BR700-730B2-14

Maximum Takeoff Thrust
81.65 kN
Bypass Ratio
5.377
Overall Pressure Ratio
35.533
Fuel Flow Take Off
0.7865 kg/s
NOx Unitaryto CAEP8
80.91 % 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 Advanced Rich Burn
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 5.377 Overall Pressure Ratio 35.533 Afterburner No

Pictures

No pictures yet for this family.

Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
CF34-10A18 GE Aircraft Engines 82.1 5.4 26.5 Compare
CFM56-3C-1 (Rerated) CFM56-3 CFM International 82.29 5.1 21.3 Compare
CF34-10E5A1 GE Aircraft Engines 83.7 5.09 27.3 Compare
CF34-10E6A1 GE Aircraft Engines 83.7 5.09 27.3 Compare
CF34-10E7 GE Aircraft Engines 83.7 5.09 27.3 Compare
CF34-10E7-B GE Aircraft Engines 83.7 5.09 27.2 Compare
All data (81 fields)
Name
BR700-730B2-14
EASA ID
06P26RR149
Aircraft Engine Manufacturer
Rolls-Royce Deutschland
Aircraft Engine Type
Turbofan
Geared Fan
No
Combustion Chamber
Advanced Rich Burn
Afterburner
No
Streams
2
Bypass Ratio
5.377
Overall Pressure Ratio
35.533
Maximum Takeoff Thrust (kN)
81.65
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)
0.277
Hydrocarbon Unitary Average (g/kN)
0.428
Hydrocarbon Unitary Sigma (g/kN)
0.101
Hydrocarbon Unitary Range (g/kN)
0.36-0.5
Hydrocarbon Unitary Characteristic (g/kN)
0.557
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
2.842
Hydrocarbon LTO (g)
34.96
Carbon Monoxide Take Off (g/kg fuel)
0.4056
Carbon Monoxide Climb Out (g/kg fuel)
0.468
Carbon Monoxide Approach (g/kg fuel)
2.438
Carbon Monoxide Idle (g/kg fuel)
22.216
Carbon Monoxide Unitary Average (g/kN)
36.519
Carbon Monoxide Unitary SD (g/kN)
0.9906
Carbon Monoxide Unitary Range (g/kN)
35.82-37.22
Carbon Monoxide Unitary Characteristic (g/kN)
41.6079
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
35.2609
NOx Take Off (g/kg fuel)
30.392
NOx Climb Out (g/kg fuel)
22.542
NOx Approach (g/kg fuel)
9.766
NOx Idle (g/kg fuel)
3.338
NOx Unitary Average (g/kN)
47.1027
NOx Unitary SD (g/kN)
1.518
NOx Unitary Range (g/kN)
46.03-48.18
NOx Unitary Characteristic (g/kN)
51.7953
NOx Unitaryto Standard (% of limit)
46.63
NOx Unitaryto CAEP2 (% of limit)
58.29
NOx Unitaryto CAEP4 (% of limit)
65.288
NOx Unitaryto CAEP6 (% of limit)
71.689
NOx Unitaryto CAEP8 (% of limit)
80.91
NOx LTO (g)
3846.03
Smoke Take Off (SN)
1.94
Smoke Climb Out (SN)
3.0904
Smoke Approach (SN)
2.25
Smoke Idle (SN)
1.161
Smoke Max (SN)
4.956
Smoke Sigma (SN)
0.256
Smoke Range (SN)
4.8-5.1
Smoke Characteristic (SN)
5.812
Smoke Characteristicto Regulatory (% of limit)
23.227
Fuel Flow Take Off (kg/s)
0.7865
Fuel Flow Climbout (kg/s)
0.646
Fuel Flow Approach (kg/s)
0.2126
Fuel Flow Idle (kg/s)
0.0809
Fuel LTO (kg)
295.56
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
2981.87
Emissions Data Status
C
NOx Compliance Demonstration
2.3.2 e)
nvPME Imass Approach (mg/kg)
76.4
nvPME Imass Climb Out (mg/kg)
95.02
nvPME Imass Idle (mg/kg)
38
nvPME Imass Max (mg/kg)
170.7
nvPME Imass Take Off (mg/kg)
51.21
nvPME Inum Approach (#/kg)
1980000000000000
nvPME Inum Climb Out (#/kg)
718000000000000
nvPME Inum Idle (#/kg)
1180000000000000
nvPME Inum Max (#/kg)
2640000000000000
nvPME Inum Take Off (#/kg)
296000000000000
nvPMLTO Mass (mg)
18491.08
nvPMLTO Mass Per Thrust (mg/kN)
277.9
nvPMLTO Mass To CAEP11 (% of limit)
40.48
nvPMLTO Number (#)
321000000000000000
nvPMLTO Number Per Thrust (#/kN)
4830000000000000
nvPMLTO Number To CAEP11 (% of limit)
58.19
nvPM Mass Concentration Characteristic (mg/m³)
558.06
nvPM Mass Concentration Max (mg/m³)
475.86
nvPM Mass Concentration To CAEP10 (% of limit)
7.56