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Aixro XF-40
German aircraft motor From Wikipedia, the free encyclopedia
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The Aixro XF-40 (or XF40) is a German aircraft engine, designed and produced by Aixro of Aachen for use in ultralight aircraft.[1]
Design and development
The XF-40 is a single-rotor Wankel engine. It is a 294 cc (17.9 cu in) displacement, liquid-cooled, petrol engine design, with a poly V belt reduction drive with a reduction ratio of 1.25:1. It employs capacitor discharge ignition and produces 36 hp (27 kW) at 6500 rpm.[1]
Applications
Specifications (XF-40)
Data from Tacke[1]
General characteristics
- Type: Single rotor Wankel aircraft engine
- Displacement: 294 cc (17.9 cu in)
- Length: 300 mm (11.8 in)
- Width: 250 mm (9.8 in)
- Height: 250 mm (9.8 in)
- Dry weight: 18.7 kg (41.2 lb)
Components
- Fuel type: petrol
- Cooling system: liquid
- Reduction gear: poly V belt
Performance
- Power output: 36 hp (27 kW)
See also
Related lists
References
External links
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