Trent 1000-R3

Maximum Takeoff Thrust
363.8735 kN
Bypass Ratio
8.8835
Overall Pressure Ratio
49.5509
Fuel Flow Take Off
2.8719 kg/s
NOx Unitaryto CAEP8
90.0452 % 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 8.8835 Overall Pressure Ratio 49.5509 Afterburner No

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
Trent 1000-R3 Rolls-Royce 363.9 8.9 49.4 Compare
Trent 1000-M3 Rolls-Royce 358.1 8.9 48.7 Compare
Trent 1000 -N3 Rolls-Royce 358.1 8.9 48.7 Compare
Trent 1000-N3 Rolls-Royce 358.1 8.9 48.7 Compare
GE90-77B GE Aircraft Engines 363.42 8.6 35.2 Compare
GE90-76B General Electric Company 363.22 8.53 35.5 Compare
All data (82 fields)
Name
Trent 1000-R3
EASA ID
02P23RR138
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Geared Fan
No
Combustion Chamber
Phase5 Tiled
Afterburner
No
Streams
2
Bypass Ratio
8.8835
Overall Pressure Ratio
49.5509
Maximum Takeoff Thrust (kN)
363.8735
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
Hydrocarbon Unitary Average (g/kN)
0
Hydrocarbon Unitary Sigma (g/kN)
0
Hydrocarbon Unitary Range (g/kN)
0-0
Hydrocarbon Unitary Characteristic (g/kN)
0
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
0
Hydrocarbon LTO (g)
0
Carbon Monoxide Take Off (g/kg fuel)
0.434
Carbon Monoxide Climb Out (g/kg fuel)
0.4313
Carbon Monoxide Approach (g/kg fuel)
0.525
Carbon Monoxide Idle (g/kg fuel)
5.9151
Carbon Monoxide Unitary Average (g/kN)
7.6094
Carbon Monoxide Unitary SD (g/kN)
1.2472
Carbon Monoxide Unitary Range (g/kN)
6.32-9.17
Carbon Monoxide Unitary Characteristic (g/kN)
8.04
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
6.8
NOx Take Off (g/kg fuel)
67.2866
NOx Climb Out (g/kg fuel)
47.8925
NOx Approach (g/kg fuel)
14.8882
NOx Idle (g/kg fuel)
6.2364
NOx Unitary Average (g/kN)
77.1665
NOx Unitary SD (g/kN)
0.8639
NOx Unitary Range (g/kN)
75.86-77.98
NOx Unitary Characteristic (g/kN)
80.3399
NOx Unitaryto Standard (% of limit)
57.7562
NOx Unitaryto CAEP2 (% of limit)
72.1953
NOx Unitaryto CAEP4 (% of limit)
75.7197
NOx Unitaryto CAEP6 (% of limit)
81.9279
NOx Unitaryto CAEP8 (% of limit)
90.0452
NOx LTO (g)
28077.44
Smoke Take Off (SN)
7.8048
Smoke Climb Out (SN)
9.7465
Smoke Approach (SN)
10.154
Smoke Idle (SN)
1.7842
Smoke Max (SN)
14.7
Smoke Sigma (SN)
2
Smoke Range (SN)
11.4-16.7
Smoke Characteristic (SN)
16.4
Smoke Characteristicto Regulatory (% of limit)
98.6
Fuel Flow Take Off (kg/s)
2.8719
Fuel Flow Climbout (kg/s)
2.3219
Fuel Flow Approach (kg/s)
0.7435
Fuel Flow Idle (kg/s)
0.2699
Fuel LTO (kg)
1026.596
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
2768.705
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)
nvPME Imass Approach (mg/kg)
84.522
nvPME Imass Climb Out (mg/kg)
58.3213
nvPME Imass Idle (mg/kg)
19.4339
nvPME Imass Max (mg/kg)
154.1347
nvPME Imass Take Off (mg/kg)
40.8116
nvPME Inum Approach (#/kg)
896117500000000
nvPME Inum Climb Out (#/kg)
184355800000000
nvPME Inum Idle (#/kg)
474920300000000
nvPME Inum Max (#/kg)
932130000000000
nvPME Inum Take Off (#/kg)
99613180000000
nvPMLTO Mass (mg)
46062.68
nvPMLTO Mass Per Thrust (mg/kN)
175.9658
nvPMLTO Mass To CAEP11 (% of limit)
82.227
nvPMLTO Number (#)
428384800000000000
nvPMLTO Number Per Thrust (#/kN)
1636490000000000
nvPMLTO Number To CAEP11 (% of limit)
58.8665
nvPM Mass Concentration Characteristic (mg/m³)
3409.81
nvPM Mass Concentration Max (mg/m³)
2649.081
nvPM Mass Concentration To CAEP10 (% of limit)
90.4434