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・ Hirtenkäse
・ Hirtenschalmei
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・ 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
・ Hirthia globosa
・ Hirthia littorina
・ Hirticallia hirsuta


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Hirth F-36 : ウィキペディア英語版
Hirth F-36

The Hirth F-36 is a single cylinder, two stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and very light ultralight trikes. It is noted for its extremely light equipped weight of including exhaust system, reduction drive and carburetor.
The F-36 was formerly known as the Solo 210, before the design was purchased by Hirth.
==Development==
The engine uses free air cooling, single capacitor discharge ignition, with a single integral pump-type carburetor. The cylinder walls are electrochemically coated with Nikasil. Standard starting is recoil start with electric start optional. A quadruple V belt reduction drive system is an option with ratios of 1.8:1, 2.0:1 or 2.5:1.〔
The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil and produces at 6000 rpm.〔


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-36」の詳細全文を読む



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