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Verner JCV 360

From Wikipedia, the free encyclopedia
JCV 360
Type Aircraft engine
National origin Czech Republic
Manufacturer Verner Motor
Major applications Airsport Song
North Wing Maverick
Spacek SD-1 Minisport
Produced up until about 2013

The Verner JCV 360 is a Czech aircraft engine, designed and built by Verner Motor of Šumperk for use in ultralight aircraft.[1]

Design and development

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The engine is a twin cylinder, 360 cc (22.0 cu in), horizontally-opposed four-stroke, liquid-cooled, gasoline engine design, with a poly V belt reduction drive with reduction ratio of 2.76:1. It employs a single electronic ignition and produces 35 hp (26 kW) at 7800 rpm.[1]

The engine was still advertised for sale on the company website in 2013, but by 2015 was no longer listed as available and it is likely that production has ended.[2]

Applications

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Specifications (JCV 360)

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Data from World Directory of Leisure Aviation 2011-12[1]

General characteristics

  • Type: Twin cylinder, horizontally-opposed, four stroke aircraft engine
  • Bore: 63 mm (2.5 in)
  • Stroke: 58 mm (2.3 in)
  • Displacement: 360 cc (22.0 cu in)
  • Length: 580 mm (22.8 in)
  • Width: 340 mm (13.4 in)
  • Height: 360 mm (14.2 in)
  • Dry weight: 30.5 kg (67.2 lb)

Components

Performance

See also

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Related lists

References

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  1. ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 242-243. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^ "Verner Motor". archive.org. Retrieved 30 June 2015. Archive index at the Wayback Machine
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