BR700-715C1-30

Turbofan · Rolls-Royce Deutschland
Reaction Turbines
Maximum Takeoff Thrust
95.33 kN
Bypass Ratio
4.54
Overall Pressure Ratio
32.15
Fuel Flow Take Off
0.984 kg/s
NOx Unitaryto CAEP8
102.5 % 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 Improved fuel injector
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 4.54 Overall Pressure Ratio 32.15 Afterburner No

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Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
BR700-715C1-30 Rolls-Royce Deutschland 95.33 4.55 32.01 Compare
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BR700-715B1-30 Rolls-Royce Deutschland 89.68 4.6 30.47 Compare
CFM56-3B-2 CFM56-3 CFM International 98.3 5.1 24.1 Compare
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All data (58 fields)
Name
BR700-715C1-30
EASA ID
4BR007
Aircraft Engine Manufacturer
Rolls-Royce Deutschland
Aircraft Engine Type
Turbofan
Fuel
AVTUR
Geared Fan
No
Combustion Chamber
Improved fuel injector
Afterburner
No
Streams
2
Bypass Ratio
4.54
Overall Pressure Ratio
32.15
Maximum Takeoff Thrust (kN)
95.33
Hydrocarbon Take Off (g/kg fuel)
0.01
Hydrocarbon Climb Out (g/kg fuel)
0.06
Hydrocarbon Approach (g/kg fuel)
0.02
Hydrocarbon Idle (g/kg fuel)
0.06
Hydrocarbon Unitary Average (g/kN)
0.18
Hydrocarbon Unitary Range (g/kN)
0.02-0.34
Hydrocarbon Unitary Characteristic (g/kN)
0.3
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
1.4
Hydrocarbon LTO (g)
18
Carbon Monoxide Take Off (g/kg fuel)
0.8
Carbon Monoxide Climb Out (g/kg fuel)
0.64
Carbon Monoxide Approach (g/kg fuel)
3.23
Carbon Monoxide Idle (g/kg fuel)
17.85
Carbon Monoxide Unitary Average (g/kN)
34.04
Carbon Monoxide Unitary Range (g/kN)
33.51-34.63
Carbon Monoxide Unitary Characteristic (g/kN)
41.8
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
35.4
NOx Take Off (g/kg fuel)
27.92
NOx Climb Out (g/kg fuel)
20.05
NOx Approach (g/kg fuel)
9.23
NOx Idle (g/kg fuel)
4.28
NOx Unitary Average (g/kN)
48.13
NOx Unitary Range (g/kN)
46.96-49.29
NOx Unitary Characteristic (g/kN)
55.8
NOx Unitaryto Standard (% of limit)
53.5
NOx Unitaryto CAEP2 (% of limit)
66.9
NOx Unitaryto CAEP4 (% of limit)
78.2
NOx Unitaryto CAEP6 (% of limit)
88.2
NOx Unitaryto CAEP8 (% of limit)
102.5
NOx LTO (g)
4588
Smoke Take Off (SN)
4.86
Smoke Climb Out (SN)
4.26
Smoke Approach (SN)
1.12
Smoke Idle (SN)
0.04
Smoke Max (SN)
4.86
Smoke Range (SN)
4.62-5.28
Smoke Characteristic (SN)
6.3
Smoke Characteristicto Regulatory (% of limit)
26.1
Fuel Flow Take Off (kg/s)
0.984
Fuel Flow Climbout (kg/s)
0.805
Fuel Flow Approach (kg/s)
0.272
Fuel Flow Idle (kg/s)
0.105
Fuel LTO (kg)
377
Carbon Monoxide LTO (g)
3236
Emissions Data Status
C
Engine Status
Out of production