V2522-A5 SelectOne™ Upgrade Package
Maximum Takeoff Thrust
102.5 kN
Overall Pressure Ratio
25.7
Fuel Flow Take Off
0.971 kg/s
NOx Unitaryto CAEP8
111.2 % 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
Floatwall |
| 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
4.9 |
Overall Pressure Ratio
25.7 |
Afterburner
No |
Pictures
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All data (75 fields)
- Name
- V2522-A5 SelectOne™ Upgrade Package
- EASA ID
- 01P10IA019
- Aircraft Engine Manufacturer
- International Aero Engines
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Combustion Chamber
- Floatwall
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 4.9
- Overall Pressure Ratio
- 25.7
- Maximum Takeoff Thrust (kN)
- 102.5
- Hydrocarbon Take Off (g/kg fuel)
- 0.03
- Hydrocarbon Climb Out (g/kg fuel)
- 0.04
- Hydrocarbon Approach (g/kg fuel)
- 0.07
- Hydrocarbon Idle (g/kg fuel)
- 0.14
- Hydrocarbon Unitary Average (g/kN)
- 0.4
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.5
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 2.5
- Hydrocarbon LTO (g)
- 39
- Carbon Monoxide Take Off (g/kg fuel)
- 0.43
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.44
- Carbon Monoxide Approach (g/kg fuel)
- 2.55
- Carbon Monoxide Idle (g/kg fuel)
- 12.49
- Carbon Monoxide Unitary Average (g/kN)
- 27.1
- Carbon Monoxide Unitary Characteristic (g/kN)
- 30.9
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 26.2
- NOx Take Off (g/kg fuel)
- 21.34
- NOx Climb Out (g/kg fuel)
- 18.33
- NOx Approach (g/kg fuel)
- 9.32
- NOx Idle (g/kg fuel)
- 5.09
- NOx Unitary Average (g/kN)
- 44.5
- NOx Unitary Characteristic (g/kN)
- 49
- NOx Unitaryto Standard (% of limit)
- 53.6
- NOx Unitaryto CAEP2 (% of limit)
- 67
- NOx Unitaryto CAEP4 (% of limit)
- 81.5
- NOx Unitaryto CAEP6 (% of limit)
- 92.6
- NOx Unitaryto CAEP8 (% of limit)
- 111.2
- NOx LTO (g)
- 4563
- Smoke Take Off (SN)
- 7.3
- Smoke Climb Out (SN)
- 8.1
- Smoke Approach (SN)
- 3.2
- Smoke Idle (SN)
- 1.7
- Smoke Max (SN)
- 9.4
- Smoke Characteristic (SN)
- 11.1
- Smoke Characteristicto Regulatory (% of limit)
- 47.1
- Fuel Flow Take Off (kg/s)
- 0.971
- Fuel Flow Climbout (kg/s)
- 0.815
- Fuel Flow Approach (kg/s)
- 0.31
- Fuel Flow Idle (kg/s)
- 0.13
- Fuel LTO (kg)
- 425
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2780
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 d)
- nvPME Imass Approach (mg/kg)
- 211.4279
- nvPME Imass Climb Out (mg/kg)
- 372.0247
- nvPME Imass Idle (mg/kg)
- 77.7508
- nvPME Imass Max (mg/kg)
- 448.8712
- nvPME Imass Take Off (mg/kg)
- 279.1137
- nvPME Inum Approach (#/kg)
- 2240590000000000
- nvPME Inum Climb Out (#/kg)
- 1571482000000000
- nvPME Inum Idle (#/kg)
- 1666323000000000
- nvPME Inum Max (#/kg)
- 2868338000000000
- nvPME Inum Take Off (#/kg)
- 1246694000000000
- nvPMLTO Mass (mg)
- 82834.26
- nvPMLTO Mass Per Thrust (mg/kN)
- 1123.351
- nvPMLTO Mass To CAEP11 (% of limit)
- 206.9
- nvPMLTO Number (#)
- 723216100000000000
- nvPMLTO Number Per Thrust (#/kN)
- 9807850000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 148.2
- nvPM Mass Concentration Characteristic (mg/m³)
- 1766
- nvPM Mass Concentration Max (mg/m³)
- 1372.3
- nvPM Mass Concentration To CAEP10 (% of limit)
- 27