PW1133G1-JM

Turbofan · Pratt & Whitney
Reaction Turbines
Maximum Takeoff Thrust
147.28 kN
Bypass Ratio
11.4
Overall Pressure Ratio
38.85
Fuel Flow Take Off
1.02297 kg/s
NOx Unitaryto CAEP8
56.48 % of limit

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan Yes 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 TALON X
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 11.4 Overall Pressure Ratio 38.85 Afterburner No

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
PW1133G-JM Pratt & Whitney 147.28 11.4 38.85 Compare
PW1130G-JM Pratt & Whitney 147.28 11.58 38.07 Compare
PW1133GA-JM Pratt & Whitney 147.28 11.58 38.07 Compare
PW1431GH-JM Pratt & Whitney 140.4386 11.8646 35.59 Compare
PW1431GA-JM Pratt & Whitney 140.4386 11.8646 35.59 Compare
PW1431G-JM Pratt & Whitney 140.4386 11.8646 35.59 Compare
All data (56 fields)
Name
PW1133G1-JM
EASA ID
15PW107
Aircraft Engine Manufacturer
Pratt & Whitney
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
Yes
Combustion Chamber
TALON X
Afterburner
No
Streams
2
Bypass Ratio
11.4
Overall Pressure Ratio
38.85
Maximum Takeoff Thrust (kN)
147.28
Hydrocarbon Take Off (g/kg fuel)
0.03
Hydrocarbon Climb Out (g/kg fuel)
0.03
Hydrocarbon Approach (g/kg fuel)
0.04
Hydrocarbon Idle (g/kg fuel)
0.05
Hydrocarbon Unitary Average (g/kN)
0.1
Hydrocarbon Unitary Characteristic (g/kN)
0.2
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
1.02
Hydrocarbon LTO (g)
16
Carbon Monoxide Take Off (g/kg fuel)
0.14
Carbon Monoxide Climb Out (g/kg fuel)
0.2
Carbon Monoxide Approach (g/kg fuel)
3.59
Carbon Monoxide Idle (g/kg fuel)
17.89
Carbon Monoxide Unitary Average (g/kN)
20.5
Carbon Monoxide Unitary Characteristic (g/kN)
25.2
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
21.36
NOx Take Off (g/kg fuel)
25.23
NOx Climb Out (g/kg fuel)
18.92
NOx Approach (g/kg fuel)
9.14
NOx Idle (g/kg fuel)
6.98
NOx Unitary Average (g/kN)
33
NOx Unitary Characteristic (g/kN)
38.3
NOx Unitaryto Standard (% of limit)
32.54
NOx Unitaryto CAEP2 (% of limit)
40.68
NOx Unitaryto CAEP4 (% of limit)
45.22
NOx Unitaryto CAEP6 (% of limit)
49.96
NOx Unitaryto CAEP8 (% of limit)
56.48
NOx LTO (g)
4864
Smoke Take Off (SN)
4.4
Smoke Climb Out (SN)
2.01
Smoke Approach (SN)
0.34
Smoke Idle (SN)
0.54
Smoke Max (SN)
4.4
Smoke Characteristic (SN)
5.7
Smoke Characteristicto Regulatory (% of limit)
26.78
Fuel Flow Take Off (kg/s)
1.02297
Fuel Flow Climbout (kg/s)
0.838543
Fuel Flow Approach (kg/s)
0.278342
Fuel Flow Idle (kg/s)
0.09878
Fuel LTO (kg)
374.6
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
3025
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)