BR700-710A1-10

Turbofan · Rolls-Royce Deutschland
Reaction Turbines
Maximum Takeoff Thrust
65.61 kN
Bypass Ratio
4.2
Overall Pressure Ratio
24.31
Fuel Flow Take Off
0.707 kg/s
NOx Unitaryto CAEP8
88.4 % 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 24.31 Afterburner No

Pictures

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All data (58 fields)
Name
BR700-710A1-10
EASA ID
3BR001
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
24.31
Maximum Takeoff Thrust (kN)
65.61
Hydrocarbon Take Off (g/kg fuel)
0
Hydrocarbon Climb Out (g/kg fuel)
0.03
Hydrocarbon Approach (g/kg fuel)
0.04
Hydrocarbon Idle (g/kg fuel)
1.98
Hydrocarbon Unitary Average (g/kN)
4.29
Hydrocarbon Unitary Range (g/kN)
3.83-5.03
Hydrocarbon Unitary Characteristic (g/kN)
6.6
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
33.7
Hydrocarbon LTO (g)
279
Carbon Monoxide Take Off (g/kg fuel)
0.52
Carbon Monoxide Climb Out (g/kg fuel)
0.66
Carbon Monoxide Approach (g/kg fuel)
4.24
Carbon Monoxide Idle (g/kg fuel)
26.09
Carbon Monoxide Unitary Average (g/kN)
59.85
Carbon Monoxide Unitary Range (g/kN)
57.89-63.69
Carbon Monoxide Unitary Characteristic (g/kN)
73.5
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
62.3
NOx Take Off (g/kg fuel)
17.07
NOx Climb Out (g/kg fuel)
13.93
NOx Approach (g/kg fuel)
8.2
NOx Idle (g/kg fuel)
4
NOx Unitary Average (g/kN)
39.32
NOx Unitary Range (g/kN)
38.09-40.51
NOx Unitary Characteristic (g/kN)
45.6
NOx Unitaryto Standard (% of limit)
51.5
NOx Unitaryto CAEP2 (% of limit)
64.3
NOx Unitaryto CAEP4 (% of limit)
72.6
NOx Unitaryto CAEP6 (% of limit)
78
NOx Unitaryto CAEP8 (% of limit)
88.4
NOx LTO (g)
2576
Smoke Take Off (SN)
11.03
Smoke Climb Out (SN)
8.69
Smoke Approach (SN)
0
Smoke Idle (SN)
0.17
Smoke Max (SN)
11.03
Smoke Range (SN)
10.18-11.87
Smoke Characteristic (SN)
14.2
Smoke Characteristicto Regulatory (% of limit)
53.4
Fuel Flow Take Off (kg/s)
0.707
Fuel Flow Climbout (kg/s)
0.588
Fuel Flow Approach (kg/s)
0.22
Fuel Flow Idle (kg/s)
0.089
Fuel LTO (kg)
299
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
3913
Emissions Data Status
C
Engine Status
Out of production