V2530-A5 SelectOne™ Upgrade Package
Maximum Takeoff Thrust
133 kN
Overall Pressure Ratio
32
Fuel Flow Take Off
1.325 kg/s
NOx Unitaryto CAEP8
113.3 % 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
4.6 |
Overall Pressure Ratio
32 |
Afterburner
No |
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All data (75 fields)
- Name
- V2530-A5 SelectOne™ Upgrade Package
- EASA ID
- 04P10IA027
- 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
- 4.6
- Overall Pressure Ratio
- 32
- Maximum Takeoff Thrust (kN)
- 133
- Hydrocarbon Take Off (g/kg fuel)
- 0.02
- Hydrocarbon Climb Out (g/kg fuel)
- 0.03
- Hydrocarbon Approach (g/kg fuel)
- 0.06
- Hydrocarbon Idle (g/kg fuel)
- 0.12
- Hydrocarbon Unitary Average (g/kN)
- 0.3
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.4
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 1.9
- Hydrocarbon LTO (g)
- 38
- Carbon Monoxide Take Off (g/kg fuel)
- 0.39
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.41
- Carbon Monoxide Approach (g/kg fuel)
- 1.65
- Carbon Monoxide Idle (g/kg fuel)
- 10.45
- Carbon Monoxide Unitary Average (g/kN)
- 19.5
- Carbon Monoxide Unitary Characteristic (g/kN)
- 22.2
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 18.8
- NOx Take Off (g/kg fuel)
- 31.43
- NOx Climb Out (g/kg fuel)
- 23.92
- NOx Approach (g/kg fuel)
- 10.92
- NOx Idle (g/kg fuel)
- 5.52
- NOx Unitary Average (g/kN)
- 55.7
- NOx Unitary Characteristic (g/kN)
- 61.3
- NOx Unitaryto Standard (% of limit)
- 59
- NOx Unitaryto CAEP2 (% of limit)
- 73.7
- NOx Unitaryto CAEP4 (% of limit)
- 86.4
- NOx Unitaryto CAEP6 (% of limit)
- 97.4
- NOx Unitaryto CAEP8 (% of limit)
- 113.3
- NOx LTO (g)
- 7414
- Smoke Take Off (SN)
- 3.7
- Smoke Climb Out (SN)
- 6.6
- Smoke Approach (SN)
- 5.7
- Smoke Idle (SN)
- 1.4
- Smoke Max (SN)
- 9.4
- Smoke Characteristic (SN)
- 11.1
- Smoke Characteristicto Regulatory (% of limit)
- 50.5
- Fuel Flow Take Off (kg/s)
- 1.325
- Fuel Flow Climbout (kg/s)
- 1.078
- Fuel Flow Approach (kg/s)
- 0.387
- Fuel Flow Idle (kg/s)
- 0.145
- Fuel LTO (kg)
- 517
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2594
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 d)
- nvPME Imass Approach (mg/kg)
- 320.5233
- nvPME Imass Climb Out (mg/kg)
- 215.4319
- nvPME Imass Idle (mg/kg)
- 59.2248
- nvPME Imass Max (mg/kg)
- 450.2573
- nvPME Imass Take Off (mg/kg)
- 114.118
- nvPME Inum Approach (#/kg)
- 2731664000000000
- nvPME Inum Climb Out (#/kg)
- 990818400000000
- nvPME Inum Idle (#/kg)
- 1424784000000000
- nvPME Inum Max (#/kg)
- 2873864000000000
- nvPME Inum Take Off (#/kg)
- 339353900000000
- nvPMLTO Mass (mg)
- 80172.63
- nvPMLTO Mass Per Thrust (mg/kN)
- 838.3277
- nvPMLTO Mass To CAEP11 (% of limit)
- 252.8602
- nvPMLTO Number (#)
- 735877600000000000
- nvPMLTO Number Per Thrust (#/kN)
- 7693076000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 185.2147
- nvPM Mass Concentration Characteristic (mg/m³)
- 1766
- nvPM Mass Concentration Max (mg/m³)
- 1372
- nvPM Mass Concentration To CAEP10 (% of limit)
- 30.7