Английская Википедия:Hirth F-263

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

The Hirth F-263 is a twin cylinder, in-line, two stroke, carburetted aircraft engine that was designed for use on ultralight aircraft. It was manufactured by Hirth of Germany, but was discontinued about 2001.[1]

Development

The F-263 uses fan cooling and piston-ported induction, with a single Bing carburetor and single capacitor discharge ignition. The cylinder walls are electrochemically coated with Nikasil. Standard starting is recoil start. A gearbox reduction drive system and electric start were factory options.[1]

The engine produces Шаблон:Convert and runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil. Recommended time between overhauls is 1000 hours.[1]

Applications

Specifications (F-263)

Шаблон:Pistonspecs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

Шаблон:Hirth aeroengines

Партнерские ресурсы
Криптовалюты
Магазины
Хостинг
Разное

  1. ↑ 1,0 1,1 1,2 Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page G-3 Cybair Limited Publishing, 2001. Шаблон:ISBN
  2. ↑ Шаблон:Cite web
  3. ↑ Шаблон:Cite web
Источник — http://wikihandbk.com/ruwiki/index.php?title=Английская_Википедия:Hirth_F-263&oldid=15253067