Английская Википедия:GEN 125

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Шаблон:Short description Шаблон:Use dmy dates Шаблон:Use American English

The GEN 125 is a Japanese aircraft engine, designed and produced by the GEN Corporation for use in ultralight helicopters.[1]

Design and development

The engine is a twin cylinder two-stroke, horizontally-opposed, air-cooled, Шаблон:Convert, direct-drive, gasoline engine design. It employs capacitor discharge ignition and produces Шаблон:Convert at 8500 rpm. The engine weighs Шаблон:Convert.[1]

The engine was designed specifically for the GEN H-4 helicopter, in which four of the engines are mounted to provide redundancy.[1]

Variants

GEN 125
Base model producing Шаблон:Convert[1]
GEN 125-F
Model producing Шаблон:Convert[1]

Applications

Specifications (GEN 125)

Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

External links

  1. 1,0 1,1 1,2 1,3 1,4 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, pages 191 and 238-239. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X