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Wankel AG LCR - 407 SGti

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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

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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)

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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

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Related lists

References

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  1. ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
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