The Austro Engine GIAE110R is an Austrian aircraft engine, designed and produced by Austro Engine of Wiener Neustadt for use in light aircraft.[1]
As of 2015 the engine is not listed as available on the company website and may not have been developed past prototype stage.[2]
Design and development
The engine is a twin rotor four-stroke, air and liquid-cooled, 588 cc (35.9 cu in), gasoline Wankel engine design, with a mechanical gearbox reduction drive, employing a helical gear set, with reduction ratio of 2.96:1. It employs dual capacitor discharge ignition and produces 105 hp (78 kW) at 7500 rpm.[1]
Specifications (GIAE110R)
Data from World Directory of Leisure Aviation 2011-12[1]
General characteristics
- Type: Twin rotor, four stroke Wankel aircraft engine
- Displacement: 588 cc (35.9 cu in)
- Length: 720 mm (28.3 in)
- Width: 530 mm (20.9 in)
- Height: 420 mm (16.5 in)
- Dry weight: 54 kg (119.0 lb)
Components
- Fuel type: gasoline
- Cooling system: liquid or air
- Reduction gear: mechanical gearbox, helical gear reduction drive, reduction ratio of 2.96:1
Performance
- Power output: 105 hp (78 kW) at 7500 rpm
- Compression ratio: 9.5:1
See also
Related lists
References
- ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 238-239. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ Austro Engine. "Products". austroengine.at. Retrieved 8 July 2015.