Trent 1000-H

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

287.1 kN

Bypass Ratio

9.62

Overall Pressure Ratio

38.33

Fuel Flow Take Off

2.07 kg/s

NOx Unitaryto CAEP8

78.08 % 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 9.62	Overall Pressure Ratio 38.33	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	286.7	9.62	38.33	Compare
Trent 1000-H2	Rolls-Royce	287.1	9.49	38.52	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
Trent 1000-E2	Rolls-Royce	268	9.62	36.32	Compare

All data (65 fields)

Name: Trent 1000-H
EASA ID: 12RR060
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Geared Fan: No
Combustion Chamber: Phase5 Tiled
Afterburner: No
Streams: 2
Bypass Ratio: 9.62
Overall Pressure Ratio: 38.33
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): 0.08
Hydrocarbon Unitary Sigma (g/kN): 0.08
Hydrocarbon Unitary Range (g/kN): 0-0.16
Hydrocarbon Unitary Characteristic (g/kN): 0.1
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 0.49
Hydrocarbon LTO (g): 24.15
Carbon Monoxide Take Off (g/kg fuel): 0.49
Carbon Monoxide Climb Out (g/kg fuel): 0.43
Carbon Monoxide Approach (g/kg fuel): 0.87
Carbon Monoxide Idle (g/kg fuel): 9.8
Carbon Monoxide Unitary Average (g/kN): 12.94
Carbon Monoxide Unitary SD (g/kN): 3.25
Carbon Monoxide Unitary Range (g/kN): 9.08-16.65
Carbon Monoxide Unitary Characteristic (g/kN): 13.84
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 11.73
NOx Take Off (g/kg fuel): 40.54
NOx Climb Out (g/kg fuel): 31.54
NOx Approach (g/kg fuel): 12.62
NOx Idle (g/kg fuel): 5.21
NOx Unitary Average (g/kN): 49.62
NOx Unitary SD (g/kN): 0.79
NOx Unitary Range (g/kN): 48.94-50.45
NOx Unitary Characteristic (g/kN): 52.14
NOx Unitaryto Standard (% of limit): 44.7
NOx Unitaryto CAEP2 (% of limit): 55.87
NOx Unitaryto CAEP4 (% of limit): 62.32
NOx Unitaryto CAEP6 (% of limit): 68.95
NOx Unitaryto CAEP8 (% of limit): 78.08
NOx LTO (g): 14247
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): 2.07
Fuel Flow Climbout (kg/s): 1.71
Fuel Flow Approach (kg/s): 0.583
Fuel Flow Idle (kg/s): 0.226
Fuel LTO (kg): 805
Fuel Venting Compliant: Yes
Carbon Monoxide LTO (g): 3714
Emissions Data Status: C/R
Emissions Data Superseded: Yes
Emissions Superseded By: 12RR066
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 e)