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en / 11.05.2000
BA000658
2/4
The
exhaust temperatures before and after the turbocharger
are used to assess the thermodynamic
load condition of the engine as they cover the overall thermodynamics of the engine, exhaust
turbine and intake condition.
The temperatures after the turbocharger should not exceed the full load value in the acceptance test
certificate
by more than
30 K.
∆
t
texh. after turb.
≤
30 K
•
Compare the exhaust temperature after the turbocharger during full load operation with the
specification in the acceptance test certificate
If
∆
t > 30 K
, then determine the cause of the temperature rise (different ambient conditions,
type of fuel, fouled charger etc.). Also refer to
.
Reduce the engine power if the maximum permissible temperature after the turbine is
exceeded during operation with
Heavy fuel
t
texh. after turb.
max. 400 °C
Distillate fuel
t
texh. after turb.
max. 420 °C
•
Make an additional check of the combustion by assessing the exhaust opacity. If combustion
is good, the exhaust will be invisible or a light grey. Assessment of the exhaust colour: refer to
Note for exhaust temperature monitors:
Contrary to the monitor for the average exhaust temperature, an alarm is only activated when limit
values are reached when monitoring the exhaust temperatures of each cylinder (thermal overload
of a cylinder or misfiring). Total misfiring can cause damage to the flexible coupling!
It should be noted that partial misfiring already subjects the flexible coupling to impermissible
loads. Refer to
.
Содержание M20
Страница 5: ...Technical engine data A1 M20 M601C en 31 10 2001 AA000103 1 1 Technical engine data...
Страница 6: ...Governor data A1 04 en 18 02 2000 AA000097 1 1 Governor data not installed on CD Rom...
Страница 10: ...Acceptance Test Records A1 10 en 16 11 1999 AA000095 1 1 Acceptance test records not installed on CD Rom...
Страница 11: ...Operating instructions A3 M20 M601C en 31 10 2001 AA000108 1 1 Operating instructions...
Страница 30: ...Initial operation Engine A3 05 00 en 14 02 2001 BA000022 1 1 Initial operation...
Страница 44: ...Operational supervision Engine A3 06 00 en 15 02 2001 BA000058 1 1 Operational supervision...
Страница 64: ...Removal from operation Engine A3 07 00 en 16 02 2001 BA000094 1 1 Removal from operation...
Страница 71: ...Danger of frost Engine A3 08 00 en 16 02 2001 BA000106 1 1 Danger of frost...
Страница 83: ...Running in Engine A3 10 00 en 16 02 2001 BA000242 1 1 Running in...
Страница 85: ...Fault tracing Engine A3 11 00 en 19 02 2001 BA000130 1 1 Fault tracing...
Страница 91: ...Emergency operation Engine A3 12 00 en 19 02 2001 BA000142 1 1 Emergency operation...
Страница 102: ...Operating media A4 en 31 10 2001 AA020105 1 1 Operating media...
Страница 106: ...Regulations and care Engine A4 05 00 en 21 02 2001 BA000158 1 1 Regulations and care...
Страница 137: ...Maintenance A5 en 31 10 2001 AA000026 1 1 Maintenance...
Страница 166: ...Periodical schedule Heavy fuel A5 04 02 M20 en 31 10 2001 AA021679 8 8...
Страница 242: ...Bearing Shells Inspection Evaluate A5 05 02 03 07 01 M20 en 13 06 1997 IB001449 3 4 02 1 2 3...
Страница 243: ...Bearing Shells Inspection Evaluate A5 05 02 03 07 01 M20 en 13 06 1997 IB001449 4 4 02 4 5 6...
Страница 435: ...Table of contents A6 01 en 31 10 2001 AA020050 1 1 Tools A6 Table of contents A6 01...