Maximum Takeoff Thrust
28.49 kN
Overall Pressure Ratio
20.21
Fuel Flow Take Off
0.327 kg/s
NOx Unitaryto CAEP8
75 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
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 II |
| 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
4.2 |
Overall Pressure Ratio
20.21 |
Afterburner
No |
Pictures
No pictures yet for this family.
Similar reaction turbines
All data (82 fields)
- Name
- PW307A
- EASA ID
- 01P16PW143
- Aircraft Engine Manufacturer
- Pratt & Whitney Canada
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A-1
- Geared Fan
- No
- Combustion Chamber
- TALON II
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 4.2
- Overall Pressure Ratio
- 20.21
- Maximum Takeoff Thrust (kN)
- 28.49
- Hydrocarbon Take Off (g/kg fuel)
- 0
- Hydrocarbon Climb Out (g/kg fuel)
- 0
- Hydrocarbon Approach (g/kg fuel)
- 0
- Hydrocarbon Idle (g/kg fuel)
- 1.99
- Hydrocarbon Unitary Average (g/kN)
- 4.8
- Hydrocarbon Unitary Sigma (g/kN)
- 1.5
- Hydrocarbon Unitary Range (g/kN)
- 3.2-6.2
- Hydrocarbon Unitary Characteristic (g/kN)
- 5.6
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 28.6
- Hydrocarbon LTO (g)
- 137
- Carbon Monoxide Take Off (g/kg fuel)
- 0.27
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.23
- Carbon Monoxide Approach (g/kg fuel)
- 3.23
- Carbon Monoxide Idle (g/kg fuel)
- 36.92
- Carbon Monoxide Unitary Average (g/kN)
- 91.6
- Carbon Monoxide Unitary SD (g/kN)
- 6.5
- Carbon Monoxide Unitary Range (g/kN)
- 85.4-98.4
- Carbon Monoxide Unitary Characteristic (g/kN)
- 99.1
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 84
- NOx Take Off (g/kg fuel)
- 18.28
- NOx Climb Out (g/kg fuel)
- 15.58
- NOx Approach (g/kg fuel)
- 8.77
- NOx Idle (g/kg fuel)
- 2.86
- NOx Unitary Average (g/kN)
- 42.8
- NOx Unitary SD (g/kN)
- 0.7
- NOx Unitary Range (g/kN)
- 42-43.3
- NOx Unitary Characteristic (g/kN)
- 45.3
- NOx Unitaryto Standard (% of limit)
- 56.3
- NOx Unitaryto CAEP2 (% of limit)
- 70.4
- NOx Unitaryto CAEP4 (% of limit)
- 70.8
- NOx Unitaryto CAEP6 (% of limit)
- 71
- NOx Unitaryto CAEP8 (% of limit)
- 75
- NOx LTO (g)
- 1221
- Smoke Take Off (SN)
- 0.65
- Smoke Climb Out (SN)
- 0.32
- Smoke Approach (SN)
- 0
- Smoke Idle (SN)
- 1.69
- Smoke Max (SN)
- 1.7
- Smoke Sigma (SN)
- 0.2
- Smoke Range (SN)
- 1.5-1.9
- Smoke Characteristic (SN)
- 1.9
- Smoke Characteristicto Regulatory (% of limit)
- 5.7
- Fuel Flow Take Off (kg/s)
- 0.327
- Fuel Flow Climbout (kg/s)
- 0.272
- Fuel Flow Approach (kg/s)
- 0.102
- Fuel Flow Idle (kg/s)
- 0.044
- Fuel LTO (kg)
- 143
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2625
- Emissions Data Status
- C/R
- Emissions Data Superseded
- Yes
- Emissions Superseded By
- 03P16PW192
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 6.6546
- nvPME Imass Climb Out (mg/kg)
- 36.0186
- nvPME Imass Idle (mg/kg)
- 272.7275
- nvPME Imass Max (mg/kg)
- 272.7275
- nvPME Imass Take Off (mg/kg)
- 56.9571
- nvPME Inum Approach (#/kg)
- 288180300000000
- nvPME Inum Climb Out (#/kg)
- 629288200000000
- nvPME Inum Idle (#/kg)
- 1918252000000000
- nvPME Inum Max (#/kg)
- 1918252000000000
- nvPME Inum Take Off (#/kg)
- 646151100000000
- nvPMLTO Mass (mg)
- 21267.62
- nvPMLTO Mass Per Thrust (mg/kN)
- 746.4942
- nvPMLTO Number (#)
- 172350900000000000
- nvPMLTO Number Per Thrust (#/kN)
- 6049523000000000
- nvPM Mass Concentration Characteristic (mg/m³)
- 1249.798
- nvPM Mass Concentration Max (mg/m³)
- 970.968
- nvPM Mass Concentration To CAEP10 (% of limit)
- 8.9938