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・ Hirtenberg HS.9
・ Hirtenberg HV.15
・ Hirtenberger M6C-210
・ Hirtenkäse
・ Hirtenschalmei
・ Hirter
・ Hirth
・ Hirth (surname)
・ Hirth 2702
・ Hirth 2704
・ Hirth 3202
・ Hirth 3502
・ Hirth 3701
・ Hirth Acrostar
・ Hirth F-23
Hirth F-263
・ Hirth F-30
・ Hirth F-33
・ Hirth F-36
・ Hirth Hi 20 MoSe
・ Hirth Hi 21
・ Hirth Hi 25 Kria
・ Hirth HM 500
・ Hirth HM 504
・ Hirth HM 506
・ Hirth HM 508
・ Hirth HM 512
・ Hirth HM 60
・ Hirth joint
・ Hirthia


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Hirth F-263 : ウィキペディア英語版
Hirth F-263

The Hirth F-263 is a twin cylinder, in-line, two stroke, carburetted aircraft engine that was designed for use on ultralight aircraft. The engine was discontinued about 2001.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page G-3 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕
==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.〔
The engine produces and runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil. Recommended time between overhauls is 1000 hours.〔


抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
ウィキペディアで「Hirth F-263」の詳細全文を読む



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