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Alphatronic 2000 PCS - MAN Diesel & Turbo

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Primary control function<br />

The manoeuvre panels are fitted with<br />

manoeuvre levers for controlling the<br />

propeller speed and pitch. The lever on<br />

the bridge centre panel and the lever on<br />

the ECR panel have individual potenti-<br />

ometers connected to the main cabinet.<br />

Depending on the chosen mode of op-<br />

eration, these lever signals will be used<br />

for setting the engine speed and the<br />

propeller pitch accordingly.<br />

An electric speed setting signal is trans-<br />

mitted from the <strong>PCS</strong> main cabinet to<br />

the engine governor. If the engine has a<br />

governor with pneumatic speed setting,<br />

the electric speed order is converted<br />

into a pressure using an E/P–converter.<br />

The propeller pitch is controlled by two<br />

solenoid valves in the hydraulic system.<br />

The electronic servo unit controls the<br />

solenoid valves for ’ahead’ and ’astern’<br />

pitch changes by comparing actual<br />

pitch and set point. Actual propeller<br />

pitch is measured by two transmitters.<br />

One transmitter is used for indication<br />

of the actual position of the propeller.<br />

The other transmitter gives the feed-<br />

back signal to the electronic servo unit.<br />

In case of emergency<br />

If the propulsion control system is out<br />

of service, the propulsion plant may still<br />

be operated from the bridge using the<br />

back-up system. The back-up system<br />

is independent of the main control sys-<br />

tem, although it is operated from the<br />

same lever on the bridge.<br />

Selection of back-up will set the gov-<br />

ernor to a fixed speed (normally corre-<br />

sponding to the nominal shaft generator<br />

speed) and set the propeller pitch corre-<br />

sponding to the present thrust. Change<br />

8 <strong>Alphatronic</strong> <strong>2000</strong> <strong>PCS</strong> Propulsion Control System<br />

Load diagram<br />

Power [%]<br />

100<br />

90<br />

80<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

0<br />

1<br />

2<br />

5<br />

60 65 70 75 80 85 90 95 100<br />

Theoretical Propeller Curve<br />

3<br />

1<br />

Combinator Curve<br />

2 100% MEP<br />

5 50% MEP<br />

3<br />

Load Limit<br />

Fig. 4: General load diagram<br />

Pitch and engine speed slew rates<br />

Propeller pitch [%]<br />

100<br />

80<br />

60<br />

40<br />

20<br />

0<br />

-20<br />

-40<br />

-60<br />

-80<br />

-100<br />

4<br />

6<br />

Zero Thrust Curve<br />

-20 0 20 40 60<br />

6<br />

4<br />

time [sec.]<br />

Normal pitch rate ahead Pitch rate at crash stop<br />

Speed [%]<br />

Normal engine speed rate Engine speed rate at crash stop<br />

Normal pitch rate astern<br />

Fig. 5: Control lever slew rate for propeller pitch command<br />

between normal control and back-up<br />

control will thus not change the actual<br />

propeller thrust.<br />

Load control<br />

The control system uses the propeller<br />

pitch and engine speed as controlling

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