Maximum Takeoff Thrust
147.28 kN
Overall Pressure Ratio
38.07
Fuel Flow Take Off
1.023 kg/s
NOx Unitaryto CAEP8
50.8 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
Yes |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
TALON X, Block-C |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
2 |
Bypass Ratio
11.58 |
Overall Pressure Ratio
38.07 |
Afterburner
No |
Pictures
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All data (75 fields)
- Name
- PW1130G-JM
- EASA ID
- 01P18PW155
- Aircraft Engine Manufacturer
- Pratt & Whitney
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- Yes
- Combustion Chamber
- TALON X, Block-C
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 11.58
- Overall Pressure Ratio
- 38.07
- Maximum Takeoff Thrust (kN)
- 147.28
- Hydrocarbon Take Off (g/kg fuel)
- 0.02
- Hydrocarbon Climb Out (g/kg fuel)
- 0.05
- Hydrocarbon Approach (g/kg fuel)
- 0.02
- Hydrocarbon Idle (g/kg fuel)
- 0.26
- Hydrocarbon Unitary Average (g/kN)
- 0.35
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.41
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 2.1
- Hydrocarbon LTO (g)
- 48
- Carbon Monoxide Take Off (g/kg fuel)
- 0.23
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.22
- Carbon Monoxide Approach (g/kg fuel)
- 3.44
- Carbon Monoxide Idle (g/kg fuel)
- 24.06
- Carbon Monoxide Unitary Average (g/kN)
- 24.88
- Carbon Monoxide Unitary Characteristic (g/kN)
- 26.91
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 22.8
- NOx Take Off (g/kg fuel)
- 25.46
- NOx Climb Out (g/kg fuel)
- 19.84
- NOx Approach (g/kg fuel)
- 9.4
- NOx Idle (g/kg fuel)
- 5.31
- NOx Unitary Average (g/kN)
- 31.3
- NOx Unitary Characteristic (g/kN)
- 33.62
- NOx Unitaryto Standard (% of limit)
- 29
- NOx Unitaryto CAEP2 (% of limit)
- 36.2
- NOx Unitaryto CAEP4 (% of limit)
- 40.4
- NOx Unitaryto CAEP6 (% of limit)
- 44.8
- NOx Unitaryto CAEP8 (% of limit)
- 50.8
- NOx LTO (g)
- 4736
- Smoke Take Off (SN)
- 15.2
- Smoke Climb Out (SN)
- 13.9
- Smoke Approach (SN)
- 0.5
- Smoke Idle (SN)
- 1
- Smoke Max (SN)
- 15.2
- Smoke Characteristic (SN)
- 16.7
- Smoke Characteristicto Regulatory (% of limit)
- 78.4
- Fuel Flow Take Off (kg/s)
- 1.023
- Fuel Flow Climbout (kg/s)
- 0.8385
- Fuel Flow Approach (kg/s)
- 0.2783
- Fuel Flow Idle (kg/s)
- 0.0988
- Fuel LTO (kg)
- 375
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 3971
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 6.9151
- nvPME Imass Climb Out (mg/kg)
- 70.7868
- nvPME Imass Idle (mg/kg)
- 7.0406
- nvPME Imass Max (mg/kg)
- 93.3457
- nvPME Imass Take Off (mg/kg)
- 93.3457
- nvPME Inum Approach (#/kg)
- 425475400000000
- nvPME Inum Climb Out (#/kg)
- 956537700000000
- nvPME Inum Idle (#/kg)
- 665217800000000
- nvPME Inum Max (#/kg)
- 963869000000000
- nvPME Inum Take Off (#/kg)
- 708296400000000
- nvPMLTO Mass (mg)
- 13398.92
- nvPMLTO Mass Per Thrust (mg/kN)
- 126.4607
- nvPMLTO Mass To CAEP11 (% of limit)
- 54.3202
- nvPMLTO Number (#)
- 267491300000000000
- nvPMLTO Number Per Thrust (#/kN)
- 2524616000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 84.1602
- nvPM Mass Concentration Characteristic (mg/m³)
- 3051.25
- nvPM Mass Concentration Max (mg/m³)
- 2370.516
- nvPM Mass Concentration To CAEP10 (% of limit)
- 55.7209