Trent 1000-E

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

268 kN

Bypass Ratio

9.74

Overall Pressure Ratio

36.19

Fuel Flow Take Off

1.907 kg/s

NOx Unitaryto CAEP8

76.32 % 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 9.74	Overall Pressure Ratio 36.19	Afterburner No

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Similar reaction turbines

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
Trent 1000-E2	Rolls-Royce	268	9.62	36.32	Compare
GEnx-1B58/P2	General Electric Company	271.3415	9.3341	37.3864	Compare
GEnx-1B58	GE Aircraft Engines	271.3	9.2	37.2	Compare
GEnx-1B58/P1	GE Aircraft Engines	271.3	9.2	37.1	Compare
Trent 1000-E	Rolls-Royce	279.8	9.67	37.51	Compare
GEnx-1B54/P2	General Electric Company	255.3279	9.4917	35.4096	Compare

All data (65 fields)

Name: Trent 1000-E
EASA ID: 12RR058
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Geared Fan: No
Combustion Chamber: Phase5 Tiled
Afterburner: No
Streams: 2
Bypass Ratio: 9.74
Overall Pressure Ratio: 36.19
Maximum Takeoff Thrust (kN): 268
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): 0.1
Hydrocarbon Unitary Average (g/kN): 0.13
Hydrocarbon Unitary Sigma (g/kN): 0.11
Hydrocarbon Unitary Range (g/kN): 0-0.25
Hydrocarbon Unitary Characteristic (g/kN): 0.14
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 0.73
Hydrocarbon LTO (g): 33.59
Carbon Monoxide Take Off (g/kg fuel): 0.46
Carbon Monoxide Climb Out (g/kg fuel): 0.42
Carbon Monoxide Approach (g/kg fuel): 0.99
Carbon Monoxide Idle (g/kg fuel): 11.2
Carbon Monoxide Unitary Average (g/kN): 15.08
Carbon Monoxide Unitary SD (g/kN): 3.64
Carbon Monoxide Unitary Range (g/kN): 10.79-19.28
Carbon Monoxide Unitary Characteristic (g/kN): 16.13
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 13.67
NOx Take Off (g/kg fuel): 36.29
NOx Climb Out (g/kg fuel): 28.62
NOx Approach (g/kg fuel): 12.16
NOx Idle (g/kg fuel): 5
NOx Unitary Average (g/kN): 45.39
NOx Unitary SD (g/kN): 0.64
NOx Unitary Range (g/kN): 44.82-46.14
NOx Unitary Characteristic (g/kN): 47.7
NOx Unitaryto Standard (% of limit): 42.45
NOx Unitaryto CAEP2 (% of limit): 53.06
NOx Unitaryto CAEP4 (% of limit): 60.09
NOx Unitaryto CAEP6 (% of limit): 66.87
NOx Unitaryto CAEP8 (% of limit): 76.32
NOx LTO (g): 12165
Smoke Take Off (SN): 4.2
Smoke Climb Out (SN): 5.2
Smoke Approach (SN): 3.1
Smoke Idle (SN): 0.6
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): 35.95
Fuel Flow Take Off (kg/s): 1.907
Fuel Flow Climbout (kg/s): 1.579
Fuel Flow Approach (kg/s): 0.549
Fuel Flow Idle (kg/s): 0.217
Fuel LTO (kg): 758
Fuel Venting Compliant: Yes
Carbon Monoxide LTO (g): 4041
Emissions Data Status: C/R
Emissions Data Superseded: Yes
Emissions Superseded By: 12RR064
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 e)