Vaxell 80i
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 |
Unit cost | €7,100 (2015) |
Design and development
The Vaxell 80i engine is a four-cylinder four-stroke, horizontally-opposed, 1,900 cc (115.9 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs dual electronic ignition, electronic, multipoint fuel injection and produces 80 hp (60 kW) at 3100 rpm.[1]
Specifications (80i)
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: gasoline
- Cooling system: air
- Reduction gear: none
Performance
- Power output: 80 hp (60 kW) at 3100 rpm
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gollark: Which TOML library are you using?
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gollark: ```python>>> print(toml.dumps({"a": {"b": {"c": 4}}})... )[a.b]c = 4```
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
External links
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