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<strong>MAN</strong> B&W 6.02<br />

L<str<strong>on</strong>g>is</str<strong>on</strong>g>t of Capacities and Cooling Water Systems<br />

The L<str<strong>on</strong>g>is</str<strong>on</strong>g>t of Capacities c<strong>on</strong>tain data regarding the<br />

necessary capacities of the auxiliary machinery<br />

for the main engine <strong>on</strong>ly, and refer to a nominally<br />

rated engine. Complying with IMO Tier I NO x limitati<strong>on</strong>s.<br />

The heat d<str<strong>on</strong>g>is</str<strong>on</strong>g>sipati<strong>on</strong> figures include 0% extra<br />

margin for overload running except for the scavenge<br />

air cooler, which <str<strong>on</strong>g>is</str<strong>on</strong>g> an integrated part of the<br />

diesel engine.<br />

Cooling Water Systems<br />

The capacities given in the tables are based <strong>on</strong><br />

tropical ambient reference c<strong>on</strong>diti<strong>on</strong>s and refer to<br />

engines with high efficiency/c<strong>on</strong>venti<strong>on</strong>al turbocharger<br />

running at nominal MCR (L ) for:<br />

• Seawater cooling system,<br />

See diagram, Fig. 6.02.0 and nominal capacities<br />

in Fig. 6.03.0<br />

• Central cooling water system,<br />

See diagram, Fig. 6.02.02 and nominal capacities<br />

in Fig. 6.03.0<br />

Seawater<br />

32 C<br />

Fig. 6.02.01: Diagram for seawater cooling system<br />

Seawater outlet<br />

Seawater inlet<br />

32 C<br />

45 C<br />

Central<br />

cooler<br />

<strong>MAN</strong> B&W MC, MC-C, ME, ME-B, ME-C, ME-GI engines<br />

Scavenge air cooler<br />

Lubricating oil cooler<br />

Central coolant<br />

36 C<br />

Fig. 6.02.02: Diagram for central cooling water system<br />

38 C<br />

Scavenge<br />

air<br />

cooler (s)<br />

<strong>MAN</strong> <strong>Diesel</strong><br />

Page of<br />

The capacities for the starting air receivers and<br />

the compressors are stated in Fig. 6.03.0 .<br />

Heat radiati<strong>on</strong> and air c<strong>on</strong>sumpti<strong>on</strong><br />

The radiati<strong>on</strong> and c<strong>on</strong>vecti<strong>on</strong> heat losses to the<br />

engine room <str<strong>on</strong>g>is</str<strong>on</strong>g> around % of the engine nominal<br />

power (kW in L ).<br />

The air c<strong>on</strong>sumpti<strong>on</strong> <str<strong>on</strong>g>is</str<strong>on</strong>g> approximately 98.2%<br />

of the calculated exhaust gas amount, ie.<br />

M air = M exh x 0.982.<br />

Flanges <strong>on</strong> engine, etc.<br />

The locati<strong>on</strong> of the flanges <strong>on</strong> the engine are<br />

shown in: ‘Engine pipe c<strong>on</strong>necti<strong>on</strong>s’, and the flanges<br />

are identified by reference letters stated in the<br />

‘L<str<strong>on</strong>g>is</str<strong>on</strong>g>t of flanges’; both can be found in Chapter 5.<br />

The diagrams use the ‘Basic symbols for piping’,<br />

whereas the symbols for instrumentati<strong>on</strong> according<br />

to ‘ISO 2 9� ’ and ‘ISO 2 9�2’ and the instrumentati<strong>on</strong><br />

l<str<strong>on</strong>g>is</str<strong>on</strong>g>t found in Appendix A.<br />

Jacket water cooler<br />

45 C<br />

80 C<br />

Jaket<br />

water<br />

cooler<br />

Lubricating<br />

oil<br />

cooler<br />

43 C<br />

Seawater outlet<br />

80 C<br />

178 11 26�4.1<br />

178 11 27�6.1<br />

198 50 42-8.3

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