Hirth F-36
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The Hirth F-36 is a single-cylinder, two-stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and ultralight trikes. It is noted for its extremely small equipped weight of Script error: No such module "convert". including exhaust system, reduction drive and carburetor. It is manufactured by Hirth of Germany.[1]
The F-36 was formerly known as the Solo 210, before the design was purchased by Hirth.[2][3]
Development
The engine uses free air cooling, single capacitor discharge ignition, with a single integral pump-type carburettor. 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.[1]
The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil and produces Script error: No such module "convert". at 6000 rpm.[1]
Applications
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Specifications (F-36)
Data from Recreational Power Engineering[1]
General characteristics
- Type: Single cylinder, two-stroke, aircraft engine
- Bore: Script error: No such module "convert".
- Stroke: Script error: No such module "convert".
- Displacement: 208 cc (12.7 cu in)
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- Dry weight: Script error: No such module "convert". with reduction drive, exhaust system and recoil start
Components
- Fuel system: 1 X integral pumper carburetor
- Fuel type: Minimum of unleaded 93 octane auto fuel
- Oil system: 50:1 fuel/oil premix
- Cooling system: free air
- Reduction gear: four element cog belt with ratios of 1.8:1, 2.0:1 or 2.5:1 available
Performance
- Power output: Script error: No such module "convert". at 6000 rpm
- Compression ratio: 10.6:1
References
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External links
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