Maximum Takeoff Thrust
334.7 kN
Overall Pressure Ratio
38.97
Fuel Flow Take Off
2.6 kg/s
NOx Unitaryto CAEP8
84.3 % 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
Phase5 Tiled |
| 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
7.5 |
Overall Pressure Ratio
38.97 |
Afterburner
No |
Pictures
No pictures yet for this family.
Airplanes
| Name |
Model |
Aircraft Engine |
Number of Engines |
Length (m) |
Flat Wing Span (m) |
Max Seating |
|
A380-841
|
A380-800 |
Trent 970-84 |
4 |
72.72 |
79.75 |
853 |
Similar reaction turbines
All data (64 fields)
- Name
- Trent 970-84
- EASA ID
- 8RR046
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Geared Fan
- No
- Combustion Chamber
- Phase5 Tiled
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 7.5
- Overall Pressure Ratio
- 38.97
- Maximum Takeoff Thrust (kN)
- 334.7
- 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)
- 0.2
- Hydrocarbon Unitary Average (g/kN)
- 0.2
- Hydrocarbon Unitary Sigma (g/kN)
- 0.091
- Hydrocarbon Unitary Range (g/kN)
- 0.2-0.3
- Hydrocarbon Unitary Characteristic (g/kN)
- 0.4
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 1.9
- Hydrocarbon LTO (g)
- 81
- Carbon Monoxide Take Off (g/kg fuel)
- 0.4
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.2
- Carbon Monoxide Approach (g/kg fuel)
- 1.4
- Carbon Monoxide Idle (g/kg fuel)
- 15.1
- Carbon Monoxide Unitary Average (g/kN)
- 19.3
- Carbon Monoxide Unitary SD (g/kN)
- 0.083
- Carbon Monoxide Unitary Range (g/kN)
- 19-19.2
- Carbon Monoxide Unitary Characteristic (g/kN)
- 23.6
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 20
- NOx Take Off (g/kg fuel)
- 37.2
- NOx Climb Out (g/kg fuel)
- 29.1
- NOx Approach (g/kg fuel)
- 11.4
- NOx Idle (g/kg fuel)
- 5.1
- NOx Unitary Average (g/kN)
- 49.5
- NOx Unitary SD (g/kN)
- 0.772
- NOx Unitary Range (g/kN)
- 49-50.5
- NOx Unitary Characteristic (g/kN)
- 57.4
- NOx Unitaryto Standard (% of limit)
- 48.7
- NOx Unitaryto CAEP2 (% of limit)
- 60.8
- NOx Unitaryto CAEP4 (% of limit)
- 67.6
- NOx Unitaryto CAEP6 (% of limit)
- 74.6
- NOx Unitaryto CAEP8 (% of limit)
- 84.3
- NOx LTO (g)
- 16555
- Smoke Take Off (SN)
- 4.1
- Smoke Climb Out (SN)
- 4.7
- Smoke Approach (SN)
- 2.6
- Smoke Idle (SN)
- 0.7
- Smoke Max (SN)
- 5.23
- Smoke Sigma (SN)
- 1.201
- Smoke Range (SN)
- 4.1-6.5
- Smoke Characteristic (SN)
- 6.8
- Smoke Characteristicto Regulatory (% of limit)
- 39.6
- Fuel Flow Take Off (kg/s)
- 2.6
- Fuel Flow Climbout (kg/s)
- 2.2
- Fuel Flow Approach (kg/s)
- 0.7
- Fuel Flow Idle (kg/s)
- 0.3
- Fuel LTO (kg)
- 980
- Fuel Venting Compliant
- No
- Carbon Monoxide LTO (g)
- 6461
- Emissions Data Status
- C
- Emissions Data Superseded
- Yes
- Emissions Superseded By
- 18RR081
- NOx Compliance Demonstration
- 2.3.2 d)