180126797-Mesin-Man-B-W-pdf.pdf

Contents

Four-stroke Propulsion systems L23/30A-K L23/ 30A-KV V .............. ...................... ............... .............. .............. .............. .............. .......... ... 800 8 00 V23/30 V23 /30A-VO A-VO ............... ...................... .............. .............. .............. .............. ............... .......... L21/31-V L21/ 31-VBS BS ............... ...................... .............. .............. .............. .............. ............... ..........1290 ..1290 L28/32A-V L28/ 32A-VO............ O................... .............. .............. ............... ............... .............. .............1470 ......1470 L27/38-V L27/ 38-VBS BS .............. ...................... ............... .............. .............. .............. .............. ...........2040 ....2040 V28/32 V28 /32A-VO A-VO ............... ...................... .............. .............. .............. .............. ............... ..........2940 ..2940 Two-stroke Propulsion Systems L35MC-VB L35MC -VBS.... S........... .............. .............. .............. .............. ............... ............... .............. .......260 2600 0 S35MC-VB S35MC -VBS S ............... ...................... .............. .............. .............. .............. ............... ..........2960 ..2960 L42MC-VB L42MC -VBS.... S........... .............. .............. .............. .............. ............... ............... .............. .......398 3980 0 S42MC-VB S42MC -VBS S ............... ...................... .............. .............. .............. .............. ............... ..........4320 ..4320 S46MC-VB S46MC -VBS S ............... ...................... .............. .............. .............. .............. ............... ..........5240 ..5240 L50MC-VB L50MC -VBS.... S........... .............. .............. .............. .............. ............... ............... .............. .......532 5320 0 S50MC-VB S50MC -VBS S ............... ...................... .............. .............. .............. .............. ............... ..........5720 ..5720 S50MC-C-V S50MC -C-VBS BS....... .............. .............. .............. ............... ............... .............. .............6320 ......6320

-

1280 128 0 1920 192 0 1935 193 5 2205 220 5 3060 306 0 3920 392 0

kW .............. ..................... .............. .......... ... 2 kW .............. ..................... .............. .......... ... 3 kW....... kW .............. .............. .............. .......... ... 4 kW .............. ..................... .............. .......... ... 5 kW .............. ..................... .............. .......... ... 6 kW .............. ..................... .............. .......... ... 7

-

7800 780 0 8880 888 0 11940 119 40 12960 129 60 10480 104 80 10640 106 40 11440 114 40 12640 126 40

kW .............. ..................... .............. .......... ... 8 kW .............. ..................... .............. .......... ... 9 kW .............. ..................... .............. ......... 10 kW .............. ..................... .............. ......... 11 kW .............. ..................... .............. ......... 12 kW .............. ..................... .............. ......... 13 kW .............. ..................... .............. ......... 14 kW .............. ..................... .............. ......... 15

Reduction gearboxes for CP Propellers KV, KV , VO and HO....... HO .............. .............. ............... ............... .............. .............. .............. ............... ............... .............. .............. .............. .............. ............... ............... .......... ...16 16 Power Take-Off/Power Take-Off/Power Take-In Flexstar Flex star and conven co nventio tional nal range r ange .............. ..................... .............. ............... ............... .............. .............. .............. .............. ............... ............... .......... ...17 17 CP Propellers VB and VBS range ran ge .............. ..................... ............... ............... .............. .............. .............. ............... ............... .............. .............. .............. .............. ............... ............ ....18 18 Alphatronic Control Systems IIA and 2000 ............... ...................... .............. .............. .............. .............. ............... ............... .............. .............. .............. ............... ............... .............. .............. .............. ......... 19 CP Propellers and Control Systems for Two-stroke Engines L60MC, S60MC and S60MC-C S60MC -C ........ ........... ....... ....... ....... ........ ......7680 ..7680 - 15360 kW ....... .......... ....... ....... ....... ........ ....... ..... 20 Alpha Clutcher Clutcher - for Auxiliary Propulsion Systems .............. ................ .............. ..................... .............. .............. .......21 21 CP Propellers and Control Systems for Four-stroke Engines L32/40 L32/ 40 and V32/40 V32/ 40 .............. ..................... ............... ............... .............. .............2880 ......2880 - 7680 768 0 kW .............. ..................... .............. ......... 22 L40/54, L48/60 and L58/64 ....... ........... ........ ....... ....... ....... ....... ........ ......4320 ..4320 - 12510 kW ....... .......... ....... ....... ....... ........ ....... ..... 23

MAN B&W Four-stroke Propulsion Systems L23/30A-KV 800-1280kW (1090-1740 BHP) C D

98 8

370

3 70

64 0

72 0

5 1 0 2

H

0 2 4

. m a i D

5 2 5

M

J

F

38 7

K Q

R

S

9 10

B

W

10 90

A

Standard programme ENGINE

REDUCTION GEAR

Type.

Series

PROPELLER

Type

Type

Output mcr

Speed

DIMENSIONS IN MM Diam

A

B

rpm

AM AMG 8 31KV8 VB 560 268 2200 AMG 8 39KV8 VB 640 214 2450 AMG 8 44KV9 VB 640 190 2600 AMG 16 52 52KV13 VB VB 740 159 2850 6L23/30A AMG 8 31KV8 VB 560 292 2250 960 kW AMG 8 39KV8 VB 640 233 2450 1305 BHP AMG 8 44KV9 VB 640 207 2600 AMG 16 52 52KV13 VB VB 740 173 2850 8L23/30A AMG 11 31 31KV11 VB VB 640 292 2350 1280 kW AMG 11 39 3 9KV11 VB V B 640 233 2600 1740 BHP AMG 11 44 4 4KV13 VB 740 207 2800 AMG 16 52 52KV13 VB VB 860 173 3100 The propeller is calculated according to DnV, DnV, No Ice with high skew

3975 3975 3975 4550 3975 3975 3975 4550 4953 4953 4953 5290

2898 2898 2898 2898 2898 2898 2898 2898 3628 3628 3628 3628

Main data

F

H

J

K

M

Q

R

W

4136 4136 4136 4660 4136 4136 4136 4660 5064 5064 5064 5400

1566 1566 1566 2090 1566 1566 1566 2090 1754 1754 1754 2090

328 328 328 318 328 328 328 318 318 318 318 318

1587 1587 1587 1587 1587 1587 1587 1587 1587 1587 1587 1587

770 770 770 1282 770 770 770 1282 950 950 950 1282

1077 1077 1077 1662 1077 1077 1077 1662 1325 1325 1325 1662

636 636 636 505 636 636 636 505 639 639 639 505

293 360 360 445 293 360 360 445 415 415 445 445

553 595 595 655 553 595 595 655 595 655 655 745

900 900 900 1200 900 900 900 1200 900 1200 1200 1350

min

Weight

BORE BORE

STRO STROKE KE

SPEE SPEED D

MEP MEP

PISTON SPE SPEED OU OUTPUT TPUT/C /CYL YLIN INDE DER R

Type

mm

mm

rpm

bar

m/s

kW

BHP

L23/30A-E L23/30A

225 225

300 300

825 900

16,3 17,9

8,25 9,00

133 160

181 217,5

Specific consumption ENGINE

FUEL OIL

Type L23/30A-E L23/30A

D

mm

6L23/30A-E 800 kW 1090 BHP

ENGIN NGINE E

C

mcr

LUBRICATING OIL 85% mcr

g/kWh

g/BHPh

188 190

138 140

g/kWh 187 189

mcr

g/BHPh

g/kWh

g/BHPh

137 139

1,0 1,0

0,7 0,7

ENGI ENGINE NE Type 6L23/30A-E

GEAR GEAR PROP PROP Dry weigh weightt in tons tons (appro (approx) x) Type Type Engine/Gear Prop* 31 31KV8 VB VB 560 15,0 2,7 39KV8 VB 640 15,0 3,4 44KV9 VB 640 15,0 3,5 52KV13 VB 740 17,6 4,4 6L23/30A 31KV8 VB 560 15,0 2,7 39KV8 VB 640 15,0 3,4 44KV9 VB 640 15,0 3,5 52KV13 VB 740 17,6 4,4 8L23/30A 31 3 1KV11 VB 640 17,9 3,4 39KV11 VB 640 17,9 3,8 44KV13 VB 740 17,9 4,5 52KV13 VB 860 20,1 6,1 * Weight incl 4.0 m shaft and 2.0 m stern tube

MAN B&W Four-stroke Propulsion Systems V23/30A-VO 1920kW (2610 BHP) 4670 1535

420

420

1035

1757

0 8 8 1

0 0 8 1

N

P

. m a i D

M

270

J

695

648

K Q

R

S

3830

W

L

A


REDUCTION GEAR

Type

Series

Type

PROPELLER Type

Output mcr 12V23/30A 1920 kW 2610 BHP

AMG AMG AMG AMG

16 16 28 28

31VO16 39VO16 48VO22 56VO28

VB VB VB VB

640 740 860 860

DIMENSIONS IN MM

Speed

Diam

rpm

mm

292 233 187 164

2550 2900 3250 3450

A

J

K

L

M

N

P

Q

R

W min

5956 5956 6091 6091

1662 1662 1693 1693

2126 2126 2261 2261

1090 1090 1500 1500

505 505 780 780

525 525 700 700

420 420 800 800

360 415 445 584

595 655 745 820

900 1200 1350 1600

ENGINE

GEAR

PROP

Type

Type

Type

Engine

Gear

Prop*

12V23/30A

31VO16 39VO16 48VO22 56VO28

VB 640 VB 740 VB 860 VB 860

17,5 17,5 17,5 17,5

6,0 6,0 8,1 8,1

3,8 5,3 7,1 8,5

Optional horizontal offset gearboxes: Series AMG 20 type 31HO20, 39HO20 and 48H022 The propeller is calculated according to DnV, No Ice with high skew

Main data

Weight

ENGINE

BORE

STROKE

SPEED

MEP

PISTON SPEED

Type

mm

mm

rpm

bar

m/s

kW

BHP

V23/30A

225

300

900

17,9

9,0

160

217,5

OUTPUT/CYLINDER

* Weight incl 4.0 m shaft and 2.0 m stern tube


FUEL OIL

Type 12V23/30A

mcr

DRY WEIGHT IN TONS (APPROX)

LUBRICATING 0IL 85% mcr

mcr

g/kWh

g/BHPh

g/kWh

g/BHPh

g/kWh

g/BHPh

191

141

190

140

1,0

0,7

MAN B&W Four-Stroke Propulsion Systems L21/31-VBS 1290-1935 kW (1755-2630 BHP)

C D

355

81 1

9 8 1 2

0 2 4

. m a i D

5 4 7

1065 1940

658

851

2241 L

M

S

B

W

A


REDUCTION GEAR

Type

Series

PROPELLER

Type

Type

Output mcr

DIMENSIONS IN MM

Speed

Diam

rpm

mm

A

B

C

D

AMG18EV 36VO18 VBS640 279 2350 5476 3235 4185 1598 46VO18 VBS640 217 2650 5476 3235 4185 1598 57VO18 VBS740 174 2950 5476 3235 4185 1598 68VO18 VBS860 147 3250 5476 3235 4185 1598 7L21/31 AMG18EV 36VO18 VBS640 279 2450 5750 3590 4540 1598 1505 kW 46VO18 VBS740 217 2750 5750 3590 4540 1598 2047 bhp 57VO18 VBS740 174 3050 5750 3590 4540 1598 68VO18 VBS860 147 3350 5750 3590 4540 1598 8L21/31 AMG18EV 36VO18 VBS640 279 2550 6186 3945 4895 1598 1720 kW 46VO18 VBS740 217 2850 6186 3945 4895 1598 2340 bhp 57VO18 VBS860 174 3150 6186 3945 4895 1598 68VO18 VBS860 147 3450 6186 3945 4895 1598 9L21/31 AMG18EV 36VO18 VBS740 279 2650 6541 4300 5250 1598 1935 kW 46VO18 VBS740 217 2950 6541 4300 5250 1598 2630 bhp 57VO18 VBS860 174 3250 6541 4300 5250 1598 68VO18 VBS860 147 3550 6541 4300 5250 1598 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

Main data

L

M

W

1018 1018 1018 1018 1018 1018 1018 1018 1018 1018 1018 1018 1018 1018 1018 1018

2029 2029 2029 2029 2029 2029 2029 2029 2029 2029 2029 2029 2029 2029 2029 2029

550 550 569 653 550 569 569 653 550 569 653 653 569 569 653 653

596 596 655 743 596 655 655 743 596 655 743 743 655 655 743 743

1200 1200 1300 1400 1200 1300 1300 1400 1200 1300 1300 1400 1300 1300 1400 1400

Weight

BORE STROKE SPEED

MEP

PISTON SPEED

OUTPUT/ CYLINDER

Type

mm

mm

rpm

bar

m/s

kW

BHP

L21/31

210

310

1000

24,1

10,3

215

292


FUEL OIL

Type L21/31

H

min

6L21/31 1290 kW 1755 bhp

ENGINE

G

mcr


g/kWh

g/BHPh

181

133

g/kWh g/BHPh 181

133

mcr g/kWh

g/BHPh

0,8

0,6

ENGINE Gear

Prop Dry weight in tons (appr.) ENGINE Gear

Type Type Type Engine Gear Prop* 6L 36VO18 VBS640 13,9 3,2 Data 21/31 46VO18 VBS640 13,9 available 3,6 upon 57VO18 VBS740 13,9 4,5 68VO18 VBS860 13,9 request 5,7 7L 36VO18 VBS640 15,2 3,6 Data 21/31 46VO18 VBS740 15,2 available 4,4 upon 57VO18 VBS740 15,2 4,9 68VO18 VBS860 15,2 request 6,2 * Weight incl 4.0 m shaft and 2.0 m stern tube

Prop Dry weight in tons (appr.)

Type Type Type 8L 36VO18 VBS640 21/31 46VO18 VBS740 57VO18 VBS860 68VO18 VBS860 9L 36VO18 VBS740 21/31 46VO18 VBS740 57VO18 VBS860 68VO18 VBS860

Engine 16,6 16,6 16,6 16,6 18,2 18,2 18,2 18,2

Gear

Prop* 3,7 4,6 6,1 6,5 4,5 Data available 5,0 upon 6,4 request 7,0 Data available upon request

MAN B&W Four-Stroke Propulsion Systems L28/32A-VO 1470-2205 kW (2000-3000 BHP) C 1770

585

480

480

G

1160

. m a i D

H

0 0 3 2

P

N

M

E J

F

808

K Q

R

S

1300

B

W

L

A


REDUCTION GEAR

Type

Series

Type

PROPELLER Type

Output mcr

DIMENSIONS IN MM

Speed

Diam

rpm

mm

A

B

C

E

F

G

AMG 11 31VO11 VB 640 252 2600 6145 4340 5330 322 780 1147 AMG 16 39VO16 VB 740 201 2850 6482 4340 5330 322 780 1147 AMG 28 48VO22 VB 860 161 3200 6599 4340 5330 322 780 1147 AMG 28 56VO28 VB 860 141 3500 6599 4340 5330 322 780 1147 7L28/32A AMG 16 31VO16 VB 740 252 2650 6892 4750 5810 252 710 1147 1715 kW AMG 16 39VO16 VB 860 201 3000 6892 4750 5810 252 710 1147 2330 BHP AMG 28 48VO22 VB 860 161 3300 7027 4750 5810 252 710 1147 AMG 28 56VO28 VB 980 141 3600 7027 4750 5810 252 710 1147 8L28/32A AMG 16 31VO16 VB 740 252 2800 7372 5230 6290 252 710 1147 1960 kW AMG 28 39VO20 VB 860 201 3100 7507 5230 6290 252 710 1147 2665 BHP AMG 28 48VO22 VB 860 161 3450 7507 5230 6290 252 710 1147 AMG 28 56VO28 VB 980 141 3750 7507 5230 6290 252 710 1147 9L28/32A AMG 28 31VO20 VB 740 248 2850 8039 5780 6770 322 780 1259 2205 kW AMG 28 39VO20 VB 860 201 3200 8039 5780 6770 322 780 1259 3000 BHP AMG 28 48VO22 VB 980 161 3550 8039 5780 6770 322 780 1259 AMG 28 56VO28 VB 980 141 3850 8039 5780 6770 322 780 1259 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

Main data

K

L

M

N

P

Q

R

W

2061 2061 2061 2061 2061 2061 2061 2061 2061 2061 2061 2061 2147 2147 2147 2147

1325 1662 1693 1693 1662 1662 1693 1693 1662 1693 1693 1693 1693 1693 1693 1693

1789 2142 2277 2277 2142 2142 2277 2277 2142 2277 2277 2277 2259 2259 2259 2259

1090 1090 1500 1500 1090 1090 1500 1500 1090 1500 1500 1500 1500 1500 1500 1500

460 505 780 780 505 505 780 780 505 780 780 780 780 780 780 780

525 525 700 700 525 525 700 700 525 700 700 700 700 700 700 700

420 420 800 800 420 420 800 800 420 800 800 800 800 800 800 800

360 415 445 445 415 445 445 584 415 445 445 584 415 445 584 584

595 655 745 745 655 745 745 820 655 745 745 820 655 745 745 820

900 1200 1350 1350 1200 1350 1350 1600 1200 1350 1350 1600 1200 1350 1350 1600

Weight

BORE STROKE SPEED

MEP

PISTON SPEED

OUTPUT/ CYLINDER

Type

mm

mm

rpm

bar

m/s

kW

BHP

L28/32A

280

320

775

19,3

8,3

245

333

Specific consumption ENGINE Type L28/32A

J

min

6L28/32A 1470 kW 2000 BHP

ENGINE

H

FUEL OIL mcr

85% mcr

g/kWh

g/BHPh

188

138

g/kWh g/BHPh 187

137

LUBRICATING OIL mcr g/kWh g/BHPh 1,0 0,7

ENGINE Gear Prop Dry weight in tons (appr.) ENGINE Gear Prop Dry weight in tons (appr.) Type Type Type Engine Gear Prop* Type Type Type Engine Gear Prop* 6L 31VO11 VB 640 19,0 3,8 3,9 8L 31VO16 VB 740 23,5 6,0 5,4 28/32A 39VO16 VB 740 19,0 6,0 5,1 28/32A 39VO20 VB 860 23,5 8,1 6,5 48VO22 VB 860 19,0 8,1 6,1 48VO22 VB 860 23,5 8,1 7,3 56VO28 VB 860 19,0 8,1 7,2 56VO28 VB 980 23,5 8,1 8,4 7L 31VO16 VB 740 21,0 6,0 4,5 9L 31VO20 VB 740 26,5 8,1 5,5 28/32A 39VO16 VB 860 21,0 6,0 5,8 28/32A 39VO20 VB 860 26,5 8,1 7,1 48VO22 VB 860 21,0 8,1 7,1 48VO22 VB 980 26,5 8,1 8,3 56VO28 VB 980 21,0 8,1 8,3 56VO28 VB 980 26,5 8,1 8,6 * Weight incl 4.0 m shaft and 2.0 m stern tube

MAN B&W Four-Stroke Propulsion Systems L27/38-VBS 2040-3060 kW (2775-4160 BHP) C D

445

G

. m a i D

0 6 9 1

H

0 3 5

0 3 5

H

0 0 7 0 8 7

1452 1693 (2689)

82 0

905

2279 (3071) Q

R

S

1500

B A

W

Figures in brackets for reduction gear AMG55EV


REDUCTION GEAR

Type

Series

PROPELLER

Type

Type

Output mcr 6L27/38 2040 kW 2775 BHP

AMG28EV

AMG55EV 7L27/38 2380 kW 3235 BHP

AMG28EV

AMG55EV 8L27/38 2720 kW 3700 BHP

AMG28EV

AMG55EV 9L27/38 3060 kW 4160 BHP

AMG28EV

AMG55EV

31VO20 39VO20 45VO30 56VO28 60VO55 31VO20 39VO20 45VO30 56V028 60VO55 31VO20 39VO30 45VO30 50VO30 60VO55 31VO30 39VO30 45VO30 50VO30 60VO55

VBS740 VBS740 VBS860 VBS860 VBS860 VBS740 VBS860 VBS860 VBS860 VBS980 VBS860 VBS860 VBS860 VBS860 VBS980 VBS860 VBS860 VBS860 VBS980 VBS980

DIMENSIONS IN MM

Speed

Diam

rpm

mm

256 208 177 145 133 256 208 177 145 133 256 208 177 161 133 256 208 177 161 133

2650 2950 3200 3500 3650 2800 3100 3350 3650 3800 2900 3200 3450 3600 3950 2950 3300 3550 3700 4050

A

B

C

D

G

H

Q

R

W min

6229 6229 6229 6229 7033 6674 6674 6674 6674 7478 7119 7119 7119 7119 7923 7563 7563 7563 7563 8334

3962 3962 3962 3962 3962 4407 4407 4407 4407 4407 4852 4852 4852 4852 4852 5263 5263 5263 5263 5263

5070 5070 5070 5070 5070 5515 5515 5515 5515 5515 5960 5960 5960 5960 5960 6405 6405 6405 6405 6405

1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940 1940

1166 1166 1166 1166 1166 1166 1166 1166 1166 1166 1256 1256 1256 1256 1256 1268 1268 1268 1268 1268

2267 2267 2267 2267 2267 2267 2267 2267 2267 2267 2237 2237 2237 2237 2237 2427 2427 2427 2427 2427

569 569 653 653 653 569 653 653 653 746 653 653 653 653 746 653 653 653 746 746

655 655 743 743 743 655 743 743 743 806 743 743 743 743 806 743 743 743 806 806

1300 1300 1400 1400 1400 1300 1400 1400 1450 1500 1400 1400 1450 1450 1500 1400 1400 1400 1500 1550

The propeller diameter is opti mized at 85% MCR, 98% rpm and 14,0 kn. The strength calculat ion is made at 100% MCR, 100% rpm and 14,5 kn. The propeller is calculat ed according to LRS, No Ice with high skew

Weight

Main data ENGINE

BORE STROKE SPEED

MEP

PISTON SPEED

OUTPUT/ CYLINDER

Type

mm

mm

rpm

bar

m/s

kW

BHP

L27/38

270

380

800

23,5

10,1

340

462


FUEL OIL

Type L27/38

mcr

LUBRICATING OIL

85% mcr

g/kWh

g/BHPh

182

134

g/kWh g/BHPh 180

132

mcr g/kWh 0,8

g/BHPh 0,6

ENGINE Gear Type

Type 31VO20 6L 39VO20 27/38 45VO30 56VO28 60VO55 31VO20 7L 39VO20 27/38 45VO30 56VO28 60VO55

Prop Dry weight in tons (appr.) Type Engine VBS740 30 VBS740 30 VBS860 30 VBS860 30 VBS860 30 VBS740 33,5 VBS860 3 3,5 VBS860 33,5 VBS860 33,5 VBS980 33,5

Gear 8,5 8,5 8,5 8,5 14 8,5 8,5 8,5 8,5 14

Prop.* 4,7 5,3 5,7 7,0 7,3 5,3 6,4 6,6 7,7 9,4

ENGINE Gear Type 8L 27/38

9L 27/38

Type 31VO20 39VO30 45VO30 50VO30 60VO55 31VO30 39VO30 45VO30 50VO30 60VO55

Prop Dry weight in tons (appr.) Type Engine VBS860 37 VBS860 37 VBS860 37 VBS860 37 VBS980 37 VBS860 40,5 VBS860 40,5 VBS860 40,5 VBS980 40,5 VBS980 40,5

Gear 8,5 8,5 8,5 8,5 14 8,5 8,5 8,5 8,5 14

Prop.* 6,4 6,8 7,6 7,8 9,6 6,7 7,1 8,1 9,4 10

MAN B&W Four-stroke Propulsion Systems V28/32A-VO 2940-3920 kW (4000-5330 BHP) C 1550

510

510

1460

970

. m a i D

1045

H

5 3 2 2

P

N

M

280

J

980

860 B

K Q

R

S

L

W

A


REDUCTION GEAR

Type

Series

Type

PROPELLER Type

Output mcr 12V28/32A 2940 kW 4000 BHP 16V28/32A 3920 kW 5330 BHP

AMG 28 AMG 28 AMG 28 AMG 40 AMG 28 AMG 36 AMG 36 AMG 40

31VO30 39VO30 45VO30 51VO36 31VO30 34VO36 41VO36 51VO36

VB 860 VB 860 VB 980 VB 980 VB 860 VB 860 VB 980 VB1080

DIMENSIONS IN MM

Speed

Diam

rpm

mm

248 201 171 151 248 231 191 151

3050 3400 3700 3950 3250 3350 3750 4250

A

B

C

H

J

K

L

M

N

P

Q

R

W

min 7044 7044 7044 7496 8036 8516 8516 8516

4870 4870 4870 4870 5890 5890 5890 5890

5560 5560 5560 5560 6580 6580 6580 6580

2152 2152 2152 2152 2212 2212 2212 2212

1693 1693 1693 2155 1693 2155 2155 2155

2174 2174 2174 2626 2242 2626 2626 2626

1500 1500 1500 1840 1500 1570 1570 1840

780 780 780 1050 780 925 925 1050

700 700 700 870 700 736 736 870

800 800 800 1045 800 911 911 1045

445 445 584 584 445 445 584 600

745 745 820 820 745 745 820 855

1350 1350 1600 1600 1350 1350 1600 1600

Engine

Gear

Prop*

Type

Type

Type

Engine

Gear

Prop*

12V28/32A

31VO30 39VO30 45VO30 51VO36 31VO30 34VO36 41VO36 51VO36

VB 860 VB 860 VB 980 VB 980 VB 860 VB 860 V B 980 VB 1080

29,5 29,5 29,5 29,5 37,0 37,0 37,0 37,0

8,1 8,1 8,1 13,4 8,1 11,6 11,6 13,4

7,1 7,9 8,6 8,9 8,1 8,2 10,0 13,2

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

Main data

Weight STROKE SPEED

MEP

PISTON SPEED OUTPUT/CYLINDER

ENGINE

BORE

Type

mm

mm

rpm

bar

m/s

kW

BHP

V28/32A

280

320

775

19,3

8,3

245

333


FUEL OIL

Type V28/32A

16V28/32A

mcr


mcr

g/kWh

g/BHPh

g/kWh

g/BHPh

g/kWh

g/BHPh

189

139

188

138

1,0

0,7

Dry weight in tons (approx)

* Weight incl 4,0 m shaft and 2,0 m stern tube

MAN B&W Two-stroke Propulsion Systems L35MC-VBS 2600-7800 kW (3520-10560 BHP)

2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D

L35MC-VBS standard programme ENGINE Type

PROPELLER

Output*

4L35MC 5L35MC 6L35MC 7L35MC 8L35MC 9L35MC 10L35MC 11L35MC 12L35MC

Hub

OD-Box

Speed

DIMENSIONS IN MM Diameter

kW

BHP

Type

Type

rpm

mm

2600 3250 3900 4550 5200 5850 6500 7150 7800

3520 4400 5280 6160 7040 7920 8800 9680 10560

VBS 860 VBS 860 VBS 980 VBS 980 VBS 980 VBS 1080 VBS 1080 VBS 1180 VBS 1180

ODS250 ODS280 ODS280 ODS310 ODS310 ODS330 ODS330 ODS350 ODS350

210 210 210 210 210 210 210 210 210

3150 3300 3450 3600 3700 3800 3900 4000 4100

The propeller diameter is optimised at 90% mcr, 210 rpm and 14.5 kn The strength calculation is made at 100% mcr, 210 rpm and 15.0 kn The propeller is calculated according to DnV, No Ice with high skew The standard plants may be subject to change due to torsional vibrations

B

C

D

E

W

655 655 746 746 746 825 825 900 900

735 735 785 785 805 880 880 940 940

4000 4600 5200 5800 6400 7000 7600 8200 8800

1980 1980 1980 1980 1980 1980 1980 1980 1980

550 550 550 550 550 550 550 550 550

1970 2000 2000 2040 2040 2140 2140 2140 2140

H1

H2

H3

5200 5200 5200 5200 5200 5200 5200 5200 5200

4900 4900 4900 4900 4900 4900 4900 4900 4900

5025 5025 5025 5025 5025 5025 5025 5025 5025

min

in tons (approx) Engine 50 58 67 75 83 92 108 118 126

Propeller** 9,1 9,5 10,3 11,8 12,3 13,9 14,7 16,5 17,2

* Engine output refers to load point L1 ** Weight incl 6.0 m shaft and 3.0 m stern tube H1: Vertical lift H2: Tilted lift - H3: Double jib crane

Main data ENGINE

DRY WEIGHT

A

Specific consumption

BORE

STROKE

SPEED

MEP


Type

mm

mm

rpm

bar

m/s

kW

BHP

L35MC

350

1050

210

18,4

7,35

650

880

ENGINE Type L35MC

FUEL OIL Layout point L1

LUBRICATING OIL

Layout point L2

CYLINDER OIL

approx

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/bhph

177

130

171

126

2,0-3,0

0,8-1,2

0,6-0,9

MAN B&W Two-stroke Propulsion Systems S35MC-VBS 2960-8880 kW (4040-12120 BHP)

2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D

S35MC-VBS standard programme ENGINE Type

PROPELLER

Output*

4S35MC 5S35MC 6S35MC 7S35MC 8S35MC 9S35MC 10S35MC 11S35MC 12S35MC

DIMENSIONS IN MM

Hub

OD-Box

Speed

Diameter

kW

BHP

Type

Type

rpm

mm

2960 3700 4440 5180 5920 6660 7400 8140 8880

4040 5050 6060 7070 8080 9090 10100 11110 12120



173 173 173 173 173 173 173 173 173

3550 3750 3950 4100 4250 4350 4450 4550 4650


* ** H1: H2:

A

B

C

D

E

DRY WEIGHT

W

H1

H2

H3

min 655 746 746 825 825 900 900 975 975

735 805 805 880 880 940 940 1035 1035

4035 4635 5235 5835 6435 7035 7635 8235 9435

2200 2200 2200 2200 2200 2200 2200 2200 2200

650 650 650 650 650 650 650 650 650

2000 2040 2070 2070 2265 2265 2265 2511 2676

6425 6425 6425 6425 6425 6425 6425 6425 6425

6050 6050 6050 6050 6050 6050 6050 6050 6050

5925 5925 5925 5925 5925 5925 5925 5925 5925

in tons (approx) Engine

Propeller**

57 65 75 84 93 103 122 132 141

9,6 12,5 14,0 16,6 18,5 20,4 21,1 24,8 27,4

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

Main data


ENGINE Type

BORE mm

STROKE mm

SPEED rpm

MEP bar

S35MC

350

1400

173

19,1

PISTON SPEED OUTPUT/CYLINDER m/s kW BHP 8,07

740

1010

ENGINE Type S35MC


Layout point L1

LUBRICATING OIL approx

CYLINDER OIL

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

178

131

173

127

2,0-3,0

0,95-1,5

0,7-1,1


2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D


PROPELLER

Output*

4L42MC 5L42MC 6L42MC 7L42MC 8L42MC 9L42MC 10L42MC 11L42MC 12L42MC

Hub

OD-Box

Speed


kW

BHP

Type

Type

rpm

mm

3980 4975 5970 6965 7960 8955 9950 10945 11940

5420 6775 8130 9485 10840 12195 13550 14905 16260



176 176 176 176 176 176 176 176 176

3750 4000 4200 4350 4500 4600 4700 4800 4900


* ** H1: H2:

A

B

746 825 900 900 975 975 975 1050 1050

805 880 940 940 1035 1035 1035 1095 1095

DRY WEIGHT

D

E

W

2460 2460 2460 2460 2460 2460 2460 2460 2460

690 690 690 690 690 690 690 690 690

2040 2140 2140 2160 2200 2200 2200 2270 2270

H1

H2

H3

6700 6700 6700 6700 6700 6700 6700 6700 6700

6250 6250 6250 6250 6250 6250 6250 6250 6250

6350 6350 6350 6350 6350 6350 6350 6350 6350

min 4921 5669 6417 7165 7913 8661 10065 10813 11561

in tons (approx) Engine 95 110 125 143 158 176 210 229 244

Propeller** 12,0 15,2 16,4 22,7 23,1 23,6 26,2 29,9 30,5


Main data ENGINE

C


BORE

STROKE

SPEED

MEP


Type

mm

mm

rpm

bar

m/s

kW

BHP

L42MC

420

1360

176

18,0

7,98

995

1355

ENGINE Type L42MC


LUBRICATING OIL

Layout point L2

CYLINDER OIL

approx

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

177

130

165

121

3,0-4,0

0,8-1,2

0,6-0,9


2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D


PROPELLER

Output*

4S42MC 5S42MC 6S42MC 7S42MC 8S42MC 9S42MC 10S42MC 11S42MC 12S42MC

DIMENSIONS IN MM

Hub

OD-Box

Speed

Diameter

kW

bhp

Type

Type

rpm

mm

4320 5400 6480 7560 8640 9720 10800 11880 12960

5880 7350 8820 10290 11760 13230 14700 16170 17640

VBS1080 VBS1180 VBS1280 VBS1280 VBS1380 VBS1380 VBS1460 VBS1460 VBS1560


136 136 136 136 136 136 136 136 136

4350 4600 4850 5050 5200 5350 5550 5650 5750


* ** H1: H2:

A

B

C

D

E

DRY WEIGHT

W

H1

H2

H3

min 825 900 975 975 1050 1050 1110 1110 1190

880 940 1035 1035 1095 1095 1140 1140 1210

4829 5577 6325 7073 7821 8569 10065 10813 11561

2670 2670 2670 2670 2670 2670 2670 2670 2670

900 900 900 900 900 900 900 900 900


2140 2265 2511 2511 2676 2676 2676 2595 2595

8050 8050 8050 8050 8050 8050 8050 8050 8050

7525 7525 7525 7525 7525 7525 7525 7525 7525

7300 7300 7300 7300 7300 7300 7300 7300 7300

109 125 143 160 176 195 232 249 269

Propeller** 16,5 20,1 24,4 27,5 30,5 32,7 36,0 38,4 42,4


Main data


ENGINE Type

BORE mm

STROKE mm

SPEED rpm

MEP bar

S42MC

420

1764

136

19,5

PISTON SPEED OUTPUT/CYLINDER m/s kW BHP 8,00

1080

1470

ENGINE Type S42MC


Layout point L1

LUBRICATING OIL approx

CYLINDER OIL

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

177

130

171

126

3,0-4,0

0,95-1,5

0,7-1,1

MAN B&W Two-stroke Propulsion Systems S46MC-C-VBS 5240-10480 kW (7140-14280 BHP)

2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D

S46MC-C-VBS standard programme ENGINE Type

PROPELLER

Output*

4S46MC 5S46MC 6S46MC 7S46MC 8S46MC

Hub

OD-Box

Speed


kW

BHP

Type

Type

rpm

mm

5240 6550 7860 9170 10480

7140 8925 10710 12495 14280

VBS 1180 VBS 1280 VBS 1380 VBS 1380 VBS 1460

ODS375 ODS400 ODS425 ODS425 ODS450

129 129 129 129 129

4700 4950 5200 5400 5600


A

B

C

D

E

W

900 975 1050 1050 1100

940 1035 1095 1095 1140

4659 5441 6223 7005 7787

2924 2924 2924 2924 2924

986 986 986 986 986

2160 2200 2270 2270 2350

H1

H2

H3

8600 8600 8600 8600 8600

8075 8075 8075 8075 8075

7850 7850 7850 7850 7850

min

in tons (approx) Engine 133 153 171 197 217

Propeller** 19,7 22,2 27,8 29,5 33,6

* Engine output refers to load point L1 ** Weight incl 6.0 m shaft and 3.0 m stern tube H1: Vertical lift H2: Tilted lift - H3: Double jib crane

Main data ENGINE

DRY WEIGHT


BORE

STROKE

SPEED

MEP


Type

mm

mm

rpm

bar

m/s

kW

BHP

S46MC-C

460

1932

129

19,0

8,31

1310

1785

ENGINE Type S46MC-C


LUBRICATING OIL

Layout point L2

CYLINDER OIL

approx

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

174

128

169

124

3,5-4,5

0,95-1,5

0,7-1,1


2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D


PROPELLER

Output*

4L50MC 5L50MC 6L50MC 7L50MC 8L50MC

DIMENSIONS IN MM

Hub

OD-Box

Speed

Diameter

kW

BHP

Type

Type

rpm

mm

5320 6650 7980 9310 10640

7240 9050 10860 12670 14480

VBS1180 VBS1180 VBS1280 VBS1380 VBS1380


148 148 148 148 148

4350 4600 4850 5050 5200

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

A

B

C

D

E

DRY WEIGHT

W

H1

H2

H3

min. 900 900 975 1050 1050 * ** H1: H2:

940 940 1035 1095 1095

5712 6602 7492 8382 9272

2710 2710 2710 2710 2710

944 944 944 944 944


2140 2160 2200 2270 2270

7825 7825 7825 7825 7825

7350 7350 7350 7350 7350

7400 7400 7400 7400 7400

163 188 215 249 276

Propeller** 18,3 20,7 25,5 29,4 30,6


Main data

Specific consumption PISTON SPEED OUTPUT/CYLINDER

ENGINE

BORE

STROKE

SPEED

MEP

Type

mm

mm

rpm

bar

m/s

kW

BHP

L50MC

500

1620

148

17,0

7,99

1330

1810

ENGINE Type L50MC


LUBRICATING OIL

Layout point L2

CYLINDER OIL

approx

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

173

127

160

118

4,0-5,0

0,8-1,2

0,6-0,9


2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D


PROPELLER

Output*

4S50MC 5S50MC 6S50MC 7S50MC 8S50MC

DIMENSIONS IN MM

Hub

OD-Box

Speed

Diameter

kW

BHP

Type

Type

rpm

mm

5720 7150 8580 10010 11440

7760 9700 11640 13580 15520



127 127 127 127 127

4800 5050 5300 5500 5700

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

A

C

D

E

W

H1

H2

H3

min. 975 975 1095 1110 1110 * ** H1: H2:

1010 1035 1095 1140 1140

5712 6602 7492 8382 9272

2950 2950 2950 2950 2950

1085 1085 1085 1085 1085


2140 2200 2270 2350 2350

8800 8800 8800 8800 8800

8250 8250 8250 8250 8250

8100 8100 8100 8100 8100

171 195 225 255 288

Propeller** 22,4 24,4 30,4 35,1 36,3


Main data ENGINE

B

DRY WEIGHT


BORE

STROKE

SPEED

MEP


Type

mm

mm

rpm

bar

m/s

kW

BHP

S50MC

500

1910

127

18,0

8,09

1430

1940

ENGINE Type S50MC


LUBRICATING OIL

Layout point L2

CYLINDER OIL

approx

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

171

126

159

117

4,0-5,0

0,95-1,5

0,7-1,1

MAN B&W Two-stroke Propulsion Systems S50MC-C-VBS 6320-12640 kW (8580-17160 BHP)

2 H

3 H

1 H

. m a i D

E

A

B

S

W

C

D

S50MC-C-VBS standard programme ENGINE Type 4S50MC-C 5S50MC-C 6S50MC-C 7S50MC-C 8S50MC-C

PROPELLER

Output*

DIMENSIONS IN MM

Hub

OD-Box

Speed

Diameter

kW

BHP

Type

Type

rpm

mm

6320 7900 9480 11060 12640

8580 10725 12870 15015 17160



127 127 127 127 127

4900 5200 5450 5650 5850

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

A

B

C

D

E

DRY WEIGHT

W

H1

H2

H3

min. 975 1050 1050 1110 1190 * ** H1: H2:

1035 1095 1095 1155 1225

5035 5875 6715 7555 8395

3150 3150 3150 3150 3150

1085 1085 1085 1085 1085


2200 2270 2350 2350 2350

8950 8950 8950 8950 8950

8375 8375 8375 8375 8375

8150 8150 8150 8150 8150

155 181 207 238 273

Propeller** 24,0 29,1 32,1 35,5 39,9


Main data

Specific consumption PISTON SPEED OUTPUT/CYLINDER

ENGINE

BORE

STROKE

SPEED

MEP

Type

mm

mm

rpm

bar

m/s

kW

BHP

S50MC-C

500

2000

127

19,0

8,47

1580

2145

ENGINE Type S50MC-C


LUBRICATING OIL

Layout point L2

CYLINDER OIL

approx

g/kWh

g/BHPh

g/kWh

g/BHPh

kg/cyl. 24 h

g/kWh

g/BHPh

171

126

159

117

4,0-5,0

0,95-1,5

0,7-1,1

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 PTO

Flexstar is a modulized multi PTO system located at the gearbox after end. The PTO’s can be arranged in centre, starboard, port and vertical sections. Up to 10 take-off positions are available - with and without individual remotely controlled hydraulic clutches. Flexstar range 10

GEAR SERIES PTO

PTO with

SPEED rpm

POWER kW

SHAFT POSITIONS

AMG 8

1500/1800

800/900

All summarized

AMG 11

1500/1800

500/600

4, 5 & 6

AMG 16

1500/1800

400/480

1+2+3, 7+8+9, 10

AMG 28

1500/1800

420/500

4, 5 & 6

1500/1800

400/480

1+2+3, 7+8+9,10

clutch

Conventional PTO/PTI

Output and input shafts at the gearbox after end. No clutch built in.

Conventional range GEAR SERIES PTO

PTO / PTI

AMG 8

SPEED rpm

POWER kW

OUTPUT SHAFT(S)

1500/1800

350

One

1500/1800

230 - each

Two

AMG 11

1500/1800

700

One

AMG 16

1500/1800

230 - each

Two

AMG 20

1500/1800

1000

One

AMG 28

1000/1200

1500

One

1500/1800

1500

One

1500/1800

1500 - total

One-two-three*

AMG 36

1000/1200

2000

One

AMG 40

1500/1800

2000

One

* Gearbox front-end design for short installation lenght

5

1

2

3

4

6

7

8

9

MAN B&W CP Propellers The standard propeller programme basically comprises two types: Type VBS - features propeller blade pitch setting by a hydraulic servo motor integrated in the propeller hub.

Standard blade/hub materials are Ni-Al-Bronze and stainless steel is available on request. The propellers are based on ”no ice” but can be delivered according to the highest arctic ice classes.

Type VB - features propeller blade pitch setting by a hydraulic servo motor integrated in the reduction gearbox.

Propeller diameter mm

7000

6000

VBS 1680 VBS 1560

5000

VBS 1460 VBS 1380 VBS 1280 VBS 1180

4000

VBS 1080

3000

VBS 980 VBS 860 VBS 740 VB 640 VB 560 VB 480

2000

1000

VB 560

Diameter of propeller hub CP propeller with hydraulic servo motor in gearbox

VBS 1280

Diameter of propeller hub CP propeller with hydraulic servo motor in hub

0 1000

3000

5000

7000

9000

11000

13000 15000 Engine power kW

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

Bridge stand 150 100

200

50

50

Engine control room stand

50

250

0

300

100

100

150 100

200

50

50

50

250

0

300

100

100

Alphatronic control unit Engine interface unit

Engine speed command Pitch command

Fuel index

Pitch indication Propeller speed

Main engine

• Additional control panels for: Bridge Bridge wing indoor Bridge wing outdoor Engine control room • Manoeuvre responsibility panels • Shaft alternator panels • Interface units for: Joystick control systems Power management systems • Additional instrument panels

Govenor

Remote Control System Structure DIagram

Alphatronic 2000 State-of-the-art The newly developed Alphatronic 2000 control, monitoring and safety systems set new standards in engine load control functions, safe operation, system redundancy, logical operator panels and simple serial interfaced installation.

MAN B&W CP Propellers and Control Systems for MAN B&W Two-stroke Engines L60MC, S60MC and S60MC-C 7680-15360 kW (10400-20800 BHP)

. m a i D

Q

R

S

W

L60MC standard programme ENGINE Type 4L60MC 5L60MC 6L50MC 7L60MC 8L60MC

PROPELLER Speed

Hub

OD-Box

Diam.

Q

R

W min

Mass

kW

Output * BHP

rpm

Type

Type

mm

mm

mm

mm

ton**

7680 9600 11520 13440 15360

10400 13000 15600 18200 20800

123 123 123 123 123



5200 5500 5750 5950 6150

1030 1100 1175 1175 1278

1131 1170 1242 1257 1338

2651 2676 2676 2919 2976

29,5 34,5 39,5 44,2 53,2

The propeller diameter is optimised at 90% mcr, 123 rpm and 17.4 kn The strenght calculation is made at 100% mcr, 123 rpm and 18.0 kn

S60MC standard programme ENGINE Type 4S60MC 5S50MC 6S60MC 7S60MC

PROPELLER Output *

Speed

Hub

OD-Box

Diam.

Q

R

W min

Mass

mm

mm

mm

mm

ton**

5650 6000 6300 6550

1100 1175 1278 1278

1170 1242 1333 1338

kW

BHP

rpm

Type

Type

8160 10200 12240 14280

11120 13900 16680 19460

105 105 105 105

VBS1460 VBS1560 VBS1680 VBS1680

ODS450 ODS450 ODS500 ODS560

2676 2676 2919 2976

34,1 39,2 47,9 54


S60MC-C standard programme ENGINE Type 4S60MC-C 5S60MC-C 6S60MC-C

PROPELLER Speed

Hub

OD-Box

Diam.

Q

R

W min

Mass

kW

Output* BHP

rpm

Type

Type

mm

mm

mm

mm

ton**

9020 11275 13530

12280 15350 18420

105 105 105

VBS1460 VBS1560 VBS1680

ODS450 ODS500 ODS560

5850 6150 6450

1100 1175 1278

1170 1257 1338

* Engine output refers to load point L1 ** The masses are stated for 3,000 mm stern tube and 6,000 mm propeller shaft

2676 2919 2976

35,2 43,5 53,3

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


Alpha Clutcher - for Auxiliary Propulsion Systems The Alpha Clutcher is a new shaftline de-clutching device for auxiliary propulsion systems which meets the class notations for redundant propulsion. It facilitates reliable and simple “take home” and “take away” functions in two-stroke engine plants.

D

L

Alpha Clutcher range for two-stroke MC engines

Main data TYPE

CB 1

CB 2

CB 3

CB 4

Lenght [L]

1445

1635

1830

2160

Diameter [D]

1185

1340

1500

1770

Weight* [ton]

14

20

29

44

Dimensions mm

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 S50MC-C

4-5

6-8

4

5-7

8

4-5

6-8

L60MC S60MC

4

5-7

S60MC-C

4

5-6

* Approx weight incl intermediate shaft.

MAN B&W CP Propellers and Control Systems for MAN B&W Four-stroke Engines L32/40 and V32/40 2880-7680 kW (3930-10480 BHP)

. m a i D

Q

R

S

W

L32/40 standard programme ENGINE Type 6L32/40

7L32/40

OUTPUT, mcr kW 2880

3360

SPEED

HUB

OD-BOX

PROPELLER

Q

R

Wmin

MASS

BHP

rpm

Type

Type

Diam, mm

mm

mm

mm

ton**

3930

200 160 120

VBS860 VBS860 VBS980


3250 3600 4150

655 655 746

735 735 805

1970 2000 2040

8,8 9,9 12,4

4585

200 160 120



3350 3750 4300

655 746 825

735 785 875

2000 2000 2040

9,7 11,8 14,5



3500 3900 4450

655 746 825

735 805 880

2000 2040 2140

10,4 12,6 16,4



3600 4000 4600

746 746 825

785 805 880

2000 2040 2140

12,2 13,2 17,2

8L32/40

3840

5240

200 160 120

9L32/40

4320

5895

200 160 120

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 GL No Ice with high skew **The masses are stated for 3,000 mm stern tube and 6,000 mm propeller shaft

V32/40 standard programme ENGINE

SPEED

HUB

OD-BOX

PROPELLER

Q

R

Wmin

MASS

Type

kW

OUTPUT, mcr BHP

rpm

Type

Type

Diam, mm

mm

mm

mm

ton**

12V32/40

5760

7860

200 160 120

VBS1080 VBS1080 VBS1280


3850 4300 4950

821 821 957

880 945 1075

2040 2170 2511

15,3 17,0 23,5

VBS1080 VBS1180 VBS1280


4000 4500 5150

821 885 957

945 996 1075

2170 2170 2511

16,6 20,2 25,7

VBS1180 VBS1180 VBS1380


4150 4650 5350

885 885 1030

996 996 1131

2170 2265 2651

19,0 22,2 29,2

14V32/40

6720

9170

200 160 120

16V32/40

7680

10480

200 160 120

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 GL No Ice with high skew **The masses are stated for 3,000 mm stern tube and 6,000 mm propeller shaft

MAN B&W CP Propellers and Control Systems for MAN B&W Four-stroke Engines L40/54, L48/60 and L58/64 4320-12510 kW (5880-17010 BHP)

. m a i D

Q

R

S

W

L40/54 standard programme ENGINE

SPEED

HUB

OD-BOX

PROPELLER

Q

R

Wmin

MASS

Type

kW

BHP

rpm

Type

Type

Diam, mm

mm

mm

mm

ton**

6L40/54

4320

5880

190 150 110



3650 4100 4800

746 825 825

805 880 880

2040 2140 2140

11,9 15,6 19

6860

190 150 110



3800 4250 4950

746 825 975

805 880 1115

2040 2140 2200

12,9 16,2 23

VBS1080 VBS1180 VBS1280


3950 4400 5100

825 900 975

880 940 1115

2140 2160 2200

15,9 18,9 25,2

VBS1080 VBS1180 VBS1280


4050 4550 5250

825 900 975

880 1020 1115

2140 2160 2350

16,5 20,3 27,4

HUB

OD-BOX

PROPELLER

Q

R

Wmin

MASS

7L40/54

OUTPUT, mcr

5040

8L40/54

5760

7840

190 150 110

9L40/54

6480

8820

190 150 110


L48/60 standard programme ENGINE Type 6L48/60

7L48/60

OUTPUT, mcr kW 6300

7350

SPEED

BHP

rpm

Type

Type

Diam, mm

mm

mm

mm

ton**

8580

180 140 100

VBS1080 VBS1180 VBS1380


4100 4600 5450

825 900 1050

880 1020 1175

2140 2160 2270

16,6 20,4 29,9

10010

180 140 100

VBS1180 VBS1280 VBS1380


4250 4800 5650

900 975 1050

940 1115 1175

2140 2200 2350

20,3 25,4 32,5

VBS1280 VBS1280 VBS1460


4400 4950 5800

975 975 1110

1115 1175 1220

2200 2200 2350

24,1 27,6 35,2

VBS1280 VBS1380 VBS1560


4550 5100 6000

975 1050 1190

1115 1175 1350

2200 2270 2550

25,7 30,8 40,6

8L48/60

8400

11440

180 140 100

9L48/60

9450

12870

180 140 100


L58/64 standard programme ENGINE

SPEED

HUB

OD-BOX

PROPELLER

Q

R

Wmin

MASS

Type

kW

BHP

rpm

Type

Type

Diam, mm

mm

mm

mm

ton**

6L58/64

8340

11340

170 130 90

VBS1280 VBS1280 VBS1560


4500 5100 6100

975 975 1190

1115 1115 1305

2200 2350 2550

23,9 28,2 40,3

13230

170 130 90

VBS1280 VBS1380 VBS1560


4650 5300 6300

975 1050 1190

1115 1175 1305

2200 2350 2570

27,1 32,2 45,4

VBS1380 VBS1460 VBS1680


4800 5500 6500

1050 1110 1280

1175 1220 1380

2270 2350 2570

30,8 35,9 52,2

VBS1380 VBS1560 VBS1680


4950 5650 6700

1050 1190 1280

1175 1305 1380

2350 2550 2570

31,9 41,2 55,4

7L58/64

OUTPUT, mcr

9730

8L58/64

11120

15120

170 130 90

9L58/64

12510

17010

170 130 90

The propeller diameter is optimised at 90% mcr, 100% rpm and 18.3 kn The strength calculation is made at 100% mcr, 100% rpm and 19.0 kn The propeller is calculated according to GL, No Ice with high skew **The masses are stated for 3,000 mm stern tube and 6,000 mm propeller shaft

180126797-Mesin-Man-B-W-pdf.pdf

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