BR700-710A1-10

Turbofan · Rolls-Royce Deutschland
Reaction Turbines
Maximum Takeoff Thrust
65.61 kN
Bypass Ratio
4.2
Overall Pressure Ratio
24.23
Fuel Flow Take Off
0.713 kg/s
NOx Unitaryto CAEP8
95.8 % 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 4.2 Overall Pressure Ratio 24.23 Afterburner No

Pictures

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Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
BR700-710A1-10 Rolls-Royce Deutschland 65.61 4.2 24.31 Compare
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All data (58 fields)
Name
BR700-710A1-10
EASA ID
4BR008
Aircraft Engine Manufacturer
Rolls-Royce Deutschland
Aircraft Engine Type
Turbofan
Fuel
AVTUR
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
4.2
Overall Pressure Ratio
24.23
Maximum Takeoff Thrust (kN)
65.61
Hydrocarbon Take Off (g/kg fuel)
0.02
Hydrocarbon Climb Out (g/kg fuel)
0.02
Hydrocarbon Approach (g/kg fuel)
0.05
Hydrocarbon Idle (g/kg fuel)
1.09
Hydrocarbon Unitary Average (g/kN)
2.37
Hydrocarbon Unitary Range (g/kN)
2.13-2.63
Hydrocarbon Unitary Characteristic (g/kN)
3.7
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
18.6
Hydrocarbon LTO (g)
156
Carbon Monoxide Take Off (g/kg fuel)
1.04
Carbon Monoxide Climb Out (g/kg fuel)
0.93
Carbon Monoxide Approach (g/kg fuel)
4.78
Carbon Monoxide Idle (g/kg fuel)
27.82
Carbon Monoxide Unitary Average (g/kN)
64.26
Carbon Monoxide Unitary Range (g/kN)
63.75-65.02
Carbon Monoxide Unitary Characteristic (g/kN)
78.9
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
66.8
NOx Take Off (g/kg fuel)
18.79
NOx Climb Out (g/kg fuel)
15.07
NOx Approach (g/kg fuel)
7.68
NOx Idle (g/kg fuel)
4.69
NOx Unitary Average (g/kN)
42.52
NOx Unitary Range (g/kN)
41.84-42.94
NOx Unitary Characteristic (g/kN)
49.3
NOx Unitaryto Standard (% of limit)
55.7
NOx Unitaryto CAEP2 (% of limit)
69.7
NOx Unitaryto CAEP4 (% of limit)
78.6
NOx Unitaryto CAEP6 (% of limit)
84.5
NOx Unitaryto CAEP8 (% of limit)
95.8
NOx LTO (g)
2790
Smoke Take Off (SN)
13.99
Smoke Climb Out (SN)
11.92
Smoke Approach (SN)
0.29
Smoke Idle (SN)
0.56
Smoke Max (SN)
13.99
Smoke Range (SN)
12.64-15.18
Smoke Characteristic (SN)
18
Smoke Characteristicto Regulatory (% of limit)
67.8
Fuel Flow Take Off (kg/s)
0.713
Fuel Flow Climbout (kg/s)
0.594
Fuel Flow Approach (kg/s)
0.214
Fuel Flow Idle (kg/s)
0.089
Fuel LTO (kg)
299
Carbon Monoxide LTO (g)
4212
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)