Hirth F-23
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The Hirth F-23 is a twin cylinder, horizontally-opposed, two stroke, carburetted or optionally fuel injected aircraft engine designed for use on ultralight aircraft. It is manufactured by Hirth of Germany.[1][2][3]
Development
The F-23 is intended to compete with the Script error: No such module "convert". Rotax 503 and is differentiated from the Rotax powerplant by offering a horizontally opposed cylinder layout. The F-23 uses free air cooling and piston-ported induction, with dual Bing 34mm slide or optional diaphragm type carburetors. The cylinder walls are electrochemically coated with Nikasil. Standard starting is recoil start. A belt reduction drive system, fuel injection, tuned exhaust and electric start are optional.[1][2]
The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil. Recommended time between overhauls is 1000 hours.[1][2]
The F-23 produces Script error: No such module "convert". at 6150 rpm and Script error: No such module "convert". at 5500 rpm.[1][2]
Applications
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Specifications (F-23)
Data from Recreational Power Engineering[2]
General characteristics
- Type: Twin cylinder, two-stroke, aircraft engine
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- Stroke: Script error: No such module "convert".
- Displacement: 521 cc (31.8 cu in)
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- Dry weight: Script error: No such module "convert". including reduction unit, full exhaust system and electric start
Components
- Valvetrain: piston-ported
- Fuel system: 2 X Bing 34mm slide or optional diaphragm type carburetor or fuel injection
- Fuel type: unleaded 93 octane auto fuel
- Oil system: 50:1 fuel/oil premix
- Cooling system: free air
- Reduction gear: cog belt with 1.8:1, 2.2:1 and 2.5:1 ratios optional
Performance
- Power output: Script error: No such module "convert". at 6150 rpm
- Compression ratio: 9.5:1
References
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External links
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