Wankel AG LCR - 814 TGti
| LCR - 814 TGti | |
|---|---|
| Type | Aircraft engine |
| National origin | Germany |
| Manufacturer | Wankel AG |
The Wankel AG LCR - 814 TGti is a German Wankel aircraft engine, designed and produced by Wankel AG of Kirchberg, Saxony for use in ultralight aircraft.[1]
Design and development
[edit]The LCR - 814 TGti engine is a twin-rotor four-stroke, 814 cc (49.7 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 75 hp (56 kW) at 6000 rpm.[1]
Specifications (LCR - 814 TGti)
[edit]Data from Tacke[1]
General characteristics
- Type: Twin rotor, four stroke, Wankel aircraft engine
- Displacement: 814 cc (49.7 cu in)
- Length: 600 mm (23.6 in)
- Width: 462 mm (18.2 in)
- Height: 430 mm (16.9 in)
- Dry weight: 46 kg (101.4 lb)
Components
- Fuel type: petrol, 92 octane
- Cooling system: liquid
- Reduction gear: toothed poly V belt
Performance
- Power output: 75 hp (56 kW)
See also
[edit]Related lists