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en / 16.12.1997
BA000256
1/2
Emergency operation of the main engine
•
Stop the engine
•
Remove the air filter silencer
Shut down the turbocharger (block the rotor), see manufacturer´s instructions
Note:
If blocking is not possible:
-
disassemble the rotor.
-
obturate the exhaust gas side against bearing housing and air side by means of a
blind flange.
•
Interrupt the oil supply to the turbocharger, for this:
-
unscrew the connection of the pipe at the engine and close the connector with a plug an
union nut.
-
Plug and fasten the free end of the pipe.
Note:
The cooling water supply is to be interrupted only in case there is a considerable
leakage at the turbine housing on gas side, which would endanger the engine.
Note:
If there are two turbochargers feeding into one charge air manifold:
-
Close the air outlet casing of the turbocharger taken out of service with a blanking
cover.
•
Start the engine and reduce the output. If the installation is for heavy fuel, we recommend the
change to distillate fuel in emergency operation.
Fixed propellers
Start the engine with a
P
me
≈
5 bar abt. 20 % nominal power
CP propellers
The load conditions, as for a fixed propeller installation, should be reached by reducing the
propeller pitch and engine speed. Operation at rated speed is practically impossible, because the
engine output that can be reached, is generally lower than the propeller input at zero pitch.
Multi-engine plants with one propeller
The propellers are generally of the variable pitch type. Declutch the engine with the defective
turbocharger. Set the propeller pitch, so that the engine remaining in service can be run at rated
speed and continuous power. It is not necessary and impossible without equipment, for unbalanced
engine loads to run the defective engine at reduced output to increase the total power available. The
expenditure and the gain in power would not justify this.
^
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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...