LEAP-1C28

Turbofan · Family: LEAP-1C · CFM International
Maximum Takeoff Thrust
129.9763 kN
Bypass Ratio
10.5594
Overall Pressure Ratio
35.4641
Diameter
1956 mm
Length
4505 mm
Full Weight
3935 kg
Fuel Flow Take Off
0.9469 kg/s
NOx Unitaryto CAEP8
79.7 % of limit

Architecture

Fan Fan Stages — Fan Blades 18 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 TAPS II
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 10.5594 Overall Pressure Ratio 35.4641 Afterburner No

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LEAP-1C

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
LEAP-1C28 129.9763 10.5594 35.4641 0.9469 6021.709 79.7 1.203 08P28CM150
LEAP-1C30/30B1 137.1379 10.4525 37.1195 1.0105 7395.37 88.1 1.203 08P28CM149

Similar reaction turbines

Name Family Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
LEAP-1A29CJ LEAP-1A CFM International 130.2891 10.5579 35.4206 Compare
PW1129G-JM Pratt & Whitney 130.08 12 34.02 Compare
PW1130G-JM Pratt & Whitney 134 11.7 35.52 Compare
PW1428GH-JM Pratt & Whitney 132.3829 12.102 33.32 Compare
PW1428GA-JM Pratt & Whitney 132.3829 12.102 33.32 Compare
PW1428G-JM Pratt & Whitney 132.3829 12.102 33.32 Compare
All data (92 fields)
Name
LEAP-1C28
Family
LEAP-1C
EASA ID
08P28CM150
Aircraft Engine Manufacturer
CFM International
Aircraft Engine Type
Turbofan
Comment
COMAC C919
Full Weight (kg)
3935
Diameter (mm)
1956
Max Rotating Diameter (mm)
1956
Length (mm)
4505
Height (mm)
2714
Width (mm)
2659
Wikipedia Article (URL)
en.wikipedia.org/wiki/CFM_International_LEAP
Fuel
JET-A1
Fan Blades
18
Geared Fan
No
Combustion Chamber
TAPS II
Afterburner
No
Streams
2
Bypass Ratio
10.5594
Overall Pressure Ratio
35.4641
Maximum Takeoff Thrust (kN)
129.9763
Hydrocarbon Take Off (g/kg fuel)
0.0302
Hydrocarbon Climb Out (g/kg fuel)
0.0216
Hydrocarbon Approach (g/kg fuel)
0.0538
Hydrocarbon Idle (g/kg fuel)
0.7118
Hydrocarbon Unitary Average (g/kN)
0.8473
Hydrocarbon Unitary Sigma (g/kN)
0.2
Hydrocarbon Unitary Range (g/kN)
0.5-1.1
Hydrocarbon Unitary Characteristic (g/kN)
0.9667
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
4.9324
Hydrocarbon LTO (g)
110.1235
Carbon Monoxide Take Off (g/kg fuel)
0.015
Carbon Monoxide Climb Out (g/kg fuel)
0.0272
Carbon Monoxide Approach (g/kg fuel)
2.3921
Carbon Monoxide Idle (g/kg fuel)
22.9132
Carbon Monoxide Unitary Average (g/kN)
26.7754
Carbon Monoxide Unitary SD (g/kN)
1.3
Carbon Monoxide Unitary Range (g/kN)
25.4-28.9
Carbon Monoxide Unitary Characteristic (g/kN)
28.646
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
24.2763
NOx Take Off (g/kg fuel)
49.7393
NOx Climb Out (g/kg fuel)
27.6964
NOx Approach (g/kg fuel)
9.007
NOx Idle (g/kg fuel)
4.4009
NOx Unitary Average (g/kN)
46.3293
NOx Unitary SD (g/kN)
2.1
NOx Unitary Range (g/kN)
43.4-49.2
NOx Unitary Characteristic (g/kN)
48.6857
NOx Unitaryto Standard (% of limit)
43.9
NOx Unitaryto CAEP2 (% of limit)
54.9
NOx Unitaryto CAEP4 (% of limit)
62.5
NOx Unitaryto CAEP6 (% of limit)
69.7
NOx Unitaryto CAEP8 (% of limit)
79.7
NOx LTO (g)
6021.709
Smoke Take Off (SN)
0.7381
Smoke Climb Out (SN)
0.679
Smoke Approach (SN)
0.5723
Smoke Idle (SN)
0.6056
Smoke Max (SN)
1.203
Smoke Sigma (SN)
0.3
Smoke Range (SN)
0.8-1.4
Smoke Characteristic (SN)
0.9501
Smoke Characteristicto Regulatory (% of limit)
4.3126
Fuel Flow Take Off (kg/s)
0.9469
Fuel Flow Climbout (kg/s)
0.7763
Fuel Flow Approach (kg/s)
0.2622
Fuel Flow Idle (kg/s)
0.0931
Fuel LTO (kg)
350.3275
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
3480.171
Emissions Data Status
R
NOx Compliance Demonstration
2.3.2 e)
nvPME Imass Approach (mg/kg)
1.9598
nvPME Imass Climb Out (mg/kg)
0.6641
nvPME Imass Idle (mg/kg)
1.4703
nvPME Imass Max (mg/kg)
12.5543
nvPME Imass Take Off (mg/kg)
0.6349
nvPME Inum Approach (#/kg)
73179670000000
nvPME Inum Climb Out (#/kg)
12307560000
nvPME Inum Idle (#/kg)
22930490000000
nvPME Inum Max (#/kg)
451258300000000
nvPME Inum Take Off (#/kg)
14703810000
nvPMLTO Mass (mg)
430.0589
nvPMLTO Mass Per Thrust (mg/kN)
3.6719
nvPMLTO Mass To CAEP11 (% of limit)
1.0418
nvPMLTO Number (#)
7935101000000000
nvPMLTO Number Per Thrust (#/kN)
67750950000000
nvPMLTO Number To CAEP11 (% of limit)
1.5405
nvPM Mass Concentration Characteristic (mg/m³)
165.986
nvPM Mass Concentration Max (mg/m³)
152.9229
nvPM Mass Concentration To CAEP10 (% of limit)
2.8568