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Wankel AG LCR - 814 TGti

From Wikipedia, the free encyclopedia

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

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)

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

Related lists

References

  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

External links

This page was last edited on 18 August 2023, at 16:58
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