Maximum Takeoff Thrust
2.7 kN
Specific Fuel Consumption
19.346 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
Annular combustion chamber |
| 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
1 |
Overall Pressure Ratio
—
|
Afterburner
No |
Pictures
No pictures yet for this family.
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All data (18 fields)
- Name
- Williams F107
- Aircraft Engine Manufacturer
- Williams International
- Aircraft Engine Type
- Turbofan
- Dry Weight (kg)
- 30.3907
- Diameter (mm)
- 304.8
- Length (mm)
- 609.6
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Williams_F107
- Fuel
- JP-4 / JP-5 / JP-10
- Geared Fan
- No
- Combustion Chamber
- Annular combustion chamber
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 1
- Maximum Takeoff Thrust (kN)
- 2.7
- Thrust To Weight
- 6.42
- Specific Fuel Consumption (g/(kN·s))
- 19.346
- Compressor Description
- 2-stage fan, 2-stage axial IP compressor, 1-stage centrifugal HP compressor
- Turbine Description
- 1-stage HP turbine, 2-stage LP turbine