• Подбор оборудования

    Монтажные работы

    Пуско-наладочные работы

    Ремонтные работы

    Эксплуатационные СЗЧ

  • Системы безопасности и жизнеобеспечения

    Оборудование арктического исполнения

    Оборудование во взрывобезопасном исполнении

    Дистанционное управление арматурой





  • Системы вентиляции и кондиционирования

    Дизайн интерьеров и мебели

    Стеновые панели, ковровые покрытия

  • Траловые комплексы

    Трапы, канаты, якоря

    Холодильная техника

    Рыбопоисковое оборудование

    Рыбообрабатывающее оборудование

  • Буровое оборудование

    Генераторные станции

    Системы позиционирования

    Оборудование жилых модулей





  • Логистика

    Таможня и экспедирование

    Консолидация и складирование

    Тракинг-система контроля поставок

  • Подбор верфи для ремонта

    Проектные работы

    Монтажные работы

    Пуско-наладочные работы

    Ремонтные работы

    Сюрвей судов

W 6L34DF

L34DF_разрез

Описание двигателя Wärtsilä 6L34DF

Wärtsilä 6L34DF - шестицилиндровый, рядный, четырехтактный, нереверсивный, с турбонаддувом, промежуточным охлаждением, двойной подачей топлива в двигатель, с прямым впрыском жидкого топлива и непрямым впрыском газообразного топлива. Двигатель может работать в газовом режиме или в режиме дизель.

Технические характеристики

 

Wärtsilä 6L34DF  IMO Tier 2

AE/DE

AE/DE

ME

Gas

Diesel

Gas

Diesel

Gas

Diesel

Cylinder output

kW

435

450

450

Engine speed

rpm

720

750

750

Engine output

kW

2610

2700

2700

Mean effective pressure

MPa

2.0

1.98

1.98

Combustion air system (Note 1)

Flow at 100% load

kg/s

4.3

5.1

4.3

5.4

4.3

5.7

Temperature at turbocharger intake, max.

°C

45

45

45

Temperature after air cooler (TE 601), load > 70%

°C

45

-

45

-

45

-

Temperature after air cooler (TE 601), load 30...70%

°C

55

-

55

-

55

-

Temperature after air cooler (TE 601)

°C

-

50

-

50

-

50

Exhaust gas system (Note 2)

Flow at 100% load

kg/s

4.5

5.2

4.5

5.6

4.5

5.9

Flow at 75% load

kg/s

3.6

4.0

3.6

4.3

3.5

4.1

Flow at 50% load

kg/s

2.9

2.6

2.9

2.8

3.0

3.1

Temperature after turbocharger at 100% load (TE 517)

°C

390

350

390

340

390

315

Temperature after turbocharger at 75% load (TE 517)

°C

425

375

425

355

410

345

Temperature after turbocharger at 50% load (TE 517)

°C

440

420

440

410

355

350

Backpressure, max.

kPa

4

4

4

Calculated exhaust diameter for 35 m/s

mm

550

578

550

591

550

594

Heat balance at 100% load (Note 3)

Jacket water, HT-circuit

kW

470

480

490

510

490

530

Charge air, HT-circuit

kW

330

570

340

640

340

690

Charge air, LT-circuit

kW

240

250

250

270

250

310

Lubricating oil, LT-circuit

kW

280

290

290

310

290

310

Radiation

kW

100

100

100

110

100

110

Fuel consumption (Note 4)

Total energy consumption at 100% load

kJ/kWh

7710

-

7710

-

7710

-

Total energy consumption at 75% load

kJ/kWh

8190

-

8190

-

8130

-

Total energy consumption at 50% load

kJ/kWh

8890

-

8890

-

8350

-

Fuel gas consumption at 100% load

kJ/kWh

7629

-

7629

-

7629

-

Fuel gas consumption at 75% load

kJ/kWh

8067

-

8067

-

8010

-

Fuel gas consumption at 50% load

kJ/kWh

8677

-

8677

-

8153

-

Fuel oil consumption at 100% load

g/kWh

2.0

189

2.0

191

2.0

193

Fuel oil consumption at 75% load

g/kWh

2.8

193

2.8

195

2.7

187

Fuel oil consumption 50% load

g/kWh

4.9

200

4.9

202

4.5

192

Gas pressure at engine inlet, min (PT901)

kPa (a)

452

-

452

-

452

-

Gas pressure to Gas Valve Unit, min

kPa (a)

572

-

572

-

572

-

Gas temperature before Gas Valve Unit

°C

0...60

-

0...60

-

0...60

-

Fuel oil system

Pressure before injection pumps (PT 101)

kPa

700±50

700±50

700±50

Fuel oil flow to engine, approx

m3/h

2.8

2.9

2.9

HFO viscosity before the engine

cSt

-

16...24

-

16...24

-

16...24

Max. HFO temperature before engine (TE 101)

°C

-

140

-

140

-

140

MDF viscosity, min.

cSt

2.0

2.0

2.0

Max. MDF temperature before engine (TE 101)

°C

45

45

45

Leak fuel quantity (MDF), clean fuel at 100% load

kg/h

5.2

10.3

5.4

10.8

5.5

10.9

Pilot fuel (MDF) viscosity before the engine

cSt

2...11

2...11

2...11

Pilot fuel pressure at engine inlet (PT 112)

kPa (a)

550...750

550...750

550...750

Pilot fuel pressure drop after engine, max

kPa

150

150

150

Pilot fuel return flow at 100% load

kg/h

590

590

590

Lubricating oil system

Pressure before bearings, nom. (PT 201)

kPa

500

500

500

Suction ability, including pipe loss, max.

kPa

30

30

30

Priming pressure, nom. (PT 201)

kPa

50

50

50

Suction ability priming pump, including pipe loss, max.

kPa

30

30

30

Temperature before bearings, nom. (TE 201)

°C

63

63

63

Temperature after engine, approx.

°C

78

78

78

Pump capacity (main), engine driven

m3/h

78

81

81

Pump capacity (main), electrically driven

m3/h

67

70

70

Priming pump capacity (50/60Hz)

m3/h

15.0 / 18.0

15.0 / 18.0

15.0 / 18.0

Oil volume in separate system oil tank

m3

3

3

3

Oil consumption at 100% load, approx.

g/kWh

0.4

0.4

0.4

Crankcase ventilation flow rate at full load

l/min

840

840

840

Crankcase ventilation backpressure, max.

kPa

0.3

0.3

0.3

Oil volume in turning device

l

8.5...9.5

8.5...9.5

8.5...9.5

Oil volume in speed governor

l

1.4...2.2

1.4...2.2

1.4...2.2

HT cooling water system

Pressure at engine, after pump, nom. (PT 401)

kPa

250 + static

250 + static

250 + static

Pressure at engine, after pump, max. (PT 401)

kPa

530

530

530

Temperature before cylinders, approx. (TE 401)

°C

85

85

85

Temperature after engine, nom.

°C

96

96

96

Capacity of engine driven pump, nom.

m3/h

60

60

60

Pressure drop over engine, total

kPa

100

100

100

Pressure drop in external system, max.

kPa

150 (1.5)

150 (1.5)

150 (1.5)

Pressure from expansion tank

kPa

70...150

70...150

70...150

Water volume in engine

m3

0.41

0.41

0.41

Delivery head of stand-by pump

kPa

250

250

250

LT cooling water system

Pressure at engine, after pump, nom. (PT 471)

kPa

250+ static

250+ static

250+ static

Pressure at engine, after pump, max. (PT 471)

kPa

530

530

530

Temperature before engine, max. (TE 471)

°C

38

38

38

Temperature before engine, min. (TE 471)

°C

25

25

25

Capacity of engine driven pump, nom.

m3/h

60

60

60

Pressure drop over charge air cooler

kPa

35

35

35

Pressure drop in external system, max.

kPa

200 (2.0)

200 (2.0)

200 (2.0)

Pressure from expansion tank

kPa

70...150

70...150

70...150

Delivery head of stand-by pump

kPa

250

250

250

Starting air system

Pressure, nom.

kPa

3000

3000

3000

Pressure, max.

kPa

3000

3000

3000

Low pressure limit in starting air receiver

kPa

1600

1600

1600

Starting air consumption, start (successful)

Nm3

4.7

4.7

4.7

Consumption per start (with slowturn)

Nm3

6.1

6.1

6.1

 

Wärtsilä 6L34DF  IMO Tier 2

AE/DE

AE/DE

ME

Gas

Diesel

Gas

Diesel

Gas

Diesel

Cylinder output

kW

480

500

500

Engine speed

rpm

720

750

750

Engine output

kW

2880

3000

3000

Mean effective pressure

MPa

2.2

2.2

2.2

Combustion air system (Note 1)

Flow at 100% load

kg/s

4.4

5.3

4.4

5.5

4.4

5.5

Temperature at turbocharger intake, max.

°C

45

45

45

Temperature after air cooler (TE 601), load > 70%

°C

45

-

45

-

45

-

Temperature after air cooler (TE 601), load 30...70%

°C

55

-

55

-

55

-

Temperature after air cooler (TE 601)

°C

-

50

-

50

-

50

Exhaust gas system (Note 2)

Flow at 100% load

kg/s

4.5

5.4

4.5

5.7

4.5

5.7

Flow at 75% load

kg/s

3.3

4.3

3.4

4.6

3.8

4.2

Flow at 50% load

kg/s

3.0

3.0

3.1

3.2

2.9

3.1

Temperature after turbocharger at 100% load (TE 517)

°C

380

340

380

335

380

335

Temperature after turbocharger at 75% load (TE 517)

°C

425

320

425

315

365

340

Temperature after turbocharger at 50% load (TE 517)

°C

386

340

386

340

353

343

Backpressure, max.

kPa

4

4

4

Calculated exhaust diameter for 35 m/s

mm

546

583

551

596

551

596

Heat balance at 100% load (Note 3)

Jacket water, HT-circuit

kW

470

504

490

528

490

528

Charge air, HT-circuit

kW

497

831

542

870

542

870

Charge air, LT-circuit

kW

223

239

243

290

243

290

Lubricating oil, LT-circuit

kW

288

307

300

321

300

321

Radiation

kW

98

107

102

112

102

112

Fuel consumption (Note 4)

Total energy consumption at 100% load

kJ/kWh

7400

-

7400

-

7400

-

Total energy consumption at 75% load

kJ/kWh

7610

-

7610

-

7610

-

Total energy consumption at 50% load

kJ/kWh

8450

-

8450

-

7730

-

Fuel gas consumption at 100% load

kJ/kWh

7324

-

7324

-

7324

-

Fuel gas consumption at 75% load

kJ/kWh

7496

-

7496

-

7505

-

Fuel gas consumption at 50% load

kJ/kWh

8286

-

8286

-

7600

-

Fuel oil consumption at 100% load

g/kWh

1.9

186

1.9

187

1.9

187

Fuel oil consumption at 75% load

g/kWh

2.6

183

2.6

184

2.4

180

Fuel oil consumption 50% load

g/kWh

3.8

190

3.8

191

3.0

182

Fuel gas system (Note 5)

Gas pressure at engine inlet, min (PT901)

kPa (a)

452

-

452

-

452

-

Gas pressure to Gas Valve Unit, min

kPa (a)

572

-

572

-

572

-

Gas temperature before Gas Valve Unit

°C

0...60

-

0...60

-

0...60

-

Fuel oil system

Pressure before injection pumps (PT 101)

kPa

700±50

700±50

700±50

Fuel oil flow to engine, approx

m3/h

3.0

3.2

3.2

HFO viscosity before the engine

cSt

-

16...24

-

16...24

-

16...24

Max. HFO temperature before engine (TE 101)

°C

-

140

-

140

-

140

MDF viscosity, min.

cSt

2.0

2.0

2.0

Max. MDF temperature before engine (TE 101)

°C

45

45

45

Leak fuel quantity (MDF), clean fuel at 100% load

kg/h

5.6

11.2

5.9

11.8

5.9

11.8

Pilot fuel (MDF) viscosity before the engine

cSt

2...11

2...11

2...11

Pilot fuel pressure at engine inlet (PT 112)

kPa (a)

550...750

550...750

550...750

Pilot fuel pressure drop after engine, max

kPa

150

150

150

Pilot fuel return flow at 100% load

kg/h

590

590

590

Lubricating oil system

Pressure before bearings, nom. (PT 201)

kPa

500

500

500

Suction ability, including pipe loss, max.

kPa

30

30

30

Priming pressure, nom. (PT 201)

kPa

50

50

50

Suction ability priming pump, including pipe loss, max.

kPa

30

30

30

Temperature before bearings, nom. (TE 201)

°C

63

63

63

Temperature after engine, approx.

°C

78

78

78

Pump capacity (main), engine driven

m3/h

78

81

81

Pump capacity (main), electrically driven

m3/h

67

70

70

Priming pump capacity (50/60Hz)

m3/h

15.0 / 18.0

15.0 / 18.0

15.0 / 18.0

Oil volume in separate system oil tank

m3

3

3

3

Oil consumption at 100% load, approx.

g/kWh

0.4

0.4

0.4

Crankcase ventilation flow rate at full load

l/min

840

840

840

Crankcase ventilation backpressure, max.

kPa

0.3

0.3

0.3

Oil volume in turning device

l

8.5...9.5

8.5...9.5

8.5...9.5

Oil volume in speed governor

l

1.4...2.2

1.4...2.2

1.4...2.2

HT cooling water system

Pressure at engine, after pump, nom. (PT 401)

kPa

250 + static

250 + static

250 + static

Pressure at engine, after pump, max. (PT 401)

kPa

530

530

530

Temperature before cylinders, approx. (TE 401)

°C

85

85

85

Temperature after engine, nom.

°C

96

96

96

Capacity of engine driven pump, nom.

m3/h

60

60

60

Pressure drop over engine, total

kPa

100

100

100

Pressure drop in external system, max.

kPa

150 (1.5)

150 (1.5)

150 (1.5)

Pressure from expansion tank

kPa

70...150

70...150

70...150

Water volume in engine

m3

0.41

0.41

0.41

Delivery head of stand-by pump

kPa

250

250

250

LT cooling water system

Pressure at engine, after pump, nom. (PT 471)

kPa

250+ static

250+ static

250+ static

Pressure at engine, after pump, max. (PT 471)

kPa

530

530

530

Temperature before engine, max. (TE 471)

°C

38

38

38

Temperature before engine, min. (TE 471)

°C

25

25

25

Capacity of engine driven pump, nom.

m3/h

60

60

60

Pressure drop over charge air cooler

kPa

35

35

35

Pressure drop in external system, max.

kPa

200 (2.0)

200 (2.0)

200 (2.0)

Pressure from expansion tank

kPa

70...150

70...150

70...150

Delivery head of stand-by pump

kPa

250

250

250

Starting air system

Pressure, nom.

kPa

3000

3000

3000

Pressure, max.

kPa

3000

3000

3000

Low pressure limit in starting air receiver

kPa

1600

1600

1600

Starting air consumption, start (successful)

Nm3

4.7

4.7

4.7

Consumption per start (with slowturn)

Nm3

6.1

6.1

6.1

Notes:

Note 1 At Gas LHV 49620kJ/kg

Note 2 At ISO 3046-1 conditions (ambient air temperature 25°C, LT-water 25°C) and 100% load. Flow tolerance 5% and temperature tolerance 10°C in gas mode operation. Flow tolerance 8% and temperature tolerance 15°C in diesel mode operation.

Note 3 At 100% output and nominal speed. The figures are valid for ambient conditions according to ISO 3046/1, except for LT-water temperature, which is corresponding to charge air receiver temperature 45ºC in gas operation. With engine driven water and lubricating oil pumps. Tolerance for cooling water heat 10%, tolerance for radiation heat 30%. Fouling factors and a margin to be taken into account when dimensioning heat exchangers.

Note 4 At ambient conditions according to ISO 3046/1, fuel net calorific value 42700 kJ/kg, with engine driven pumps (two cooling water + one lubricating oil pumps). Tolerance 5%.

Note 5 Fuel gas pressure given at LHV ≥ 36MJ/m³N. Required fuel gas pressure depends on fuel gas LHV and need to be increased for lower LHV's. Pressure drop in external fuel gas system to be considered. See chapter Fuel system for further information.

ME = Engine driving propeller, variable speed

AE = Auxiliary engine driving generator

DE = Diesel-Electric engine driving generator

Subject to revision without notice.


Ко всему вышеуказанному оборудованию мы поставляем СЗЧ согласно каталожным номерам производителя.

Для получения коммерческого предложения на поставку двигателя или запчастей к нему обращайтесь к нашим специалистам по указанным ниже контактным данным, либо воспользуйтесь формой подачи заявки прямо с сайта.

Оставить отзыв
Закрыть

Оставить отзыв

Защита от автоматического заполнения
 
Введите символы с картинки*


Оставить заявку
Закрыть

Оставить заявку

Защита от автоматического заполнения
 
Введите символы с картинки*