P70810-182103

CFM56-7B24E

Turbofan · Family: CFM56-7B · CFM International
Maximum Takeoff Thrust
107.6 kN
Bypass Ratio
5.3
Overall Pressure Ratio
25.6
Diameter
1549 mm
Length
2507 mm
Dry Weight
2366 kg
Fuel Flow Take Off
1.086 kg/s
NOx Unitaryto CAEP8
89.5 % of limit

Architecture

Fan Fan Stages — Fan Blades 24 Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages 3 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 9 High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber Tech Insertion
HP turbine High Pressure Compressor Stages 1 High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages 4 Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 5.3 Overall Pressure Ratio 25.6 Afterburner No

Pictures

CFM56-7B

Name Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio Fuel Flow Take Off (kg/s) NOx LTO (g) NOx Unitaryto CAEP8 (% of limit) Smoke Max (SN) EASA ID
CFM56-7B18/3 86.7 5.5 21.4 0.842 2729 85.5 8.04 8CM061
CFM56-7B18 86.74 5.5 21.59 0.854 3472 118.4 10.7 3CM029
CFM56-7B20/3 91.6 5.5 22.4 0.896 2987 87.5 8.66 8CM062
CFM56-7B20E 91.6 5.5 22.4 0.896 2987 87.5 8.66 01P11CM111
CFM56-7B20 91.63 5.4 22.61 0.913 3829 122.1 11.4 3CM030
CFM56-7B20/2 91.63 5.4 22.77 0.903 2802 81.1 1.52 4CM039
CFM56-7B22 100.97 5.3 24.41 1.021 4560 124 12 3CM031
CFM56-7B22/2 100.97 5.3 24.61 1.008 3091 76.2 0.69 4CM040
CFM56-7B22/3 101 5.3 24.2 1.004 3540 88.4 9.84 8CM063
CFM56-7B22E 101 5.3 24.2 1.004 3538 88.4 9.84 01P11CM112
CFM56-7B22E/B1 101 5.3 24.2 1.004 3538 88.4 9.84 01P11CM113
CFM56-7B24/3 107.6 5.3 25.6 1.086 3995 89.5 12.07 8CM064
CFM56-7B24E 107.6 5.3 25.6 1.086 3996 89.5 12.07 01P11CM114
CFM56-7B24E/B1 107.6 5.3 25.6 1.086 3996 89.5 12.07 01P11CM115
CFM56-7B24 107.65 5.2 25.78 1.103 5149 125.4 12.6 3CM032
CFM56-7B24/2 107.65 5.2 25.95 1.089 3534 78.4 0.65 4CM041
CFM56-7B26 116.99 5.1 27.61 1.221 6149 130.5 14.7 8CM051
CFM56-7B26/2 116.99 5.1 27.8 1.203 4233 81.7 0.71 4CM042
CFM56-7B26/3 117 5.1 27.7 1.213 4763 91.9 13.07 8CM065
CFM56-7B26/3 (Research Measurement) 117 5.1 27.7 1.213 4923 104 01P22FC001
CFM56-7B26E 117 5.1 27.7 1.213 4762 91.9 13.07 01P11CM116
CFM56-7B26E/B1 117 5.1 27.7 1.213 4762 91.9 13.07 01P11CM117
CFM56-7B26E/B2 117 5.1 27.7 1.213 4762 91.9 13.07 01P11CM118
CFM56-7B26E/B2F 117 5.1 27.7 1.213 4762 91.9 13.07 01P11CM120
CFM56-7B26E/F 117 5.1 27.7 1.213 4762 91.9 13.07 01P11CM119
CFM56-7B27/3 121.4 5.1 29 1.293 5232 93.6 13.38 8CM066
CFM56-7B27AE 121.4 5.1 29 1.293 5231 93.6 13.38 01P11CM124
CFM56-7B27E 121.4 5.1 29 1.293 5231 93.6 13.38 01P11CM121
CFM56-7B27E/B1 121.4 5.1 29 1.293 5231 93.6 13.38 01P11CM122
CFM56-7B27E/B1F 121.4 5.1 29 1.293 5231 93.6 13.38 01P11CM126
CFM56-7B27E/B3 121.4 5.1 29 1.293 5231 93.6 13.38 01P11CM123
CFM56-7B27E/F 121.4 5.1 29 1.293 5231 93.6 13.38 01P11CM125
CFM56-7B27 121.44 5 28.63 1.284 6719 133 15.7 3CM034
CFM56-7B27/2 121.44 5 28.84 1.265 4648 83.5 0.75 4CM043

Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
V2500-A1 International Aero Engines 111.2 5.3 29.8 Compare
CFM56-3C-1 CFM56-3 CFM International 104.6 5.1 25.5 Compare
V2524-A5 SelectOne™ Upgrade Package International Aero Engines 108.9 4.8 27 Compare
V2524-A5 International Aero Engines 109.06 4.81 26.9 Compare
PW6124A Pratt & Whitney 105.87 4.8 28 Compare
CFM56-5B6/2 CFM56-5B CFM International 104.5 5.7 24.8 Compare
All data (97 fields)
Name
CFM56-7B24E
Family
CFM56-7B
EASA ID
01P11CM114
Aircraft Engine Manufacturer
CFM International
Aircraft Engine Type
Turbofan
Comment
Boeing 737 Next Generation
Dry Weight (kg)
2366
Diameter (mm)
1549
Max Rotating Diameter (mm)
1549
Length (mm)
2507
Wikipedia Article (URL)
en.wikipedia.org/wiki/CFM_International_CFM56
Fuel
Jet A
Fan Blades
24
Geared Fan
No
Low-Pressure Compressor Stages
3
High-Pressure Compressor Stages
9
Combustion Chamber
Tech Insertion
High Pressure Compressor Stages
1
Low-Pressure Turbine Stages
4
Afterburner
No
Streams
2
Bypass Ratio
5.3
Overall Pressure Ratio
25.6
Maximum Takeoff Thrust (kN)
107.6
Hydrocarbon Take Off (g/kg fuel)
0.02
Hydrocarbon Climb Out (g/kg fuel)
0.03
Hydrocarbon Approach (g/kg fuel)
0.06
Hydrocarbon Idle (g/kg fuel)
2.3
Hydrocarbon Unitary Average (g/kN)
3.51
Hydrocarbon Unitary Sigma (g/kN)
0.45
Hydrocarbon Unitary Range (g/kN)
3.01-3.88
Hydrocarbon Unitary Characteristic (g/kN)
4.09
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
20.9
Hydrocarbon LTO (g)
377
Carbon Monoxide Take Off (g/kg fuel)
0.18
Carbon Monoxide Climb Out (g/kg fuel)
0.15
Carbon Monoxide Approach (g/kg fuel)
3.68
Carbon Monoxide Idle (g/kg fuel)
34.71
Carbon Monoxide Unitary Average (g/kN)
54.38
Carbon Monoxide Unitary SD (g/kN)
2.8
Carbon Monoxide Unitary Range (g/kN)
51.2-56.4
Carbon Monoxide Unitary Characteristic (g/kN)
58.8
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
49.8
NOx Take Off (g/kg fuel)
18.93
NOx Climb Out (g/kg fuel)
15.6
NOx Approach (g/kg fuel)
8.6
NOx Idle (g/kg fuel)
4.09
NOx Unitary Average (g/kN)
37.11
NOx Unitary SD (g/kN)
1.2
NOx Unitary Range (g/kN)
36.1-38.5
NOx Unitary Characteristic (g/kN)
39.3
NOx Unitaryto Standard (% of limit)
43.1
NOx Unitaryto CAEP2 (% of limit)
53.9
NOx Unitaryto CAEP4 (% of limit)
65.5
NOx Unitaryto CAEP6 (% of limit)
74.5
NOx Unitaryto CAEP8 (% of limit)
89.5
NOx LTO (g)
3996
Smoke Take Off (SN)
12.1
Smoke Climb Out (SN)
8.7
Smoke Approach (SN)
2.1
Smoke Idle (SN)
2.1
Smoke Max (SN)
12.07
Smoke Sigma (SN)
3.4
Smoke Range (SN)
8.3-14.7
Smoke Characteristic (SN)
13.28
Smoke Characteristicto Regulatory (% of limit)
57.2
Fuel Flow Take Off (kg/s)
1.086
Fuel Flow Climbout (kg/s)
0.895
Fuel Flow Approach (kg/s)
0.308
Fuel Flow Idle (kg/s)
0.103
Fuel LTO (kg)
398
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
5854
Compressor Description
1 fan, 3-stage LP, 9-stage HP
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)
nvPME Imass Approach (mg/kg)
1.29
nvPME Imass Climb Out (mg/kg)
33.6
nvPME Imass Idle (mg/kg)
0.8
nvPME Imass Max (mg/kg)
48.6
nvPME Imass Take Off (mg/kg)
48.6
nvPME Inum Approach (#/kg)
54600000000000
nvPME Inum Climb Out (#/kg)
424000000000000
nvPME Inum Idle (#/kg)
36900000000000
nvPME Inum Max (#/kg)
431000000000000
nvPME Inum Take Off (#/kg)
428000000000000
nvPMLTO Mass (mg)
6408
nvPMLTO Mass Per Thrust (mg/kN)
82.8
nvPMLTO Mass To CAEP11 (% of limit)
16.3
nvPMLTO Number (#)
79500000000000000
nvPMLTO Number Per Thrust (#/kN)
1030000000000000
nvPMLTO Number To CAEP11 (% of limit)
16.6
nvPM Mass Concentration Characteristic (mg/m³)
1434
nvPM Mass Concentration Max (mg/m³)
1114
nvPM Mass Concentration To CAEP10 (% of limit)
22.5
Turbine Description
1-stage HP, 4-stage LP