Engineering:Wankel AG LCR - 407 SGti
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Short description: German aircraft motor
LCR - 407 SGti | |
---|---|
Type | Aircraft engine |
National origin | Germany |
Manufacturer | Wankel AG |
The Wankel AG LCR - 407 SGti is a German Wankel aircraft engine, designed and produced by Wankel AG of Kirchberg, Saxony for use in ultralight aircraft.[1]
Design and development
The LCR - 407 SGti engine is a single-rotor four-stroke, 407 cc (24.8 cu in) displacement, liquid-cooled, fuel injected, petrol, Wankel engine design, with a toothed poly V belt reduction drive with a reduction ratio of 3:1. It employs dual electronic ignition and produces 37 hp (28 kW) at 6000 rpm.[1]
Specifications (LCR - 407 SGti)
Data from Tacke[1]
General characteristics
- Type: Single rotor, four stroke, Wankel aircraft engine
- Displacement: 407 cc (24.8 cu in)
- Length: 481 mm (18.9 in)
- Width: 462 mm (18.2 in)
- Height: 430 mm (16.9 in)
- Dry weight: 35.0 kg (77.2 lb)
Components
- Fuel type: petrol, 92 octane
- Cooling system: liquid
- Reduction gear: toothed poly V belt
Performance
- Power output: 37 hp (28 kW)
See also
Related lists
References
External links
Original source: https://en.wikipedia.org/wiki/Wankel AG LCR - 407 SGti.
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