Specific Fuel Consumption
19.827 g/(kN·s)
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
Compact reverse flow annular |
| 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
2.9 |
Overall Pressure Ratio
—
|
Afterburner
No |
Pictures
No pictures yet for this family.
Airplanes
All data (15 fields)
- Name
- GE Honda HF120
- Aircraft Engine Manufacturer
- GE Honda Aero Engines
- Aircraft Engine Type
- Turbofan
- Dry Weight (kg)
- 211.3
- Diameter (mm)
- 655.32
- Length (mm)
- 1511.3
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/GE_Honda_HF120
- Geared Fan
- No
- Combustion Chamber
- Compact reverse flow annular
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 2.9
- Specific Fuel Consumption (g/(kN·s))
- 19.827
- Compressor Description
- One wide-chord fan, two axial LP stages, one centrifugal HP stage.
- Turbine Description
- One axial HP stage (48,777 rpm), two axial LP stages (19,055 rpm).