Maximum Takeoff Thrust
134 kN
Overall Pressure Ratio
35.52
Fuel Flow Take Off
0.910084 kg/s
NOx Unitaryto CAEP8
56.09 % 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 |
| 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
11.7 |
Overall Pressure Ratio
35.52 |
Afterburner
No |
Pictures
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Airplanes
| Name |
Model |
Aircraft Engine |
Number of Engines |
Length (m) |
Flat Wing Span (m) |
Two Class Typical Seating |
Max Seating |
|
A321-272N
|
A321neo |
PW1130G-JM |
2 |
44.51 |
35.8 |
206 |
244 |
|
A321-272NX
|
A321neo |
PW1130G-JM |
2 |
44.51 |
35.8 |
206 |
244 |
Similar reaction turbines
All data (56 fields)
- Name
- PW1130G-JM
- EASA ID
- 15PW106
- Aircraft Engine Manufacturer
- Pratt & Whitney
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- Yes
- Combustion Chamber
- TALON X
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 11.7
- Overall Pressure Ratio
- 35.52
- Maximum Takeoff Thrust (kN)
- 134
- Hydrocarbon Take Off (g/kg fuel)
- 0.03
- Hydrocarbon Climb Out (g/kg fuel)
- 0.03
- Hydrocarbon Approach (g/kg fuel)
- 0.04
- Hydrocarbon Idle (g/kg fuel)
- 0.07
- Hydrocarbon Unitary Average (g/kN)
- 0.1
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.2
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 1.02
- Hydrocarbon LTO (g)
- 18
- Carbon Monoxide Take Off (g/kg fuel)
- 0.17
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.25
- Carbon Monoxide Approach (g/kg fuel)
- 4.55
- Carbon Monoxide Idle (g/kg fuel)
- 19.48
- Carbon Monoxide Unitary Average (g/kN)
- 23.7
- Carbon Monoxide Unitary Characteristic (g/kN)
- 29.1
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 24.66
- NOx Take Off (g/kg fuel)
- 21.16
- NOx Climb Out (g/kg fuel)
- 16.33
- NOx Approach (g/kg fuel)
- 8.99
- NOx Idle (g/kg fuel)
- 6.78
- NOx Unitary Average (g/kN)
- 29.6
- NOx Unitary Characteristic (g/kN)
- 34.3
- NOx Unitaryto Standard (% of limit)
- 30.89
- NOx Unitaryto CAEP2 (% of limit)
- 38.61
- NOx Unitaryto CAEP4 (% of limit)
- 43.95
- NOx Unitaryto CAEP6 (% of limit)
- 49
- NOx Unitaryto CAEP8 (% of limit)
- 56.09
- NOx LTO (g)
- 3969
- Smoke Take Off (SN)
- 2.8
- Smoke Climb Out (SN)
- 0.79
- Smoke Approach (SN)
- 0.35
- Smoke Idle (SN)
- 0.55
- Smoke Max (SN)
- 2.8
- Smoke Characteristic (SN)
- 3.6
- Smoke Characteristicto Regulatory (% of limit)
- 16.48
- Fuel Flow Take Off (kg/s)
- 0.910084
- Fuel Flow Climbout (kg/s)
- 0.748352
- Fuel Flow Approach (kg/s)
- 0.254698
- Fuel Flow Idle (kg/s)
- 0.094272
- Fuel LTO (kg)
- 345.2
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 3174
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)