Maximum Takeoff Thrust
81.65 kN
Overall Pressure Ratio
35.533
Fuel Flow Take Off
0.7865 kg/s
NOx Unitaryto CAEP8
80.91 % 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
Advanced Rich Burn |
| 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
5.377 |
Overall Pressure Ratio
35.533 |
Afterburner
No |
Pictures
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All data (81 fields)
- Name
- BR700-730B2-14
- EASA ID
- 06P26RR149
- Aircraft Engine Manufacturer
- Rolls-Royce Deutschland
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Advanced Rich Burn
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 5.377
- Overall Pressure Ratio
- 35.533
- Maximum Takeoff Thrust (kN)
- 81.65
- 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)
- 0.277
- Hydrocarbon Unitary Average (g/kN)
- 0.428
- Hydrocarbon Unitary Sigma (g/kN)
- 0.101
- Hydrocarbon Unitary Range (g/kN)
- 0.36-0.5
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.557
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 2.842
- Hydrocarbon LTO (g)
- 34.96
- Carbon Monoxide Take Off (g/kg fuel)
- 0.4056
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.468
- Carbon Monoxide Approach (g/kg fuel)
- 2.438
- Carbon Monoxide Idle (g/kg fuel)
- 22.216
- Carbon Monoxide Unitary Average (g/kN)
- 36.519
- Carbon Monoxide Unitary SD (g/kN)
- 0.9906
- Carbon Monoxide Unitary Range (g/kN)
- 35.82-37.22
- Carbon Monoxide Unitary Characteristic (g/kN)
- 41.6079
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 35.2609
- NOx Take Off (g/kg fuel)
- 30.392
- NOx Climb Out (g/kg fuel)
- 22.542
- NOx Approach (g/kg fuel)
- 9.766
- NOx Idle (g/kg fuel)
- 3.338
- NOx Unitary Average (g/kN)
- 47.1027
- NOx Unitary SD (g/kN)
- 1.518
- NOx Unitary Range (g/kN)
- 46.03-48.18
- NOx Unitary Characteristic (g/kN)
- 51.7953
- NOx Unitaryto Standard (% of limit)
- 46.63
- NOx Unitaryto CAEP2 (% of limit)
- 58.29
- NOx Unitaryto CAEP4 (% of limit)
- 65.288
- NOx Unitaryto CAEP6 (% of limit)
- 71.689
- NOx Unitaryto CAEP8 (% of limit)
- 80.91
- NOx LTO (g)
- 3846.03
- Smoke Take Off (SN)
- 1.94
- Smoke Climb Out (SN)
- 3.0904
- Smoke Approach (SN)
- 2.25
- Smoke Idle (SN)
- 1.161
- Smoke Max (SN)
- 4.956
- Smoke Sigma (SN)
- 0.256
- Smoke Range (SN)
- 4.8-5.1
- Smoke Characteristic (SN)
- 5.812
- Smoke Characteristicto Regulatory (% of limit)
- 23.227
- Fuel Flow Take Off (kg/s)
- 0.7865
- Fuel Flow Climbout (kg/s)
- 0.646
- Fuel Flow Approach (kg/s)
- 0.2126
- Fuel Flow Idle (kg/s)
- 0.0809
- Fuel LTO (kg)
- 295.56
- Fuel Venting Compliant
- Yes
- Carbon Monoxide LTO (g)
- 2981.87
- Emissions Data Status
- C
- NOx Compliance Demonstration
- 2.3.2 e)
- nvPME Imass Approach (mg/kg)
- 76.4
- nvPME Imass Climb Out (mg/kg)
- 95.02
- nvPME Imass Idle (mg/kg)
- 38
- nvPME Imass Max (mg/kg)
- 170.7
- nvPME Imass Take Off (mg/kg)
- 51.21
- nvPME Inum Approach (#/kg)
- 1980000000000000
- nvPME Inum Climb Out (#/kg)
- 718000000000000
- nvPME Inum Idle (#/kg)
- 1180000000000000
- nvPME Inum Max (#/kg)
- 2640000000000000
- nvPME Inum Take Off (#/kg)
- 296000000000000
- nvPMLTO Mass (mg)
- 18491.08
- nvPMLTO Mass Per Thrust (mg/kN)
- 277.9
- nvPMLTO Mass To CAEP11 (% of limit)
- 40.48
- nvPMLTO Number (#)
- 321000000000000000
- nvPMLTO Number Per Thrust (#/kN)
- 4830000000000000
- nvPMLTO Number To CAEP11 (% of limit)
- 58.19
- nvPM Mass Concentration Characteristic (mg/m³)
- 558.06
- nvPM Mass Concentration Max (mg/m³)
- 475.86
- nvPM Mass Concentration To CAEP10 (% of limit)
- 7.56