The 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]
| Scarlett 7H | |
|---|---|
| Type | Aircraft engine |
| National origin | Czech Republic |
| Manufacturer | Verner Motor |
By April 2018 the engine was no longer advertised on the company website and seems to be out of production.[2]
Design and development edit
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) edit
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
Performance
- Power output: 117 hp (87 kW)
- Compression ratio: 7.3:1
See also edit
Related lists
References edit
- ^ 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
- ^ Verner Motor. "Verner Motor". www.vernermotor.com. Retrieved 25 April 2018.