Motoare Man

Contents Four-stroke Propulsion systems L23/30A-KV ............................................................ 800 - 1280 kW............................... 2 V23/30A-VO ........................................................... 1920 kW............................... 3 L21/31-VBS ............................................................1290 - 1935 kW............................... 4 L28/32A-VO.............................................................1470 - 2205 kW............................... 5 L27/38-VBS .............................................................2040 - 3060 kW............................... 6 V28/32A-VO ............................................................2940 - 3920 kW............................... 7 Two-stroke Propulsion Systems L35MC-VBS.............................................................2600 - 7800 kW............................... 8 S35MC-VBS............................................................2960 - 8880 kW............................... 9 L42MC-VBS.............................................................3980 - 11940 kW.............................10 S42MC-VBS............................................................4320 - 12960 kW.............................11 S46MC-VBS............................................................5240 - 10480 kW.............................12 L50MC-VBS.............................................................5320 - 10640 kW.............................13 S50MC-VBS............................................................5720 - 11440 kW.............................14 S50MC-C-VBS........................................................6320 - 12640 kW.............................15 Reduction gearboxes for CP Propellers KV, VO and HO......................................................................................................................16 Power Take-Off/Power Take-In Flexstar and conventional range .........................................................................................17 CP Propellers VB and VBS range ................................................................................................................18 Alphatronic Control Systems IIA and 2000 ...........................................................................................................................19 CP Propellers and Control Systems for Two-stroke Engines L60MC, S60MC and S60MC-C ............................7680 - 15360 kW.............................20 Alpha Clutcher - for Auxiliary Propulsion Systems ............... ...................................21 CP Propellers and Control Systems for Four-stroke Engines L32/40 and V32/40 .................................................2880 - 7680 kW.............................22 L40/54, L48/60 and L58/64 ...................................4320 - 12510 kW.............................23

MAN B&W Diesel A/S

Screen version of the publication "Quick Guide to Propulsion Packages" (300/6.0-GB. Status Sept 2000A) Data pages only. All general company and product information from the printed version are left out.

MAN B&W Four-stroke Propulsion SystemsL23/30A-KV800-1280kW(1090-1740 BHP)

Dia

m.

Q R S W A

K B 1090

J F 387 910

C 988 640D 370 370 720

420

525

M20

15

H

Standard programme

Main data

Specific consumption

Weight

ENGINE REDUCTION GEAR PROPELLER DIMENSIONS IN MM

Type. Series Type Type Speed Diam A B C D F H J K M Q R W

Output mcr rpm mm min

6L23/30A-E AMG 8 31KV8 VB 560 268 2200 3975 2898 4136 1566 328 1587 770 1077 636 293 553 900800 kW AMG 8 39KV8 VB 640 214 2450 3975 2898 4136 1566 328 1587 770 1077 636 360 595 900

1090 BHP AMG 8 44KV9 VB 640 190 2600 3975 2898 4136 1566 328 1587 770 1077 636 360 595 900AMG 16 52KV13 VB 740 159 2850 4550 2898 4660 2090 318 1587 1282 1662 505 445 655 1200

6L23/30A AMG 8 31KV8 VB 560 292 2250 3975 2898 4136 1566 328 1587 770 1077 636 293 553 900960 kW AMG 8 39KV8 VB 640 233 2450 3975 2898 4136 1566 328 1587 770 1077 636 360 595 900

1305 BHP AMG 8 44KV9 VB 640 207 2600 3975 2898 4136 1566 328 1587 770 1077 636 360 595 900AMG 16 52KV13 VB 740 173 2850 4550 2898 4660 2090 318 1587 1282 1662 505 445 655 1200

8L23/30A AMG 11 31KV11 VB 640 292 2350 4953 3628 5064 1754 318 1587 950 1325 639 415 595 9001280 kW AMG 11 39KV11 VB 640 233 2600 4953 3628 5064 1754 318 1587 950 1325 639 415 655 12001740 BHP AMG 11 44KV13 VB 740 207 2800 4953 3628 5064 1754 318 1587 950 1325 639 445 655 1200

AMG 16 52KV13 VB 860 173 3100 5290 3628 5400 2090 318 1587 1282 1662 505 445 745 1350

PISTONENGINE BORE STROKE SPEED MEP SPEED OUTPUT/CYLINDER

Type mm mm rpm bar m/s kW BHP

L23/30A-E 225 300 825 16,3 8,25 133 181L23/30A 225 300 900 17,9 9,00 160 217,5

ENGINE FUEL OIL LUBRICATING OIL

Type mcr 85% mcr mcr

g/kWh g/BHPh g/kWh g/BHPh g/kWh g/BHPh

L23/30A-E 188 138 187 137 1,0 0,7L23/30A 190 140 189 139 1,0 0,7

* Weight incl 4.0 m shaft and 2.0 m stern tube

ENGINE GEAR PROP Dry weight in tons (approx)Type Type Type Engine/Gear Prop*

6L23/30A-E 31KV8 VB 560 15,0 2,739KV8 VB 640 15,0 3,444KV9 VB 640 15,0 3,552KV13 VB 740 17,6 4,4

6L23/30A 31KV8 VB 560 15,0 2,739KV8 VB 640 15,0 3,444KV9 VB 640 15,0 3,552KV13 VB 740 17,6 4,4

8L23/30A 31KV11 VB 640 17,9 3,439KV11 VB 640 17,9 3,844KV13 VB 740 17,9 4,552KV13 VB 860 20,1 6,1

The propeller is calculated according to DnV, No Ice with high skew

Main data


Weight



V23/30A 225 300 900 17,9 9,0 160 217,5

ENGINE GEAR PROP DRY WEIGHT IN TONS (APPROX)

Type Type Type Engine Gear Prop*

12V23/30A 31VO16 VB 640 17,5 6,0 3,839VO16 VB 740 17,5 6,0 5,348VO22 VB 860 17,5 8,1 7,156VO28 VB 860 17,5 8,1 8,5

ENGINE FUEL OIL LUBRICATING 0IL



12V23/30A 191 141 190 140 1,0 0,7


MAN B&W Four-stroke Propulsion SystemsV23/30A-VO1920kW(2610 BHP)

Q R S W A

Dia

m.

J 695270

648

K 3830 L

46701535 420 420 1035 1757

P18

80

NM

1800

Standard programme

Optional horizontal offset gearboxes: Series AMG 20 type 31HO20, 39HO20 and 48H022The propeller is calculated according to DnV, No Ice with high skew


Type Series Type Type Speed Diam A J K L M N P Q R W


12V23/30A AMG 16 31VO16 VB 640 292 2550 5956 1662 2126 1090 505 525 420 360 595 9001920 kW AMG 16 39VO16 VB 740 233 2900 5956 1662 2126 1090 505 525 420 415 655 12002610 BHP AMG 28 48VO22 VB 860 187 3250 6091 1693 2261 1500 780 700 800 445 745 1350

AMG 28 56VO28 VB 860 164 3450 6091 1693 2261 1500 780 700 800 584 820 1600

MAN B&W Four-Stroke Propulsion SystemsL21/31-VBS1290-1935 kW (1755-2630 BHP)

Dia

m.

L M S W A

2241 B

1065

1940 658 851

C

811D 355

420

745

2189

Main data

PISTON OUTPUT/ENGINE BORE STROKE SPEED MEP SPEED CYLINDER

Type mm mm rpm bar m/s kW BHPL21/31 210 310 1000 24,1 10,3 215 292

Weight

ENGINE Gear Prop Dry weight in tons (appr.)Type Type Type Engine Gear Prop*6L 36VO18 VBS640 13,9 3,2

21/31 46VO18 VBS640 13,9 3,657VO18 VBS740 13,9 4,568VO18 VBS860 13,9 5,7

7L 36VO18 VBS640 15,2 3,621/31 46VO18 VBS740 15,2 4,4

57VO18 VBS740 15,2 4,968VO18 VBS860 15,2 6,2

ENGINE Gear Prop Dry weight in tons (appr.)Type Type Type Engine Gear Prop*8L 36VO18 VBS640 16,6 3,7

21/31 46VO18 VBS740 16,6 4,657VO18 VBS860 16,6 6,168VO18 VBS860 16,6 6,5

9L 36VO18 VBS740 18,2 4,521/31 46VO18 VBS740 18,2 5,0

57VO18 VBS860 18,2 6,468VO18 VBS860 18,2 7,0


The propeller diameter is optimized at 85% MCR, 98% rpm and 14,0 kn. The strength calculation is made at 100% MCR, 100% rpm and 14,5 kn The propeller is calculated according to LR, No Ice with high skew


ENGINE FUEL OIL LUBRICATING OILType mcr 85% mcr mcr

g/kWh g/BHPh g/kWh g/BHPh g/kWh g/BHPhL21/31 181 133 181 133 0,8 0,6

Standard programme

ENGINE REDUCTION GEAR PROPELLER DIMENSIONS IN MMType Series Type Type Speed Diam A B C D G H L M W

Output mcr rpm mm min6L21/31 AMG18EV 36VO18 VBS640 279 2350 5476 3235 4185 1598 1018 2029 550 596 12001290 kW 46VO18 VBS640 217 2650 5476 3235 4185 1598 1018 2029 550 596 12001755 bhp 57VO18 VBS740 174 2950 5476 3235 4185 1598 1018 2029 569 655 1300

68VO18 VBS860 147 3250 5476 3235 4185 1598 1018 2029 653 743 14007L21/31 AMG18EV 36VO18 VBS640 279 2450 5750 3590 4540 1598 1018 2029 550 596 12001505 kW 46VO18 VBS740 217 2750 5750 3590 4540 1598 1018 2029 569 655 13002047 bhp 57VO18 VBS740 174 3050 5750 3590 4540 1598 1018 2029 569 655 1300



68VO18 VBS860 147 3550 6541 4300 5250 1598 1018 2029 653 743 1400

Dataavailable

uponrequest

Dataavailable

uponrequest

Dataavailable

uponrequest

Dataavailable

uponrequest

MAN B&W Four-Stroke Propulsion SystemsL28/32A-VO1470-2205 kW (2000-3000 BHP)

Dia

m.

Q R S W A

K B LJ F 808 1300

E

C 585 G

1770 480 480 1160

HP N

M23

00

Standard programme

Main data


Type mm mm rpm bar m/s kW BHPL28/32A 280 320 775 19,3 8,3 245 333

Weight

ENGINE Gear Prop Dry weight in tons (appr.)Type Type Type Engine Gear Prop*6L 31VO11 VB 640 19,0 3,8 3,9

28/32A 39VO16 VB 740 19,0 6,0 5,148VO22 VB 860 19,0 8,1 6,156VO28 VB 860 19,0 8,1 7,2

7L 31VO16 VB 740 21,0 6,0 4,528/32A 39VO16 VB 860 21,0 6,0 5,8

48VO22 VB 860 21,0 8,1 7,156VO28 VB 980 21,0 8,1 8,3

ENGINE Gear Prop Dry weight in tons (appr.)Type Type Type Engine Gear Prop*8L 31VO16 VB 740 23,5 6,0 5,4

28/32A 39VO20 VB 860 23,5 8,1 6,548VO22 VB 860 23,5 8,1 7,356VO28 VB 980 23,5 8,1 8,4

9L 31VO20 VB 740 26,5 8,1 5,528/32A 39VO20 VB 860 26,5 8,1 7,1

48VO22 VB 980 26,5 8,1 8,356VO28 VB 980 26,5 8,1 8,6


Optional horizontal offset gearboxes: Series AMG 20 type 31HO20, 39HO20, 48HO22, 31HO30, 39HO30, 45HO30 and 52HO27 The propeller is calculated according to DnV, No Ice with high skew


ENGINE REDUCTION GEAR PROPELLER DIMENSIONS IN MMType Series Type Type Speed Diam A B C E F G H J K L M N P Q R W

Output mcr rpm mm min6L28/32A AMG 11 31VO11 VB 640 252 2600 6145 4340 5330 322 780 1147 2061 1325 1789 1090 460 525 420 360 595 9001470 kW AMG 16 39VO16 VB 740 201 2850 6482 4340 5330 322 780 1147 2061 1662 2142 1090 505 525 420 415 655 12002000 BHP AMG 28 48VO22 VB 860 161 3200 6599 4340 5330 322 780 1147 2061 1693 2277 1500 780 700 800 445 745 1350

AMG 28 56VO28 VB 860 141 3500 6599 4340 5330 322 780 1147 2061 1693 2277 1500 780 700 800 445 745 13507L28/32A AMG 16 31VO16 VB 740 252 2650 6892 4750 5810 252 710 1147 2061 1662 2142 1090 505 525 420 415 655 12001715 kW AMG 16 39VO16 VB 860 201 3000 6892 4750 5810 252 710 1147 2061 1662 2142 1090 505 525 420 445 745 13502330 BHP AMG 28 48VO22 VB 860 161 3300 7027 4750 5810 252 710 1147 2061 1693 2277 1500 780 700 800 445 745 1350



AMG 28 56VO28 VB 980 141 3850 8039 5780 6770 322 780 1259 2147 1693 2259 1500 780 700 800 584 820 1600


g/kWh g/BHPh g/kWh g/BHPh g/kWh g/BHPhL28/32A 188 138 187 137 1,0 0,7

MAN B&W Four-Stroke Propulsion SystemsL27/38-VBS2040-3060 kW (2775-4160 BHP)

Standard programme

Main data


Type mm mm rpm bar m/s kW BHPL27/38 270 380 800 23,5 10,1 340 462

Weight

ENGINE Gear Prop Dry weight in tons (appr.)Type Type Type Engine Gear Prop.*

31VO20 VBS740 30 8,5 4,76L 39VO20 VBS740 30 8,5 5,3

27/38 45VO30 VBS860 30 8,5 5,756VO28 VBS860 30 8,5 7,060VO55 VBS860 30 14 7,331VO20 VBS740 33,5 8,5 5,3

7L 39VO20 VBS860 33,5 8,5 6,427/38 45VO30 VBS860 33,5 8,5 6,6

56VO28 VBS860 33,5 8,5 7,760VO55 VBS980 33,5 14 9,4

ENGINE Gear Prop Dry weight in tons (appr.)Type Type Type Engine Gear Prop.*

31VO20 VBS860 37 8,5 6,48L 39VO30 VBS860 37 8,5 6,8

27/38 45VO30 VBS860 37 8,5 7,650VO30 VBS860 37 8,5 7,860VO55 VBS980 37 14 9,631VO30 VBS860 40,5 8,5 6,7

9L 39VO30 VBS860 40,5 8,5 7,127/38 45VO30 VBS860 40,5 8,5 8,1

50VO30 VBS980 40,5 8,5 9,460VO55 VBS980 40,5 14 10



g/kWh g/BHPh g/kWh g/BHPh g/kWh g/BHPhL27/38 182 134 180 132 0,8 0,6


Dia

m.

Q R S W A

15001693 (2689)

2279 (3071) B

1452820

C

GD 445

1960

530

530

H

700

H

ENGINE REDUCTION GEAR PROPELLER DIMENSIONS IN MMType Series Type Type Speed Diam A B C D G H Q R W

Output mcr rpm mm min31VO20 VBS740 256 2650 6229 3962 5070 1940 1166 2267 569 655 1300

6L27/38 AMG28EV 39VO20 VBS740 208 2950 6229 3962 5070 1940 1166 2267 569 655 13002040 kW 45VO30 VBS860 177 3200 6229 3962 5070 1940 1166 2267 653 743 1400

2775 BHP 56VO28 VBS860 145 3500 6229 3962 5070 1940 1166 2267 653 743 1400AMG55EV 60VO55 VBS860 133 3650 7033 3962 5070 1940 1166 2267 653 743 1400

31VO20 VBS740 256 2800 6674 4407 5515 1940 1166 2267 569 655 13007L27/38 AMG28EV 39VO20 VBS860 208 3100 6674 4407 5515 1940 1166 2267 653 743 14002380 kW 45VO30 VBS860 177 3350 6674 4407 5515 1940 1166 2267 653 743 1400

3235 BHP 56V028 VBS860 145 3650 6674 4407 5515 1940 1166 2267 653 743 1450AMG55EV 60VO55 VBS980 133 3800 7478 4407 5515 1940 1166 2267 746 806 1500





905

780

Figures in brackets for reduction gear AMG55EV

The propeller diameter is optimized at 85% MCR, 98% rpm and 14,0 kn. The strength calculation is made at 100% MCR, 100% rpm and 14,5 kn. The propeller is calculated according to LRS, No Ice with high skew

MAN B&W Four-stroke Propulsion SystemsV28/32A-VO2940-3920 kW(4000-5330 BHP)

Dia

m.

Q R S W AK B

LJ 860280

980

C970 10451550 510 510 1460

HP N

M22

35

Standard programme

Main data


Weight



V28/32A 280 320 775 19,3 8,3 245 333

ENGINE FUEL OIL LUBRICATING OIL



V28/32A 189 139 188 138 1,0 0,7* Weight incl 4,0 m shaft and 2,0 m stern tube

Optional horizontal offset gearboxes (12V28/32A only):Series AMG 20 type 31HO30, 39HO30 and 45HO30The propeller is calculated according to DnV, No Ice with high skew


Type Series Type Type Speed Diam A B C H J K L M N P Q R W


12V28/32A AMG 28 31VO30 VB 860 248 3050 7044 4870 5560 2152 1693 2174 1500 780 700 800 445 745 13502940 kW AMG 28 39VO30 VB 860 201 3400 7044 4870 5560 2152 1693 2174 1500 780 700 800 445 745 13504000 BHP AMG 28 45VO30 VB 980 171 3700 7044 4870 5560 2152 1693 2174 1500 780 700 800 584 820 1600

AMG 40 51VO36 VB 980 151 3950 7496 4870 5560 2152 2155 2626 1840 1050 870 1045 584 820 160016V28/32A AMG 28 31VO30 VB 860 248 3250 8036 5890 6580 2212 1693 2242 1500 780 700 800 445 745 13503920 kW AMG 36 34VO36 VB 860 231 3350 8516 5890 6580 2212 2155 2626 1570 925 736 911 445 745 13505330 BHP AMG 36 41VO36 VB 980 191 3750 8516 5890 6580 2212 2155 2626 1570 925 736 911 584 820 1600

AMG 40 51VO36 VB1080 151 4250 8516 5890 6580 2212 2155 2626 1840 1050 870 1045 600 855 1600

Engine Gear Prop* Dry weight in tons (approx)

Type Type Type Engine Gear Prop*

12V28/32A 31VO30 VB 860 29,5 8,1 7,139VO30 VB 860 29,5 8,1 7,945VO30 VB 980 29,5 8,1 8,651VO36 VB 980 29,5 13,4 8,9

16V28/32A 31VO30 VB 860 37,0 8,1 8,134VO36 VB 860 37,0 11,6 8,241VO36 VB 980 37,0 11,6 10,051VO36 VB1080 37,0 13,4 13,2

A B S W C D

H1

H2

H3

EDia

m.

L35MC-VBS standard programme

The propeller diameter is optimised at 90% mcr, 210 rpm and 14.5 kn * Engine output refers to load point L1The strength calculation is made at 100% mcr, 210 rpm and 15.0 kn ** Weight incl 6.0 m shaft and 3.0 m stern tubeThe propeller is calculated according to DnV, No Ice with high skew H1: Vertical liftThe standard plants may be subject to change due to torsional vibrations H2: Tilted lift - H3: Double jib crane

Main data


Type mm mm rpm bar m/s kW BHPL35MC 350 1050 210 18,4 7,35 650 880


ENGINE FUEL OIL LUBRICATING OIL CYLINDER OILType Layout point L1 Layout point L2 approx

g/kWh g/BHPh g/kWh g/BHPh kg/cyl. 24 h g/kWh g/bhphL35MC 177 130 171 126 2,0-3,0 0,8-1,2 0,6-0,9

MAN B&W Two-stroke Propulsion SystemsL35MC-VBS2600-7800 kW (3520-10560 BHP)

ENGINE PROPELLER DIMENSIONS IN MM DRY WEIGHT

Type Output* Hub OD-Box Speed Diameter A B C D E W H1 H2 H3 in tons (approx)

kW BHP Type Type rpm mm min Engine Propeller**

4L35MC 2600 3520 VBS 860 ODS250 210 3150 655 735 4000 1980 550 1970 5200 4900 5025 50 9,15L35MC 3250 4400 VBS 860 ODS280 210 3300 655 735 4600 1980 550 2000 5200 4900 5025 58 9,56L35MC 3900 5280 VBS 980 ODS280 210 3450 746 785 5200 1980 550 2000 5200 4900 5025 67 10,37L35MC 4550 6160 VBS 980 ODS310 210 3600 746 785 5800 1980 550 2040 5200 4900 5025 75 11,88L35MC 5200 7040 VBS 980 ODS310 210 3700 746 805 6400 1980 550 2040 5200 4900 5025 83 12,39L35MC 5850 7920 VBS 1080 ODS330 210 3800 825 880 7000 1980 550 2140 5200 4900 5025 92 13,9

10L35MC 6500 8800 VBS 1080 ODS330 210 3900 825 880 7600 1980 550 2140 5200 4900 5025 108 14,711L35MC 7150 9680 VBS 1180 ODS350 210 4000 900 940 8200 1980 550 2140 5200 4900 5025 118 16,512L35MC 7800 10560 VBS 1180 ODS350 210 4100 900 940 8800 1980 550 2140 5200 4900 5025 126 17,2

MAN B&W Two-stroke Propulsion SystemsS35MC-VBS2960-8880 kW (4040-12120 BHP)

A B S W C D

H1

H2

H3

E

S35MC-VBS standard programme

Main data


Type mm mm rpm bar m/s kW BHPS35MC 350 1400 173 19,1 8,07 740 1010



g/kWh g/BHPh g/kWh g/BHPh kg/cyl. 24 h g/kWh g/BHPhS35MC 178 131 173 127 2,0-3,0 0,95-1,5 0,7-1,1

Dia

m.





4S35MC 2960 4040 VBS 860 ODS280 173 3550 655 735 4035 2200 650 2000 6425 6050 5925 57 9,65S35MC 3700 5050 VBS 980 ODS310 173 3750 746 805 4635 2200 650 2040 6425 6050 5925 65 12,56S35MC 4440 6060 VBS 980 ODS330 173 3950 746 805 5235 2200 650 2070 6425 6050 5925 75 14,07S35MC 5180 7070 VBS 1080 ODS350 173 4100 825 880 5835 2200 650 2070 6425 6050 5925 84 16,68S35MC 5920 8080 VBS 1080 ODS375 173 4250 825 880 6435 2200 650 2265 6425 6050 5925 93 18,59S35MC 6660 9090 VBS 1180 ODS375 173 4350 900 940 7035 2200 650 2265 6425 6050 5925 103 20,4

10S35MC 7400 10100 VBS 1180 ODS375 173 4450 900 940 7635 2200 650 2265 6425 6050 5925 122 21,111S35MC 8140 11110 VBS 1280 ODS400 173 4550 975 1035 8235 2200 650 2511 6425 6050 5925 132 24,812S35MC 8880 12120 VBS 1280 ODS425 173 4650 975 1035 9435 2200 650 2676 6425 6050 5925 141 27,4

A B S W C D

H1

H2

H3

EDia

m.

MAN B&W Two-stroke Propulsion SystemsL42MC-VBS3980-11940 kW (5420-16260 BHP)


The propeller diameter is optimised at 90% mcr, 176 rpm and 15.4 knThe strength calculation is made at 100% mcr, 176 rpm and 16.0 knThe propeller is calculated according to DnV, No Ice with high skew The standard plants may be subject to change due to torsional vibrations

* Engine output refers to load point L1** Weight incl 6.0 m shaft and 3.0 m stern tubeH1: Vertical liftH2: Tilted lift - H3: Double jib crane

Main data





g/kWh g/BHPh g/kWh g/BHPh kg/cyl. 24 h g/kWh g/BHPhL42MC 177 130 165 121 3,0-4,0 0,8-1,2 0,6-0,9




4L42MC 3980 5420 VBS 980 ODS310 176 3750 746 805 4921 2460 690 2040 6700 6250 6350 95 12,05L42MC 4975 6775 VBS 1080 ODS330 176 4000 825 880 5669 2460 690 2140 6700 6250 6350 110 15,26L42MC 5970 8130 VBS 1180 ODS350 176 4200 900 940 6417 2460 690 2140 6700 6250 6350 125 16,47L42MC 6965 9485 VBS 1180 ODS375 176 4350 900 940 7165 2460 690 2160 6700 6250 6350 143 22,78L42MC 7960 10840 VBS 1280 ODS375 176 4500 975 1035 7913 2460 690 2200 6700 6250 6350 158 23,19L42MC 8955 12195 VBS 1280 ODS400 176 4600 975 1035 8661 2460 690 2200 6700 6250 6350 176 23,6

10L42MC 9950 13550 VBS 1280 ODS400 176 4700 975 1035 10065 2460 690 2200 6700 6250 6350 210 26,211L42MC 10945 14905 VBS 1380 ODS425 176 4800 1050 1095 10813 2460 690 2270 6700 6250 6350 229 29,912L42MC 11940 16260 VBS 1380 ODS425 176 4900 1050 1095 11561 2460 690 2270 6700 6250 6350 244 30,5

MAN B&W Two-stroke Propulsion SystemsS42MC-VBS4320-12960 kW (5880-17640 BHP)

A B S W C D

H1

H2

H3

E


The propeller diameter is optimised at 90% mcr, 136 rpm and 15.4 knThe strength calculation is made at 100% mcr, 136 rpm and 16.0 knThe propeller is calculated according to DnV, No Ice with high skewThe standard plants may be subject to change due to torsional vibrations

Main data






Dia

m.




kW bhp Type Type rpm mm min Engine Propeller**

4S42MC 4320 5880 VBS1080 ODS350 136 4350 825 880 4829 2670 900 2140 8050 7525 7300 109 16,55S42MC 5400 7350 VBS1180 ODS375 136 4600 900 940 5577 2670 900 2265 8050 7525 7300 125 20,16S42MC 6480 8820 VBS1280 ODS400 136 4850 975 1035 6325 2670 900 2511 8050 7525 7300 143 24,47S42MC 7560 10290 VBS1280 ODS425 136 5050 975 1035 7073 2670 900 2511 8050 7525 7300 160 27,58S42MC 8640 11760 VBS1380 ODS425 136 5200 1050 1095 7821 2670 900 2676 8050 7525 7300 176 30,59S42MC 9720 13230 VBS1380 ODS450 136 5350 1050 1095 8569 2670 900 2676 8050 7525 7300 195 32,7

10S42MC 10800 14700 VBS1460 ODS450 136 5550 1110 1140 10065 2670 900 2676 8050 7525 7300 232 36,011S42MC 11880 16170 VBS1460 ODS475 136 5650 1110 1140 10813 2670 900 2595 8050 7525 7300 249 38,412S42MC 12960 17640 VBS1560 ODS475 136 5750 1190 1210 11561 2670 900 2595 8050 7525 7300 269 42,4

A B S W C D

H1

H2

H3

EDia

m.

MAN B&W Two-stroke Propulsion SystemsS46MC-C-VBS5240-10480 kW (7140-14280 BHP)


S46MC-C-VBS standard programme

Main data


Type mm mm rpm bar m/s kW BHPS46MC-C 460 1932 129 19,0 8,31 1310 1785



g/kWh g/BHPh g/kWh g/BHPh kg/cyl. 24 h g/kWh g/BHPhS46MC-C 174 128 169 124 3,5-4,5 0,95-1,5 0,7-1,1




4S46MC 5240 7140 VBS 1180 ODS375 129 4700 900 940 4659 2924 986 2160 8600 8075 7850 133 19,75S46MC 6550 8925 VBS 1280 ODS400 129 4950 975 1035 5441 2924 986 2200 8600 8075 7850 153 22,26S46MC 7860 10710 VBS 1380 ODS425 129 5200 1050 1095 6223 2924 986 2270 8600 8075 7850 171 27,87S46MC 9170 12495 VBS 1380 ODS425 129 5400 1050 1095 7005 2924 986 2270 8600 8075 7850 197 29,58S46MC 10480 14280 VBS 1460 ODS450 129 5600 1100 1140 7787 2924 986 2350 8600 8075 7850 217 33,6

MAN B&W Two-stroke Propulsion SystemsL50MC-VBS5320-10640 kW(7240-14480 BHP)

A B S W C D

EH

3

H1

H2

The propeller diameter is optimised at 90% mcr, 148 rpm and 16.4 kn The propeller strength calculation is made at 100% mcr, 148 rpm and 17.0 knThe propeller is calculated according to DnV, No Ice with high skew The standard plants may be subject to change due to torsional vibrations


Dia

m.

Main data





g/kWh g/BHPh g/kWh g/BHPh kg/cyl. 24 h g/kWh g/BHPhL50MC 173 127 160 118 4,0-5,0 0,8-1,2 0,6-0,9


ENGINE PROPELLER DIMENSIONS IN MM DRY WEIGHTType Output* Hub OD-Box Speed Diameter A B C D E W H1 H2 H3 in tons (approx)

kW BHP Type Type rpm mm min. Engine Propeller**4L50MC 5320 7240 VBS1180 ODS350 148 4350 900 940 5712 2710 944 2140 7825 7350 7400 163 18,35L50MC 6650 9050 VBS1180 ODS375 148 4600 900 940 6602 2710 944 2160 7825 7350 7400 188 20,76L50MC 7980 10860 VBS1280 ODS400 148 4850 975 1035 7492 2710 944 2200 7825 7350 7400 215 25,57L50MC 9310 12670 VBS1380 ODS425 148 5050 1050 1095 8382 2710 944 2270 7825 7350 7400 249 29,48L50MC 10640 14480 VBS1380 ODS425 148 5200 1050 1095 9272 2710 944 2270 7825 7350 7400 276 30,6

A B S W C D

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3

H1

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MAN B&W Two-stroke Propulsion SystemsS50MC-VBS5720-11440 kW(7760-15520 BHP)

Main data






The propeller diameter is optimised at 90% mcr, 127 rpm and 16.4 kn The propeller strength calculation is made at 100% mcr, 127 rpm and 17.0 knThe propeller is calculated according to DnV, No Ice with high skewThe standard plants may be subject to change due to torsional vibrations




kW BHP Type Type rpm mm min. Engine Propeller**4S50MC 5720 7760 VBS1280 ODS375 127 4800 975 1010 5712 2950 1085 2140 8800 8250 8100 171 22,45S50MC 7150 9700 VBS1280 ODS400 127 5050 975 1035 6602 2950 1085 2200 8800 8250 8100 195 24,46S50MC 8580 11640 VBS1380 ODS425 127 5300 1095 1095 7492 2950 1085 2270 8800 8250 8100 225 30,47S50MC 10010 13580 VBS1460 ODS450 127 5500 1110 1140 8382 2950 1085 2350 8800 8250 8100 255 35,18S50MC 11440 15520 VBS1460 ODS450 127 5700 1110 1140 9272 2950 1085 2350 8800 8250 8100 288 36,3

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MAN B&W Two-stroke Propulsion SystemsS50MC-C-VBS6320-12640 kW(8580-17160 BHP)

Main data


Type mm mm rpm bar m/s kW BHPS50MC-C 500 2000 127 19,0 8,47 1580 2145



g/kWh g/BHPh g/kWh g/BHPh kg/cyl. 24 h g/kWh g/BHPhS50MC-C 171 126 159 117 4,0-5,0 0,95-1,5 0,7-1,1

The propeller diameter is optimised at 90% mcr, 127 rpm and 16.4 kn The propeller strength calculation is made at 100% mcr, 127 rpm and 17.0 kn The propellers are calculated according to DnV, No ice with high skew The standard plants may be subject to change du to torsional vibrations

S50MC-C-VBS standard programme



kW BHP Type Type rpm mm min. Engine Propeller**4S50MC-C 6320 8580 VBS1280 ODS400 127 4900 975 1035 5035 3150 1085 2200 8950 8375 8150 155 24,05S50MC-C 7900 10725 VBS1380 ODS425 127 5200 1050 1095 5875 3150 1085 2270 8950 8375 8150 181 29,16S50MC-C 9480 12870 VBS1380 ODS450 127 5450 1050 1095 6715 3150 1085 2350 8950 8375 8150 207 32,17S50MC-C 11060 15015 VBS1460 ODS450 127 5650 1110 1155 7555 3150 1085 2350 8950 8375 8150 238 35,58S50MC-C 12640 17160 VBS1560 ODS450 127 5850 1190 1225 8395 3150 1085 2350 8950 8375 8150 273 39,9

Reduction Gearboxes for CP Propellers

Gearbox range - compact versions

Type KV: Vertical offset, compact version(close-coupled with L23/30A engines)

Series: AMG 8, AMG 11, AMG 16

Standard reduction ratios: From 3,1:1 to 6,0:1

Power range: Up to 1280 kW (900 engine rpm)

Gearbox range - free-standing versions

Type VO: Vertical offset, free-standing version

Series: AMG 8, AMG 11, AMG 16,AMG 28, AMG 36, AMG 40

Type HO: Horizontal offset, free-standing version

Series: AMG 20

Standard reduction ratios: From 3,1:1 to 6,0:1

Power range: Up to 3920 kW (775 engine rpm)

Power Take-Off/Power Take-In

Flexstar PTOFlexstar is a modulized multi PTO system located atthe gearbox after end.The PTO’s can be arranged in centre, starboard, portand vertical sections. Up to 10 take-off positions areavailable - with and without individual remotely con-trolled hydraulic clutches.

1 2 3 4 6 7 8 9

10

5GEAR SERIES SPEED POWER SHAFT POSITIONS

rpm kWPTO AMG 8 1500/1800 800/900 All summarized

AMG 11 1500/1800 500/600 4, 5 & 6AMG 16 1500/1800 400/480 1+2+3, 7+8+9, 10

PTO with AMG 28 1500/1800 420/500 4, 5 & 6clutch 1500/1800 400/480 1+2+3, 7+8+9,10

GEAR SERIES SPEED POWER OUTPUT SHAFT(S)rpm kW

PTO AMG 8 1500/1800 350 One1500/1800 230 - each Two

AMG 11 1500/1800 700 OneAMG 16 1500/1800 230 - each TwoAMG 20 1500/1800 1000 One

PTO / PTI AMG 28 1000/1200 1500 One1500/1800 1500 One1500/1800 1500 - total One-two-three*

AMG 36 1000/1200 2000 OneAMG 40 1500/1800 2000 One

* Gearbox front-end design for short installation lenght

Flexstar range

Conventional range

Conventional PTO/PTIOutput and input shafts at the gearbox after end. No clutch built in.

Propeller diameter mm

7000

6000

5000

4000

3000

2000

1000

1000 3000 5000 7000 9000 11000

VBS 1680

VBS 1560

VBS 1460

VBS 1380VBS 1280

VBS 1180

VBS 1080VBS 980

VBS 860VBS 740

VB 640VB 560

VB 480

13000Engine power kW

150000

VB 560Diameter of propeller hubCP propeller with hydraulic servo motor in gearbox

Diameter of propeller hubCP propeller with hydraulic servo motor in hub

VBS 1280

MAN B&W CP Propellers

The standard propeller programmebasically comprises two types:

Type VBS- features propeller blade pitch set-ting by a hydraulic servo motor integrated in the propeller hub.

Type VB- features propellerblade pitch settingby a hydraulicservo motor integrated in thereduction gearbox.

Standard blade/hub materials are Ni-Al-Bronze and stainless steel isavailable on request.

The propellers are based on ”no ice”but can be delivered according to thehighest arctic ice classes.

Alphatronic Control Systems

Alphatronic II A

The standard remote control and safety system comprises:

• Bridge control panel• Bridge safety panel• Control units• Filter units for noise suppression• Power supply unit and battery

charger• Engine interface unit

Optionals

• Additional control panels for:BridgeBridge wing indoorBridge wing outdoorEngine control room

• Manoeuvre responsibility panels• Shaft alternator panels• Interface units for:

Joystick control systemsPower management systems

• Additional instrument panels

0

100

50

150

200

250

300 100

50 50

100

0

100

50

150

200

250

300 100

50 50

100Engine control room stand

Bridge stand

Alphatronic control unit

Engine interface unit

Main engineGovenor

Engine speed commandPitch command

Pitch indication

Propeller speed

Fuel index

Remote ControlSystem StructureDIagram

Alphatronic 2000

State-of-the-art The newly developed Alphatronic2000 control, monitoring and safetysystems set new standards in engineload control functions, safe operation,system redundancy, logical operatorpanels and simple serial interfacedinstallation.

MAN B&W CP Propellers and Control Systems for

MAN B&W Two-stroke EnginesL60MC, S60MC and S60MC-C7680-15360 kW(10400-20800 BHP)

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L60MC standard programme

S60MC standard programme

S60MC-C standard programme

* Engine output refers to load point L1** The masses are stated for 3,000 mm

stern tube and 6,000 mm propeller shaft

The propeller diameter is optimised at 90% mcr, 123 rpmand 17.4 kn

The strenght calculation is made at 100% mcr, 123 rpmand 18.0 kn





The propeller is calculated according to DnV, No Ice with high skewThe standard plants can be subject to change due to torsional vibrations

ENGINE PROPELLER

Type Output * Speed Hub OD-Box Diam. Q R W min Mass

kW BHP rpm Type Type mm mm mm mm ton**

4L60MC 7680 10400 123 VBS1380 ODS425 5200 1030 1131 2651 29,55L60MC 9600 13000 123 VBS1460 ODS450 5500 1100 1170 2676 34,56L50MC 11520 15600 123 VBS1560 ODS450 5750 1175 1242 2676 39,57L60MC 13440 18200 123 VBS1560 ODS500 5950 1175 1257 2919 44,28L60MC 15360 20800 123 VBS1680 ODS560 6150 1278 1338 2976 53,2

ENGINE PROPELLER

Type Output * Speed Hub OD-Box Diam. Q R W min Mass


4S60MC 8160 11120 105 VBS1460 ODS450 5650 1100 1170 2676 34,15S50MC 10200 13900 105 VBS1560 ODS450 6000 1175 1242 2676 39,26S60MC 12240 16680 105 VBS1680 ODS500 6300 1278 1333 2919 47,97S60MC 14280 19460 105 VBS1680 ODS560 6550 1278 1338 2976 54

ENGINE PROPELLER

Type Output* Speed Hub OD-Box Diam. Q R W min Mass


4S60MC-C 9020 12280 105 VBS1460 ODS450 5850 1100 1170 2676 35,25S60MC-C 11275 15350 105 VBS1560 ODS500 6150 1175 1257 2919 43,56S60MC-C 13530 18420 105 VBS1680 ODS560 6450 1278 1338 2976 53,3

Alpha Clutcher - for Auxiliary Propulsion Systems

The Alpha Clutcher is a new shaftlinede-clutching device for auxiliary pro-pulsion systems which meets theclass notations for redundant propul-sion. It facilitates reliable and simple“take home” and “take away” func-tions in two-stroke engine plants.

Main dataAlpha Clutcher range for two-stroke MC engines

TYPE CB 1 CB 2 CB 3 CB 4

Dimensions mm

Lenght [L] 1445 1635 1830 2160

Diameter [D] 1185 1340 1500 1770

Weight* [ton] 14 20 29 44

ENGINE Cylinder versions

S26MC 4-12

L35MC 4-12

S35MC 4-10 11-12

L42MC 4-7 8-10 10-12

S42MC 4-5 6-7 8-12

S46MC-C 4 5 6-8

L50MC 4 5-6 7-8

S50MC 4-5 6-8

S50MC-C 4 5-7 8

L60MC 4-5 6-8

S60MC 4 5-7

S60MC-C 4 5-6

* Approx weight incl intermediate shaft.

D

L


MAN B&W Four-stroke EnginesL32/40 and V32/402880-7680 kW(3930-10480 BHP)

The propeller diameter is optimised at 90% mcr, 100% rpm and 15,4 kn

The strength calculation is made at 100% mcr, 100% rpm and 16,0 kn

The propeller is calculated according to GLNo Ice with high skew

**The masses are stated for 3,000 mm stern tube and 6,000 mm propeller shaft

V32/40 standard programme

The propeller diameter is optimised at 90% mcr, 100% rpm and 15.4 kn

The strength calculation is made at 100% mcr, 100% rpm and 16.0 kn



L32/40 standard programme

ENGINE OUTPUT, mcr SPEED HUB OD-BOX PROPELLER Q R Wmin MASS

Type kW BHP rpm Type Type Diam, mm mm mm mm ton**200 VBS860 ODS250 3250 655 735 1970 8,8

6L32/40 2880 3930 160 VBS860 ODS280 3600 655 735 2000 9,9120 VBS980 ODS310 4150 746 805 2040 12,4200 VBS860 ODS280 3350 655 735 2000 9,7



9L32/40 4320 5895 160 VBS980 ODS310 4000 746 805 2040 13,2120 VBS1080 ODS330 4600 825 880 2140 17,2



12V32/40 5760 7860 160 VBS1080 ODS330 4300 821 945 2170 17,0120 VBS1280 ODS375 4950 957 1075 2511 23,5200 VBS1080 ODS330 4000 821 945 2170 16,6

14V32/40 6720 9170 160 VBS1180 ODS350 4500 885 996 2170 20,2120 VBS1280 ODS375 5150 957 1075 2511 25,7200 VBS1180 ODS330 4150 885 996 2170 19,0

16V32/40 7680 10480 160 VBS1180 ODS375 4650 885 996 2265 22,2120 VBS1380 ODS375 5350 1030 1131 2651 29,2

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6L40/54 4320 5880 150 VBS1080 ODS310 4100 825 880 2140 15,6110 VBS1180 ODS330 4800 825 880 2140 19190 VBS980 ODS310 3800 746 805 2040 12,9

7L40/54 5040 6860 150 VBS1080 ODS330 4250 825 880 2140 16,2110 VBS1280 ODS350 4950 975 1115 2200 23190 VBS1080 ODS310 3950 825 880 2140 15,9


9L40/54 6480 8820 150 VBS1180 ODS350 4550 900 1020 2160 20,3110 VBS1280 ODS400 5250 975 1115 2350 27,4


MAN B&W Four-stroke EnginesL40/54, L48/60 and L58/644320-12510 kW(5880-17010 BHP)

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The propeller is calculated according to GL,No Ice with high skew







9L48/60 9450 12870 140 VBS1380 ODS400 5100 1050 1175 2270 30,8100 VBS1560 ODS450 6000 1190 1350 2550 40,6






9L58/64 12510 17010 130 VBS1560 ODS450 5650 1190 1305 2550 41,290 VBS1680 ODS500 6700 1280 1380 2570 55,4

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