The Vaxell 80i is a Polish aircraft engine, designed and produced by Vaxell of Bydgoszcz for use in ultralight and homebuilt aircraft.[1]
| 80i | |
|---|---|
| Type | Aircraft engine |
| National origin | Poland |
| Manufacturer | Vaxell |
Design and development edit
The Vaxell 80i engine is a four-cylinder four-stroke, horizontally-opposed, 1,900 cc (115.9 cu in) displacement, air-cooled, direct-drive, petrol engine design. It employs dual electronic ignition, electronic, multipoint fuel injection and produces 80 hp (60 kW) at 3100 rpm.[1]
Specifications (80i) edit
Data from Tacke[1]
General characteristics
- Type: Four cylinder, four stroke aircraft engine
- Displacement: 1,900 cc (115.9 cu in)
- Length: 670 mm (26.4 in)
- Width: 770 mm (30.3 in)
- Height: 380 mm (15.0 in)
- Dry weight: 73.5 kg (162.0 lb) dry weight
Components
- Fuel system: electronic, multipoint fuel injection
- Fuel type: petrol
- Cooling system: air
- Reduction gear: none
Performance
- Power output: 80 hp (60 kW) at 3100 rpm
See also edit
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