Trent 1000-H2

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
287.1 kN
Bypass Ratio
9.49
Overall Pressure Ratio
38.52
Fuel Flow Take Off
2.075 kg/s
NOx Unitaryto CAEP8
77.93 % 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 9.49 Overall Pressure Ratio 38.52 Afterburner No

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
Trent 1000-H Rolls-Royce 287.1 9.62 38.33 Compare
Trent 1000-H3 Rolls-Royce 287.1372 9.319 39.6253 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-1B58/P2 General Electric Company 271.3415 9.3341 37.3864 Compare
GEnx-1B64 GE Aircraft Engines 298 9 40.6 Compare
All data (63 fields)
Name
Trent 1000-H2
EASA ID
12RR066
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Geared Fan
No
Combustion Chamber
Phase5 Tiled
Afterburner
No
Streams
2
Bypass Ratio
9.49
Overall Pressure Ratio
38.52
Maximum Takeoff Thrust (kN)
287.1
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)
0.07
Hydrocarbon Unitary Average (g/kN)
0.09
Hydrocarbon Unitary Sigma (g/kN)
0.08
Hydrocarbon Unitary Range (g/kN)
0-0.17
Hydrocarbon Unitary Characteristic (g/kN)
0.1
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
0.5
Hydrocarbon LTO (g)
24.81
Carbon Monoxide Take Off (g/kg fuel)
0.48
Carbon Monoxide Climb Out (g/kg fuel)
0.43
Carbon Monoxide Approach (g/kg fuel)
0.89
Carbon Monoxide Idle (g/kg fuel)
9.82
Carbon Monoxide Unitary Average (g/kN)
13.35
Carbon Monoxide Unitary SD (g/kN)
3.36
Carbon Monoxide Unitary Range (g/kN)
9.37-17.18
Carbon Monoxide Unitary Characteristic (g/kN)
14.28
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
12.1
NOx Take Off (g/kg fuel)
40.46
NOx Climb Out (g/kg fuel)
31.49
NOx Approach (g/kg fuel)
12.56
NOx Idle (g/kg fuel)
5.21
NOx Unitary Average (g/kN)
49.8
NOx Unitary SD (g/kN)
0.77
NOx Unitary Range (g/kN)
49.13-50.61
NOx Unitary Characteristic (g/kN)
52.34
NOx Unitaryto Standard (% of limit)
44.72
NOx Unitaryto CAEP2 (% of limit)
55.9
NOx Unitaryto CAEP4 (% of limit)
62.28
NOx Unitaryto CAEP6 (% of limit)
68.86
NOx Unitaryto CAEP8 (% of limit)
77.93
NOx LTO (g)
14299
Smoke Take Off (SN)
3.8
Smoke Climb Out (SN)
4.8
Smoke Approach (SN)
3.3
Smoke Idle (SN)
0.5
Smoke Max (SN)
5.98
Smoke Sigma (SN)
2.26
Smoke Range (SN)
3-8.3
Smoke Characteristic (SN)
6.5
Smoke Characteristicto Regulatory (% of limit)
36.64
Fuel Flow Take Off (kg/s)
2.075
Fuel Flow Climbout (kg/s)
1.715
Fuel Flow Approach (kg/s)
0.582
Fuel Flow Idle (kg/s)
0.233
Fuel LTO (kg)
817
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
3832
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)