Maximum Takeoff Thrust
120.43 kN
Overall Pressure Ratio
31.66
Fuel Flow Take Off
0.8 kg/s
NOx Unitaryto CAEP8
51 % 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
12.28 |
Overall Pressure Ratio
31.66 |
Afterburner
No |
Pictures
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All data (75 fields)
- Name
- PW1127G1-JM
- EASA ID
- 01P18PW151
- 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
- 12.28
- Overall Pressure Ratio
- 31.66
- Maximum Takeoff Thrust (kN)
- 120.43
- Hydrocarbon Take Off (g/kg fuel)
- 0.02
- Hydrocarbon Climb Out (g/kg fuel)
- 0.04
- Hydrocarbon Approach (g/kg fuel)
- 0.02
- Hydrocarbon Idle (g/kg fuel)
- 0.43
- Hydrocarbon Unitary Average (g/kN)
- 0.51
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.6
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 3.1
- Hydrocarbon LTO (g)
- 59
- Carbon Monoxide Take Off (g/kg fuel)
- 0.22
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.3
- Carbon Monoxide Approach (g/kg fuel)
- 5.36
- Carbon Monoxide Idle (g/kg fuel)
- 27.93
- Carbon Monoxide Unitary Average (g/kN)
- 32.43
- Carbon Monoxide Unitary Characteristic (g/kN)
- 35.07
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 30
- NOx Take Off (g/kg fuel)
- 18.82
- NOx Climb Out (g/kg fuel)
- 15.3
- NOx Approach (g/kg fuel)
- 9.07
- NOx Idle (g/kg fuel)
- 4.84
- NOx Unitary Average (g/kN)
- 25.3
- NOx Unitary Characteristic (g/kN)
- 27.29
- NOx Unitaryto Standard (% of limit)
- 26
- NOx Unitaryto CAEP2 (% of limit)
- 33
- NOx Unitaryto CAEP4 (% of limit)
- 39
- NOx Unitaryto CAEP6 (% of limit)
- 44
- NOx Unitaryto CAEP8 (% of limit)
- 51
- NOx LTO (g)
- 3096
- Smoke Take Off (SN)
- 13.4
- Smoke Climb Out (SN)
- 10.5
- Smoke Approach (SN)
- 0.5
- Smoke Idle (SN)
- 1.2
- Smoke Max (SN)
- 13.4
- Smoke Characteristic (SN)
- 14.8
- Smoke Characteristicto Regulatory (% of limit)
- 66
- Fuel Flow Take Off (kg/s)
- 0.8
- Fuel Flow Climbout (kg/s)
- 0.67
- Fuel Flow Approach (kg/s)
- 0.2322
- Fuel Flow Idle (kg/s)
- 0.08
- Fuel LTO (kg)
- 303
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 3819
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 6.4464
- nvPME Imass Climb Out (mg/kg)
- 32.0653
- nvPME Imass Idle (mg/kg)
- 9.2971
- nvPME Imass Max (mg/kg)
- 62.7674
- nvPME Imass Take Off (mg/kg)
- 62.7674
- nvPME Inum Approach (#/kg)
- 370765700000000
- nvPME Inum Climb Out (#/kg)
- 676986000000000
- nvPME Inum Idle (#/kg)
- 836628200000000
- nvPME Inum Max (#/kg)
- 949866800000000
- nvPME Inum Take Off (#/kg)
- 943036700000000
- nvPMLTO Mass (mg)
- 6464.058
- nvPMLTO Mass Per Thrust (mg/kN)
- 74.6043
- nvPMLTO Mass To CAEP11 (% of limit)
- 17.8318
- nvPMLTO Number (#)
- 216614100000000000
- nvPMLTO Number Per Thrust (#/kN)
- 2500032000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 48.371
- nvPM Mass Concentration Characteristic (mg/m³)
- 1856.632
- nvPM Mass Concentration Max (mg/m³)
- 1442.417
- nvPM Mass Concentration To CAEP10 (% of limit)
- 30.7905