|
8 |
9 |
||
|
|
|
|
|
|
|
|
|
|
|
Turbocharger |
DA |
|
DB |
DC |
DC |
|
DC |
DC |
||
Make |
Type |
mm |
|
mm |
mm |
mm |
|
mm |
mm |
|
MAN Diesel |
|
NA70 |
10.1 |
|
1.6 |
2.4 |
2.7 |
|
3.0 |
3.4 |
|
|
|
|
|
|
|
|
|
|
|
ABB |
|
TPL80 |
8.7 |
|
1.6 |
2.4 |
2.7 |
|
3.0 |
3.4 |
|
|
|
|
|
|
|
|
|
|
|
|
TPL85 |
9.6 |
|
1.6 |
2.4 |
2.7 |
|
3.0 |
3.4 |
|
|
|
|
|
|||||||
|
|
|
|
|
|
|
|
|
|
|
MHI |
|
MET71 |
9.0 |
|
1.6 |
2.4 |
2.7 |
|
3.0 |
3.4 |
|
|
|
|
|
|
|
|
|
|
|
|
MET83 |
9.7 |
|
1.6 |
2.4 |
2.7 |
|
3.0 |
3.4 |
|
|
|
|
|
|||||||
|
|
|
|
|
|
|
|
|
|
|
Table 15.06.02: Max. expected movements of the exhaust gas flange resulting from thermal expansion
MAN B&W S90MC-C7/8, S90ME-C7/8
MAN Diesel |
198 41 44-2.1 |
|
MAN B&W |
|
|
|
15.06 |
|
|
|
|
Page of 2 |
|
-!.æ$IESEL |
|
|
!""æ40, |
& |
|
|
& |
|
- |
- |
|
- |
- |
& |
& |
& |
|
& |
|
|
-ITSUBISHI |
|
& |
- |
|
- |
|
|
& |
& |
|
|
|
078 38 48-6.2.0
Fig. 15.06.03: Forces and moments on the turbochargers’ exhaust gas outlet flange
Table 15.06.04 indicates the maximum permis sible forces (F1, F2 and F3) and moments (M1 and M3), on the exhaust gas outlet flange of the turbo charger(s). Reference is made to Fig. 15.06.03.
Turbocharger |
M1 |
M3 |
F1 |
F2 |
F3 |
||
Make |
Type |
Nm |
Nm |
N |
N |
N |
|
MAN Diesel |
NA70 |
5,300 |
3,500 |
8,800 |
8,800 |
3,500 |
|
|
|
|
|
|
|
|
|
ABB |
TPL80 |
11,000 |
11,000 |
15,000 |
13,000 |
13,000 |
|
|
|
|
|
|
|
||
TPL85 |
16,000 |
16,000 |
19,000 |
15,000 |
15,000 |
||
|
|||||||
|
|
|
|
|
|
|
|
MHI |
MET71 |
7,000 |
3,500 |
9,600 |
3,300 |
3,100 |
|
|
|
|
|
|
|
||
MET83 |
9,800 |
4,900 |
11,700 |
4,100 |
3,700 |
||
|
|||||||
|
|
|
|
|
|
|
|
Table 15.06.04: The max. permissible forces and moments on the turbocharger’s gas outlet flanges
MAN B&W S90MC-C7/8, S90ME-C7/8
MAN Diesel |
198 41 44-2.1 |
|
MAN B&W |
15.07 |
|
|
Diameter of Exhaust Gas Pipes
The exhaust gas pipe diameters listed in Table 15.07.02 are based on the exhaust gas flow capacity according to ISO ambient conditions and an exhaust gas temperature of 250 ºC.
Page of 1
The exhaust gas velocities and mass flow listed apply to collector pipe D4. The table also lists the diameters of the corresponding exhaust gas pipes D0 for various numbers of turbochargers installed.
$ |
%XPANSIONæJOINT |
|
OPTION æ æ æ |
$ |
|
$ |
$ |
4RANSITIONæPIECE OPTION æ æ æ
#ENTREæLINEæTURBOCHARGER 
178 09 39 5.2
Fig. 15.07.01: Exhaust pipe system, with turbocharger located on exhaust side of engine
|
Gas velocity |
|
|
Exhaust gas pipe diameters |
|
||||
35 m/s |
40 m/s |
45 m/s |
50 m/s |
|
|
D0 |
|
D4 |
|
|
Gas mass flow |
|
1 T/C |
2 T/C |
|
3 T/C |
4 T/C |
|
|
kg/s |
kg/s |
kg/s |
kg/s |
[DN] |
[DN] |
|
[DN] |
[DN] |
[DN] |
60.1 |
68.7 |
77.3 |
85.9 |
1,800 |
1,300 |
|
1,050 |
900 |
1,800 |
|
|
|
|
|
|
|
|
|
|
67.0 |
76.5 |
86.1 |
95.7 |
N.A. |
1,300 |
|
1,100 |
950 |
1,900 |
|
|
|
|
|
|
|
|
|
|
74.2 |
84.8 |
95.4 |
106.0 |
N.A. |
1,400 |
|
1,150 |
1,000 |
2,000 |
|
|
|
|
|
|
|
|
|
|
81.8 |
93.5 |
105.2 |
116.9 |
N.A. |
1,500 |
|
1,200 |
1,050 |
2,100 |
|
|
|
|
|
|
|
|
|
|
89.8 |
102.6 |
115.5 |
128.3 |
N.A. |
1,600 |
|
1,300 |
1,100 |
2,200 |
|
|
|
|
|
|
|
|
|
|
98.1 |
112.2 |
126.2 |
140.2 |
N.A. |
1,600 |
|
1,300 |
1,150 |
2,300 |
|
|
|
|
|
|
|
|
|
|
106.9 |
122.1 |
137.4 |
152.7 |
N.A. |
1,700 |
|
1,400 |
1,200 |
2,400 |
|
|
|
|
|
|
|
|
|
|
116.0 |
132.5 |
149.1 |
165.6 |
N.A. |
1,800 |
|
1,400 |
1,300 |
2,500 |
|
|
|
|
|
|
|
|
|
|
Table 15.07.02: Exhaust gas pipe diameters and exhaust gas mass flow at various velocities
MAN B&W S90MC-C7, S90ME-C7
MAN Diesel |
198 64 93-8.0 |
|
MAN B&W
Engine Control System
16
MAN Diesel
