Gas Generator Set
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Gas Generator Sets
EPIOR gas-fired gensets are characterized by high efficiency, not only low fuel consumption, low emissions and low gas consumption, but also high power generation efficiency, easy maintenance and flexible operation. In addition, the gensets have design advantages such as high-precision technology, precise mixing, thin combustion, automatic regulation, data monitoring, etc., which make them very competitive in terms of power density, reliability, durability as well as operation and maintenance costs.
Technical Parameters
Natural gas applications
Biogas applications
Highly concentrated gas applications
Low concentration gas applications
Wellhead gas applications
XE512-N
| Model | unit (of measure) | XE512-N | ||||||||||||
| flight crew (on a plane) | ||||||||||||||
| Length | mm | 4545 | ||||||||||||
| Width | mm | 1795 | ||||||||||||
| Height | mm | 2465 | ||||||||||||
| Net weight of the unit | kg | 10650 | ||||||||||||
| energy balance | ||||||||||||||
| Electrical power | kW | 1056 | ||||||||||||
| Jacket water heat | kW | 423 | ||||||||||||
| Inter-cooling water heat | kW | 124 | ||||||||||||
| Outlet temperature of jacket water | ℃ | 84/92 | ||||||||||||
| Heat (exhaust cooled to 120°C) | kW | 574 | ||||||||||||
| exhaust temperature | ℃ | ~500 | ||||||||||||
| efficiency | ||||||||||||||
| electrical efficiency | % | 41 | ||||||||||||
| Heat efficiency | % | 43.5 | ||||||||||||
| total efficiency | % | 84.5 | ||||||||||||
| Engine | ||||||||||||||
| Engine Model | X512-N | |||||||||||||
| power (output) | kW | 1200 | ||||||||||||
| number of revolutions per minute | rpm | 1500 | ||||||||||||
| structure | V90° | |||||||||||||
| Number of cylinders | 12 | |||||||||||||
| bore | mm | 171 | ||||||||||||
| course (of history) | mm | 210 | ||||||||||||
| emission (e.g. of CO2, etc.) | L | 57.87 | ||||||||||||
| compression ratio | 13.5 | |||||||||||||
| Average effective pressure | MPa | 1.55 | ||||||||||||
| Gas consumption rate | MJ/kW -h | 8.78 | ||||||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | ||||||||||||
| alternators | ||||||||||||||
| makers | EPIOR | |||||||||||||
| Generator Model | XFS 1500 | |||||||||||||
| power factor | cos φ | 0.8 | ||||||||||||
| efficiency | % | 94 | ||||||||||||
| capacity | kVA | 1500 | ||||||||||||
| extremity | 4 | |||||||||||||
| frequency | Hz | 50 | ||||||||||||
| protection class | IP23 | |||||||||||||
| Insulation class | H | |||||||||||||
XE516-N
| Model | unit (of measure) | XE516-N | ||||||||||||
| flight crew (on a plane) | ||||||||||||||
| 长 | mm | 5360 | ||||||||||||
| 宽 | mm | 1795 | ||||||||||||
| 高 | mm | 2465 | ||||||||||||
| Net weight of the unit | kg | 14700 | ||||||||||||
| energy balance | ||||||||||||||
| electric power (measured in watts) | kW | 1408 | ||||||||||||
| Cylinder liner water heat | kW | 571 | ||||||||||||
| Medium cold water heat | kW | 157 | ||||||||||||
| Cylinder sleeve water outlet temperature | ℃ | 84/94 | ||||||||||||
| Exhaust cooling to 120°C heat | kW | 756 | ||||||||||||
| exhaust temperature | ℃ | ~500 | ||||||||||||
| efficiency | ||||||||||||||
| electrical efficiency | % | 41.5 | ||||||||||||
| thermal efficiency | % | 43.7 | ||||||||||||
| total efficiency | % | 85.2 | ||||||||||||
| motor | ||||||||||||||
| Engine Model | X516-N | |||||||||||||
| power (output) | kW | 1600 | ||||||||||||
| number of revolutions per minute | rpm | 1500 | ||||||||||||
| structure | V90° | |||||||||||||
| Number of cylinders | 16 | |||||||||||||
| bore | mm | 171 | ||||||||||||
| course (of history) | mm | 210 | ||||||||||||
| emission (e.g. of CO2, etc.) | L | 77.17 | ||||||||||||
| compression ratio | 13.5 | |||||||||||||
| Average effective pressure | MPa | 1.55 | ||||||||||||
| Gas consumption rate | MJ/kW -h | 8.67 | ||||||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | ||||||||||||
| alternators | ||||||||||||||
| makers | EPIOR | |||||||||||||
| Generator Model | XFS 2000 | |||||||||||||
| power factor | cos φ | 0.8 | ||||||||||||
| efficiency | % | 94 | ||||||||||||
| capacity | kVA | 2000 | ||||||||||||
| extremity | 4 | |||||||||||||
| frequency | Hz | 50 | ||||||||||||
| protection class | IP23 | |||||||||||||
| Insulation class | H | |||||||||||||
XE520-N
| Model | unit (of measure) | XE520-N | |||||||||||
| flight crew (on a plane) | |||||||||||||
| 长 | mm | 6278 | |||||||||||
| 宽 | mm | 1795 | |||||||||||
| 高 | mm | 2465 | |||||||||||
| Net weight of the unit | kg | 18500 | |||||||||||
| energy balance | |||||||||||||
| electric power (measured in watts) | kW | 1760 | |||||||||||
| Cylinder liner water heat | kW | 696 | |||||||||||
| Medium cold water heat | kW | 205 | |||||||||||
| Cylinder sleeve water outlet temperature | ℃ | 84/94 | |||||||||||
| Exhaust cooling to 120°C heat | kW | 934 | |||||||||||
| exhaust temperature | ℃ | ~500 | |||||||||||
| efficiency | |||||||||||||
| electrical efficiency | % | 42 | |||||||||||
| thermal efficiency | % | 43.8 | |||||||||||
| total efficiency | % | 85.8 | |||||||||||
| motor | |||||||||||||
| Engine Model | X520-N | ||||||||||||
| power (output) | kW | 2000 | |||||||||||
| number of revolutions per minute | rpm | 1500 | |||||||||||
| structure | V90° | ||||||||||||
| Number of cylinders | 20 | ||||||||||||
| bore | mm | 171 | |||||||||||
| course (of history) | mm | 210 | |||||||||||
| emission (e.g. of CO2, etc.) | L | 96.46 | |||||||||||
| compression ratio | 13.5 | ||||||||||||
| Average effective pressure | MPa | 1.55 | |||||||||||
| Gas consumption rate | MJ/kW -h | 8.57 | |||||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | |||||||||||
| alternators | |||||||||||||
| makers | EPIOR | ||||||||||||
| Generator Model | XFS 2500 | ||||||||||||
| power factor | cos φ | 0.8 | |||||||||||
| efficiency | % | 94 | |||||||||||
| capacity | kVA | 2500 | |||||||||||
| extremity | 4 | ||||||||||||
| frequency | Hz | 50 | |||||||||||
| protection class | IP23 | ||||||||||||
| Insulation class | H | ||||||||||||
XE512-B
| Model | unit (of measure) | XE512-B | |||||
| flight crew (on a plane) | |||||||
| 长 | mm | 4545 | |||||
| 宽 | mm | 1795 | |||||
| 高 | mm | 2465 | |||||
| Net weight of the unit | kg | 10650 | |||||
| energy balance | |||||||
| electric power (measured in watts) | kW | 1000 | |||||
| Cylinder liner water heat | kW | 489 | |||||
| Medium cold water heat | kW | 126 | |||||
| Cylinder sleeve water outlet temperature | ℃ | 84/92 | |||||
| Exhaust cooling to 120°C heat | kW | 544 | |||||
| exhaust temperature | ℃ | ≤550 | |||||
| efficiency | |||||||
| electrical efficiency | % | 39 | |||||
| thermal efficiency | % | 45.2 | |||||
| total efficiency | % | 84.2 | |||||
| motor | |||||||
| Engine Model | X512-B | ||||||
| power (output) | kW | 1064 | |||||
| number of revolutions per minute | rpm | 1500 | |||||
| structure | V90° | ||||||
| Number of cylinders | 12 | ||||||
| bore | mm | 171 | |||||
| course (of history) | mm | 210 | |||||
| emission (e.g. of CO2, etc.) | L | 57.87 | |||||
| compression ratio | 13.5 | ||||||
| Average effective pressure | MPa | 1.47 | |||||
| Gas consumption rate | MJ/kW -h | 9.23 | |||||
| Lubricant consumption rate | g/kW -h | 0.35 | |||||
| alternators | |||||||
| makers | EPIOR | ||||||
| Generator Model | XFS 1320 | ||||||
| power factor | cos φ | 0.8 | |||||
| efficiency | % | 94 | |||||
| capacity | kVA | 1320 | |||||
| extremity | 4 | ||||||
| frequency | Hz | 50 | |||||
| protection class | P23 | ||||||
| Insulation class | H | ||||||
XE516-B
| Model | unit (of measure) | XE516-B | ||||||||
| flight crew (on a plane) | ||||||||||
| 长 | mm | 5360 | ||||||||
| 宽 | mm | 1795 | ||||||||
| 高 | mm | 2465 | ||||||||
| Net weight of the unit | kg | 14700 | ||||||||
| energy balance | ||||||||||
| electric power (measured in watts) | kW | 1350 | ||||||||
| Cylinder liner water heat | kW | 672 | ||||||||
| Medium cold water heat | kW | 161 | ||||||||
| Cylinder sleeve water outlet temperature | ℃ | 84/94 | ||||||||
| Exhaust cooling to 120°C heat | kW | 724 | ||||||||
| exhaust temperature | ℃ | ≤550 | ||||||||
| efficiency | ||||||||||
| electrical efficiency | % | 39.5 | ||||||||
| thermal efficiency | % | 45.6 | ||||||||
| total efficiency | % | 85.1 | ||||||||
| motor | ||||||||||
| Engine Model | X516-B | |||||||||
| power (output) | kW | 1436 | ||||||||
| number of revolutions per minute | rpm | 1500 | ||||||||
| structure | V90° | |||||||||
| Number of cylinders | 16 | |||||||||
| bore | mm | 171 | ||||||||
| course (of history) | mm | 210 | ||||||||
| emission (e.g. of CO2, etc.) | L | 77.17 | ||||||||
| compression ratio | 13.5 | |||||||||
| Average effective pressure | MPa | 1.49 | ||||||||
| Gas consumption rate | MJ/kW -h | 9.11 | ||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | ||||||||
| alternators | ||||||||||
| makers | EPIOR | |||||||||
| Generator Model | XFS 1800 | |||||||||
| power factor | cos φ | 0.8 | ||||||||
| efficiency | % | 94 | ||||||||
| capacity | kVA | 1800 | ||||||||
| extremity | 4 | |||||||||
| frequency | Hz | 50 | ||||||||
| protection class | IP23 | |||||||||
| Insulation class | H | |||||||||
XE520-B
| Model | unit (of measure) | XE520-B | ||||
| flight crew (on a plane) | ||||||
| 长 | mm | 6278 | ||||
| 宽 | mm | 1795 | ||||
| 高 | mm | 2465 | ||||
| Net weight of the unit | kg | 18500 | ||||
| energy balance | ||||||
| electric power (measured in watts) | kW | 1650 | ||||
| Cylinder liner water heat | kW | 789 | ||||
| Medium cold water heat | kW | 224 | ||||
| Cylinder sleeve water outlet temperature | ℃ | 84/94 | ||||
| Exhaust cooling to 120°C heat | kW | 874 | ||||
| exhaust temperature | ℃ | ≤550 | ||||
| efficiency | ||||||
| electrical efficiency | % | 40 | ||||
| thermal efficiency | % | 45.7 | ||||
| total efficiency | % | 85.7 | ||||
| motor | ||||||
| Engine Model | X520-B | |||||
| power (output) | kW | 1755 | ||||
| number of revolutions per minute | rpm | 1500 | ||||
| structure | V90° | |||||
| Number of cylinders | 20 | |||||
| bore | mm | 171 | ||||
| course (of history) | mm | 210 | ||||
| emission (e.g. of CO2, etc.) | L | 96.46 | ||||
| compression ratio | 13.5 | |||||
| Average effective pressure | MPa | 1.46 | ||||
| Gas consumption rate | MJ/kW -h | 9 | ||||
| Lubricant consumption rate | g/kW -h | 0.35 | ||||
| alternators | ||||||
| makers | EPIOR | |||||
| Generator Model | XFS 2250 | |||||
| power factor | cos φ | 0.8 | ||||
| efficiency | % | 94 | ||||
| capacity | kVA | 2250 | ||||
| extremity | 4 | |||||
| frequency | Hz | 50 | ||||
| protection class | IP23 | |||||
| Insulation class | H | |||||
XE512-M
| Model | unit (of measure) | XE512-M | ||||||||||
| flight crew (on a plane) | ||||||||||||
| 长 | mm | 4545 | ||||||||||
| 宽 | mm | 1795 | ||||||||||
| 高 | mm | 2465 | ||||||||||
| Net weight of the unit | kg | 10650 | ||||||||||
| energy balance | ||||||||||||
| electric power (measured in watts) | kW | 1000 | ||||||||||
| Cylinder liner water heat | kW | 441 | ||||||||||
| Medium cold water heat | kW | 114 | ||||||||||
| Cylinder sleeve water outlet temperature | ℃ | 84/92 | ||||||||||
| Exhaust cooling to 120°C heat | kW | 579 | ||||||||||
| exhaust temperature | ℃ | ≤550 | ||||||||||
| efficiency | ||||||||||||
| electrical efficiency | % | 39 | ||||||||||
| thermal efficiency | % | 44.2 | ||||||||||
| total efficiency | % | 83.2 | ||||||||||
| motor | ||||||||||||
| Engine Model | X512-M | |||||||||||
| power (output) | kW | 1064 | ||||||||||
| number of revolutions per minute | rpm | 1500 | ||||||||||
| structure | V90° | |||||||||||
| Number of cylinders | 12 | |||||||||||
| bore | mm | 171 | ||||||||||
| course (of history) | mm | 210 | ||||||||||
| emission (e.g. of CO2, etc.) | L | 57.87 | ||||||||||
| compression ratio | 13.5 | |||||||||||
| Average effective pressure | MPa | 1.47 | ||||||||||
| Gas consumption rate | MJ/kW -h | 9.23 | ||||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | ||||||||||
| alternators | ||||||||||||
| makers | EPIOR | |||||||||||
| Generator Model | XFS 1320 | |||||||||||
| power factor | cos φ | 0.8 | ||||||||||
| efficiency | % | 94 | ||||||||||
| capacity | kVA | 1320 | ||||||||||
| extremity | 4 | |||||||||||
| frequency | Hz | 50 | ||||||||||
| protection class | IP23 | |||||||||||
| Insulation class | H | |||||||||||
XE516-M
| Model | unit (of measure) | XE516-M | ||||||||||
| flight crew (on a plane) | ||||||||||||
| 长 | mm | 5360 | ||||||||||
| 宽 | mm | 1795 | ||||||||||
| 高 | mm | 2465 | ||||||||||
| Net weight of the unit | kg | 14700 | ||||||||||
| energy balance | ||||||||||||
| electric power (measured in watts) | kW | 1350 | ||||||||||
| Cylinder liner water heat | kW | 593 | ||||||||||
| Medium cold water heat | kW | 171 | ||||||||||
| Cylinder sleeve water outlet temperature | ℃ | 84/92 | ||||||||||
| Exhaust cooling to 120°C heat | kW | 772 | ||||||||||
| exhaust temperature | ℃ | ≤550 | ||||||||||
| efficiency | ||||||||||||
| electrical efficiency | % | 39.5 | ||||||||||
| thermal efficiency | % | 44.9 | ||||||||||
| total efficiency | % | 84.4 | ||||||||||
| motor | ||||||||||||
| Engine Model | X516-M | |||||||||||
| power (output) | kW | 1436 | ||||||||||
| number of revolutions per minute | rpm | 1500 | ||||||||||
| structure | V90° | |||||||||||
| Number of cylinders | 16 | |||||||||||
| bore | mm | 171 | ||||||||||
| course (of history) | mm | 210 | ||||||||||
| emission (e.g. of CO2, etc.) | L | 77.17 | ||||||||||
| compression ratio | 13.5 | |||||||||||
| Average effective pressure | MPa | 1.49 | ||||||||||
| Gas consumption rate | MJ/kW -h | 9.11 | ||||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | ||||||||||
| alternators | ||||||||||||
| makers | EPIOR | |||||||||||
| Generator Model | XFS 1800 | |||||||||||
| power factor | cos φ | 0.8 | ||||||||||
| efficiency | % | 94 | ||||||||||
| capacity | kVA | 1800 | ||||||||||
| extremity | 4 | |||||||||||
| frequency | Hz | 50 | ||||||||||
| protection class | IP23 | |||||||||||
| Insulation class | H | |||||||||||
XE520-M
| Model | unit (of measure) | XE520-M | |||||||||||
| flight crew (on a plane) | |||||||||||||
| 长 | mm | 6278 | |||||||||||
| 宽 | mm | 1795 | |||||||||||
| 高 | mm | 2465 | |||||||||||
| Net weight of the unit | kg | 18500 | |||||||||||
| energy balance | |||||||||||||
| electric power (measured in watts) | kW | 1650 | |||||||||||
| Cylinder liner water heat | kW | 717 | |||||||||||
| Medium cold water heat | kW | 216 | |||||||||||
| Cylinder sleeve water outlet temperature | ℃ | 84/94 | |||||||||||
| Exhaust cooling to 120°C heat | kW | 932 | |||||||||||
| exhaust temperature | ℃ | ≤550 | |||||||||||
| efficiency | |||||||||||||
| electrical efficiency | % | 40 | |||||||||||
| thermal efficiency | % | 45.2 | |||||||||||
| total efficiency | % | 85.2 | |||||||||||
| motor | |||||||||||||
| Engine Model | X520-M | ||||||||||||
| power (output) | kW | 1755 | |||||||||||
| number of revolutions per minute | rpm | 1500 | |||||||||||
| structure | V90° | ||||||||||||
| Number of cylinders | 20 | ||||||||||||
| bore | mm | 171 | |||||||||||
| course (of history) | mm | 210 | |||||||||||
| emission (e.g. of CO2, etc.) | L | 96.46 | |||||||||||
| compression ratio | 13.5 | ||||||||||||
| Average effective pressure | MPa | 1.46 | |||||||||||
| Gas consumption rate | MJ/kW -h | 9 | |||||||||||
| Lubricant consumption rate | g/kW -h | 0.35 | |||||||||||
| alternators | |||||||||||||
| makers | EPIOR | ||||||||||||
| Generator Model | XFS 2250 | ||||||||||||
| power factor | cos φ | 0.8 | |||||||||||
| efficiency | % | 94 | |||||||||||
| capacity | kVA | 2250 | |||||||||||
| extremity | 4 | ||||||||||||
| frequency | Hz | 50 | |||||||||||
| protection class | IP23 | ||||||||||||
| Insulation class | H | ||||||||||||
XE512-LM
| Model | unit (of measure) | XE512-LM | |||||
| flight crew (on a plane) | |||||||
| 长 | mm | 4545 | |||||
| 宽 | mm | 1795 | |||||
| 高 | mm | 2465 | |||||
| Net weight of the unit | kg | 10650 | |||||
| energy balance | |||||||
| electric power (measured in watts) | kW | 1000 | |||||
| Cylinder liner water heat | kW | 465 | |||||
| Medium cold water heat | kW | 110 | |||||
| Cylinder sleeve water outlet temperature | ℃ | 84/92 | |||||
| Exhaust cooling to 120°C heat | kW | 580 | |||||
| exhaust temperature | ℃ | ≤550 | |||||
| efficiency | |||||||
| electrical efficiency | % | 39 | |||||
| thermal efficiency | % | 43.9 | |||||
| total efficiency | % | 82.9 | |||||
| motor | |||||||
| Engine Model | X512-LM | ||||||
| power (output) | kW | 1064 | |||||
| number of revolutions per minute | rpm | 1500 | |||||
| structure | V90° | ||||||
| Number of cylinders | 12 | ||||||
| bore | mm | 171 | |||||
| course (of history) | mm | 210 | |||||
| emission (e.g. of CO2, etc.) | L | 57.87 | |||||
| compression ratio | 13.5 | ||||||
| Average effective pressure | MPa | 1.47 | |||||
| Gas consumption rate | MJ/kW -h | 9.23 | |||||
| Lubricant consumption rate | g/kW -h | 0.35 | |||||
| alternators | |||||||
| makers | EPIOR | ||||||
| Generator Model | XFS 1320 | ||||||
| power factor | cos φ | 0.8 | |||||
| efficiency | % | 94 | |||||
| capacity | kVA | 1320 | |||||
| extremity | 4 | ||||||
| frequency | Hz | 50 | |||||
| protection class | P23 | ||||||
| Insulation class | H | ||||||
XE516-LM
XE520-LM
XE512-F
XE516-F
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