Maximum Takeoff Thrust
92.79 kN
Overall Pressure Ratio
33.27
Fuel Flow Take Off
0.65 kg/s
NOx Unitaryto CAEP8
61 % 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
11.6 |
Overall Pressure Ratio
33.27 |
Afterburner
No |
Pictures
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All data (80 fields)
- Name
- PW1919G
- EASA ID
- 01P20PW187
- 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
- 11.6
- Overall Pressure Ratio
- 33.27
- Maximum Takeoff Thrust (kN)
- 92.79
- Hydrocarbon Take Off (g/kg fuel)
- 0
- Hydrocarbon Climb Out (g/kg fuel)
- 0
- Hydrocarbon Approach (g/kg fuel)
- 0.1
- Hydrocarbon Idle (g/kg fuel)
- 0.2
- Hydrocarbon Unitary Average (g/kN)
- 0.3
- Hydrocarbon Unitary Range (g/kN)
- 0.2-0.4
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.4
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 2
- Hydrocarbon LTO (g)
- 25
- Carbon Monoxide Take Off (g/kg fuel)
- 0
- Carbon Monoxide Climb Out (g/kg fuel)
- 0
- Carbon Monoxide Approach (g/kg fuel)
- 3.3
- Carbon Monoxide Idle (g/kg fuel)
- 22.2
- Carbon Monoxide Unitary Average (g/kN)
- 27
- Carbon Monoxide Unitary Range (g/kN)
- 26.7-27.6
- Carbon Monoxide Unitary Characteristic (g/kN)
- 33.2
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 28
- NOx Take Off (g/kg fuel)
- 20
- NOx Climb Out (g/kg fuel)
- 16.7
- NOx Approach (g/kg fuel)
- 9.8
- NOx Idle (g/kg fuel)
- 5.2
- NOx Unitary Average (g/kN)
- 29.6
- NOx Unitary Range (g/kN)
- 29.4-29.8
- NOx Unitary Characteristic (g/kN)
- 34.3
- NOx Unitaryto Standard (% of limit)
- 32
- NOx Unitaryto CAEP2 (% of limit)
- 40
- NOx Unitaryto CAEP4 (% of limit)
- 47
- NOx Unitaryto CAEP6 (% of limit)
- 52
- NOx Unitaryto CAEP8 (% of limit)
- 61
- NOx LTO (g)
- 2746
- Smoke Take Off (SN)
- 2
- Smoke Climb Out (SN)
- 1.3
- Smoke Approach (SN)
- 0.8
- Smoke Idle (SN)
- 0.5
- Smoke Max (SN)
- 2
- Smoke Range (SN)
- 1.7-2.3
- Smoke Characteristic (SN)
- 2.6
- Smoke Characteristicto Regulatory (% of limit)
- 11
- Fuel Flow Take Off (kg/s)
- 0.65
- Fuel Flow Climbout (kg/s)
- 0.54
- Fuel Flow Approach (kg/s)
- 0.2
- Fuel Flow Idle (kg/s)
- 0.07
- Fuel LTO (kg)
- 251.7
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2508
- Emissions Data Status
- C
- Emissions Data Superseded
- Yes
- Emissions Superseded By
- 04P20PW200
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 0.1686
- nvPME Imass Climb Out (mg/kg)
- 3.5826
- nvPME Imass Idle (mg/kg)
- 0.7614
- nvPME Imass Max (mg/kg)
- 8.0606
- nvPME Imass Take Off (mg/kg)
- 8.0606
- nvPME Inum Approach (#/kg)
- 16931440000000
- nvPME Inum Climb Out (#/kg)
- 140183800000000
- nvPME Inum Idle (#/kg)
- 90063890000000
- nvPME Inum Max (#/kg)
- 186895400000000
- nvPME Inum Take Off (#/kg)
- 186895400000000
- nvPMLTO Mass (mg)
- 564.0733
- nvPMLTO Mass Per Thrust (mg/kN)
- 8.4501
- nvPMLTO Mass To CAEP11 (% of limit)
- 1.4
- nvPMLTO Number (#)
- 25437490000000000
- nvPMLTO Number Per Thrust (#/kN)
- 381068100000000
- nvPMLTO Number To CAEP11 (% of limit)
- 5.1
- nvPM Mass Concentration Characteristic (mg/m³)
- 247.4
- nvPM Mass Concentration Max (mg/m³)
- 192.2
- nvPM Mass Concentration To CAEP10 (% of limit)
- 3.6