avia.wikisort.org - EngineThe Verner Scarlett 7H is a Czech aircraft radial engine, designed and produced by Verner Motor of Šumperk for use in ultralight and homebuilt aircraft.[1]
By April 2018 the engine was no longer advertised on the company website and seems to be out of production.[2]
Design and development
The engine is a four-stroke, seven-cylinder radial, 4,386 cc (267.7 cu in) displacement, air-cooled, direct-drive, gasoline engine design. It employs electronic ignition and produces 117 hp (87 kW) at 2300 rpm, with a compression ratio of 7.3:1.[1]
Specifications (Scarlett 7H)
Data from Tacke[1]
General characteristics
- Type: Seven cylinder, four stroke radial aircraft engine
- Bore: 94 mm (3.7 in)
- Stroke: 90 mm (3.5 in)
- Displacement: 4,386 cc (267.7 cu in)
- Length: 602 mm (23.7 in)
- Diameter: 780 mm (30.7 in)
- Dry weight: 81 kg (178.6 lb)
Components
- Fuel type: gasoline, minimum of 95 octane
- Cooling system: air
- Reduction gear: none
- Power output: 117 hp (87 kW)
- Compression ratio: 7.3:1
See also
Related lists
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Verner Motor. "Verner Motor". www.vernermotor.com. Retrieved 25 April 2018.
External links
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