Trent 1000-H3

Maximum Takeoff Thrust
287.1372 kN
Bypass Ratio
9.282
Overall Pressure Ratio
40.3476
Fuel Flow Take Off
2.1075 kg/s
NOx Unitaryto CAEP8
76.5202 % 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 9.282 Overall Pressure Ratio 40.3476 Afterburner No

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
Trent 1000-H3 Rolls-Royce 287.1 9.3 40.1 Compare
Trent 1000-H2 Rolls-Royce 287.1 9.49 38.52 Compare
Trent 1000-H Rolls-Royce 287.1 9.62 38.33 Compare
Trent 1000-E Rolls-Royce 279.8 9.67 37.51 Compare
GEnx-1B64/P2 General Electric Company 298.0353 9.0819 40.6539 Compare
GEnx-1B64 GE Aircraft Engines 298 9 40.6 Compare
All data (82 fields)
Name
Trent 1000-H3
EASA ID
02P23RR130
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Geared Fan
No
Combustion Chamber
Phase5 Tiled
Afterburner
No
Streams
2
Bypass Ratio
9.282
Overall Pressure Ratio
40.3476
Maximum Takeoff Thrust (kN)
287.1372
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)
0.427
Carbon Monoxide Climb Out (g/kg fuel)
0.385
Carbon Monoxide Approach (g/kg fuel)
0.8262
Carbon Monoxide Idle (g/kg fuel)
8.3928
Carbon Monoxide Unitary Average (g/kN)
11.4447
Carbon Monoxide Unitary SD (g/kN)
2.0505
Carbon Monoxide Unitary Range (g/kN)
7.4-14.1
Carbon Monoxide Unitary Characteristic (g/kN)
12
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
10.2
NOx Take Off (g/kg fuel)
42.1376
NOx Climb Out (g/kg fuel)
32.826
NOx Approach (g/kg fuel)
13.0422
NOx Idle (g/kg fuel)
5.2915
NOx Unitary Average (g/kN)
52.3346
NOx Unitary SD (g/kN)
0.892
NOx Unitary Range (g/kN)
50.9-53.47
NOx Unitary Characteristic (g/kN)
54.1879
NOx Unitaryto Standard (% of limit)
44.8965
NOx Unitaryto CAEP2 (% of limit)
56.1206
NOx Unitaryto CAEP4 (% of limit)
61.7912
NOx Unitaryto CAEP6 (% of limit)
68.0281
NOx Unitaryto CAEP8 (% of limit)
76.5202
NOx LTO (g)
15026.47
Smoke Take Off (SN)
11.1422
Smoke Climb Out (SN)
13.7777
Smoke Approach (SN)
7.6908
Smoke Idle (SN)
2.1653
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)
92.4
Fuel Flow Take Off (kg/s)
2.1075
Fuel Flow Climbout (kg/s)
1.7323
Fuel Flow Approach (kg/s)
0.5983
Fuel Flow Idle (kg/s)
0.2323
Fuel LTO (kg)
823.1809
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
3286.042
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)
nvPME Imass Approach (mg/kg)
64.1533
nvPME Imass Climb Out (mg/kg)
114.0449
nvPME Imass Idle (mg/kg)
18.3136
nvPME Imass Max (mg/kg)
150.392
nvPME Imass Take Off (mg/kg)
71.5551
nvPME Inum Approach (#/kg)
811570200000000
nvPME Inum Climb Out (#/kg)
417370300000000
nvPME Inum Idle (#/kg)
434505600000000
nvPME Inum Max (#/kg)
918210000000000
nvPME Inum Take Off (#/kg)
236022300000000
nvPMLTO Mass (mg)
48260.9
nvPMLTO Mass Per Thrust (mg/kN)
233.6337
nvPMLTO Mass To CAEP11 (% of limit)
109.1746
nvPMLTO Number (#)
390335500000000000
nvPMLTO Number Per Thrust (#/kN)
1889636000000000
nvPMLTO Number To CAEP11 (% of limit)
67.9725
nvPM Mass Concentration Characteristic (mg/m³)
3409.81
nvPM Mass Concentration Max (mg/m³)
2649.081
nvPM Mass Concentration To CAEP10 (% of limit)
82.7371