Maximum Takeoff Thrust
61.6 kN
Overall Pressure Ratio
15.88
Fuel Flow Take Off
0.731 kg/s
NOx Unitaryto CAEP8
105.1 % 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
Tubular |
| 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
3.26 |
Overall Pressure Ratio
15.88 |
Afterburner
No |
Pictures
No pictures yet for this family.
Similar reaction turbines
All data (63 fields)
- Name
- TAY611-8C
- EASA ID
- 11RR048
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Tubular
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 3.26
- Overall Pressure Ratio
- 15.88
- Maximum Takeoff Thrust (kN)
- 61.6
- Hydrocarbon Take Off (g/kg fuel)
- 0.03
- Hydrocarbon Climb Out (g/kg fuel)
- 0.05
- Hydrocarbon Approach (g/kg fuel)
- 0.65
- Hydrocarbon Idle (g/kg fuel)
- 1.49
- Hydrocarbon Unitary Average (g/kN)
- 4.465
- Hydrocarbon Unitary Sigma (g/kN)
- 1.308
- Hydrocarbon Unitary Range (g/kN)
- 2.57-5.62
- Hydrocarbon Unitary Characteristic (g/kN)
- 5.2
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 26.6
- Hydrocarbon LTO (g)
- 275
- Carbon Monoxide Take Off (g/kg fuel)
- 0.5
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.95
- Carbon Monoxide Approach (g/kg fuel)
- 2.89
- Carbon Monoxide Idle (g/kg fuel)
- 24.4
- Carbon Monoxide Unitary Average (g/kN)
- 66.9
- Carbon Monoxide Unitary SD (g/kN)
- 11.5
- Carbon Monoxide Unitary Range (g/kN)
- 59.55-82.67
- Carbon Monoxide Unitary Characteristic (g/kN)
- 72.4
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 61.3
- NOx Take Off (g/kg fuel)
- 19.3
- NOx Climb Out (g/kg fuel)
- 15.4
- NOx Approach (g/kg fuel)
- 5.31
- NOx Idle (g/kg fuel)
- 2.53
- NOx Unitary Average (g/kN)
- 40.58
- NOx Unitary SD (g/kN)
- 0.9
- NOx Unitary Range (g/kN)
- 39.5-41.7
- NOx Unitary Characteristic (g/kN)
- 43
- NOx Unitaryto Standard (% of limit)
- 59.9
- NOx Unitaryto CAEP2 (% of limit)
- 74.9
- NOx Unitaryto CAEP4 (% of limit)
- 85.7
- NOx Unitaryto CAEP6 (% of limit)
- 91.2
- NOx Unitaryto CAEP8 (% of limit)
- 105.1
- NOx LTO (g)
- 2500
- Smoke Take Off (SN)
- 4.39
- Smoke Climb Out (SN)
- 3.46
- Smoke Approach (SN)
- 0.46
- Smoke Idle (SN)
- 0.21
- Smoke Max (SN)
- 4.7
- Smoke Sigma (SN)
- 0.59
- Smoke Range (SN)
- 3.67-5.2
- Smoke Characteristic (SN)
- 5.2
- Smoke Characteristicto Regulatory (% of limit)
- 19.1
- Fuel Flow Take Off (kg/s)
- 0.731
- Fuel Flow Climbout (kg/s)
- 0.604
- Fuel Flow Approach (kg/s)
- 0.215
- Fuel Flow Idle (kg/s)
- 0.102
- Fuel LTO (kg)
- 321
- Fuel Venting Compliant
- No
- Carbon Monoxide LTO (g)
- 4123
- Emissions Data Status
- C/R
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 d)