DSC05589

RB211-535E4B

Maximum Takeoff Thrust
191.73 kN
Bypass Ratio
4.1
Overall Pressure Ratio
27.65
Fuel Flow Take Off
2.08 kg/s
NOx Unitaryto CAEP8
190.6 % 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 —
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 4.1 Overall Pressure Ratio 27.65 Afterburner No

Pictures

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
RB211-535E4B Rolls-Royce 191.7 4.1 27.9 Compare
RB211-535E4 Rolls-Royce 178.4 4.1 25.8 Compare
CF6-45A GE Aircraft Engines 202.8 4.3 25.38 Compare
CF6-45A2 GE Aircraft Engines 202.8 4.3 25.9 Compare
General Electric TF39 General Electric Company 193 Compare
RB211-22B Rolls-Royce 182.5 4.7 25 Compare
All data (58 fields)
Name
RB211-535E4B
EASA ID
3RR034
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Fuel
AVTUR
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
4.1
Overall Pressure Ratio
27.65
Maximum Takeoff Thrust (kN)
191.73
Hydrocarbon Take Off (g/kg fuel)
0.01
Hydrocarbon Climb Out (g/kg fuel)
0
Hydrocarbon Approach (g/kg fuel)
0.03
Hydrocarbon Idle (g/kg fuel)
0.28
Hydrocarbon Unitary Average (g/kN)
0.45
Hydrocarbon Unitary Range (g/kN)
0.41-0.49
Hydrocarbon Unitary Characteristic (g/kN)
0.7
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
3.6
Hydrocarbon LTO (g)
88
Carbon Monoxide Take Off (g/kg fuel)
0.94
Carbon Monoxide Climb Out (g/kg fuel)
0.6
Carbon Monoxide Approach (g/kg fuel)
1.05
Carbon Monoxide Idle (g/kg fuel)
11.76
Carbon Monoxide Unitary Average (g/kN)
19.67
Carbon Monoxide Unitary Range (g/kN)
19.35-19.92
Carbon Monoxide Unitary Characteristic (g/kN)
24.1
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
20.5
NOx Take Off (g/kg fuel)
54.46
NOx Climb Out (g/kg fuel)
36.82
NOx Approach (g/kg fuel)
7.35
NOx Idle (g/kg fuel)
3.52
NOx Unitary Average (g/kN)
76.97
NOx Unitary Range (g/kN)
75.9-77.9
NOx Unitary Characteristic (g/kN)
89.2
NOx Unitaryto Standard (% of limit)
93.6
NOx Unitaryto CAEP2 (% of limit)
117
NOx Unitaryto CAEP4 (% of limit)
141
NOx Unitaryto CAEP6 (% of limit)
160.3
NOx Unitaryto CAEP8 (% of limit)
190.6
NOx LTO (g)
14791
Smoke Take Off (SN)
1.73
Smoke Climb Out (SN)
1.84
Smoke Approach (SN)
0.96
Smoke Idle (SN)
0.5
Smoke Max (SN)
1.84
Smoke Range (SN)
1.5-2.2
Smoke Characteristic (SN)
2.4
Smoke Characteristicto Regulatory (% of limit)
12.1
Fuel Flow Take Off (kg/s)
2.08
Fuel Flow Climbout (kg/s)
1.65
Fuel Flow Approach (kg/s)
0.55
Fuel Flow Idle (kg/s)
0.19
Fuel LTO (kg)
734
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
3837
Emissions Data Status
R
Engine Status
Out of production