Trent 1000-G3

Maximum Takeoff Thrust
323.7283 kN
Bypass Ratio
9.074
Overall Pressure Ratio
44.6969
Fuel Flow Take Off
2.4492 kg/s
NOx Unitaryto CAEP8
81.2417 % 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 9.074 Overall Pressure Ratio 44.6969 Afterburner No

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Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
Trent 1000-G3 Rolls-Royce 323.7 9.1 44.5 Compare
Trent 1000-G2 Rolls-Royce 323.7 9.23 42.81 Compare
Trent7000-72 Rolls-Royce 327.914 9.0559 44.62 Compare
Trent7000-72C Rolls-Royce 327.914 9.0559 44.62 Compare
Trent7000-72D Rolls-Royce 327.914 9.0559 44.62 Compare
GEnx-1B70/75/P2, 1B70/72/P2, 1B70C/P2, 1B70/P2 General Electric Company 321.6064 8.8829 43.5248 Compare
All data (82 fields)
Name
Trent 1000-G3
EASA ID
02P23RR129
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Geared Fan
No
Combustion Chamber
Phase5 Tiled
Afterburner
No
Streams
2
Bypass Ratio
9.074
Overall Pressure Ratio
44.6969
Maximum Takeoff Thrust (kN)
323.7283
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)
0.4326
Carbon Monoxide Climb Out (g/kg fuel)
0.418
Carbon Monoxide Approach (g/kg fuel)
0.6511
Carbon Monoxide Idle (g/kg fuel)
6.8971
Carbon Monoxide Unitary Average (g/kN)
9.1163
Carbon Monoxide Unitary SD (g/kN)
1.7283
Carbon Monoxide Unitary Range (g/kN)
5.84-11.33
Carbon Monoxide Unitary Characteristic (g/kN)
9.56
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
8.1
NOx Take Off (g/kg fuel)
51.9266
NOx Climb Out (g/kg fuel)
39.3035
NOx Approach (g/kg fuel)
13.982
NOx Idle (g/kg fuel)
5.6704
NOx Unitary Average (g/kN)
62.3891
NOx Unitary SD (g/kN)
0.7662
NOx Unitary Range (g/kN)
61.46-63.48
NOx Unitary Characteristic (g/kN)
64.5984
NOx Unitaryto Standard (% of limit)
49.9238
NOx Unitaryto CAEP2 (% of limit)
62.4048
NOx Unitaryto CAEP4 (% of limit)
67.015
NOx Unitaryto CAEP6 (% of limit)
73.1133
NOx Unitaryto CAEP8 (% of limit)
81.2417
NOx LTO (g)
20196.11
Smoke Take Off (SN)
8.7858
Smoke Climb Out (SN)
11.9715
Smoke Approach (SN)
8.9136
Smoke Idle (SN)
1.9567
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)
95.5
Fuel Flow Take Off (kg/s)
2.4492
Fuel Flow Climbout (kg/s)
2.0055
Fuel Flow Approach (kg/s)
0.6666
Fuel Flow Idle (kg/s)
0.2502
Fuel LTO (kg)
917.8536
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
2951.064
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)
nvPME Imass Approach (mg/kg)
73.6268
nvPME Imass Climb Out (mg/kg)
84.4271
nvPME Imass Idle (mg/kg)
18.9856
nvPME Imass Max (mg/kg)
152.4431
nvPME Imass Take Off (mg/kg)
48.6841
nvPME Inum Approach (#/kg)
855949100000000
nvPME Inum Climb Out (#/kg)
284459000000000
nvPME Inum Idle (#/kg)
452375000000000
nvPME Inum Max (#/kg)
926180000000000
nvPME Inum Take Off (#/kg)
147753900000000
nvPMLTO Mass (mg)
46547.02
nvPMLTO Mass Per Thrust (mg/kN)
199.8669
nvPMLTO Mass To CAEP11 (% of limit)
93.3957
nvPMLTO Number (#)
403995400000000000
nvPMLTO Number Per Thrust (#/kN)
1734704000000000
nvPMLTO Number To CAEP11 (% of limit)
62.3994
nvPM Mass Concentration Characteristic (mg/m³)
3409.81
nvPM Mass Concentration Max (mg/m³)
2649.081
nvPM Mass Concentration To CAEP10 (% of limit)
86.6146