Vaxell 60i
From Wikipedia, the free encyclopedia
| 60i | |
|---|---|
| Type | Aircraft engine |
| National origin | Poland |
| Manufacturer | Vaxell |
The Vaxell 60i is a Polish aircraft engine, designed and produced by Vaxell of Bydgoszcz for use in ultralight and homebuilt aircraft.[1]
The Vaxell 60i engine is a four-cylinder four-stroke, horizontally opposed, 1,600 cc (97.6 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs dual electronic ignition, electronic, multipoint fuel injection and produces 60 hp (45 kW) at 3200 rpm.[1]
Specifications (60i)
Data from Tacke[1]
General characteristics
- Type: Four-cylinder, four-stroke aircraft engine
- Displacement: 1,600 cc (97.6 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: gasoline
- Cooling system: air
- Reduction gear: none
Performance
- Power output: 60 hp (45 kW) at 3200 rpm