Hirth F-23

{{Short description|German two-stroke aircraft engine}}

{{Use dmy dates|date=January 2022}}

{{Use British English|date=January 2022}}

{{Infobox Aircraft Begin

| name=Hirth F-23

| image=

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}}{{Infobox Aircraft Engine

|type=Twin cylinder two-stroke aircraft engine

|manufacturer=Hirth

|national origin=Germany

|first run=

|major applications=

|produced=

|number built=

|developed from=

|variants with their own articles=

}}

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.Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page G-3 Cybair Limited Publishing, 2001. {{ISBN|0-9680628-1-4}}{{cite web|url = http://www.recpower.com/F-23%202%20cycle%2050hp.htm|title = F-23 2 cycle 50hp |accessdate = 17 January 2013|last = Recreational Power Engineering |authorlink = |year = n.d.}}Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 72. BAI Communications. {{ISBN|0-9636409-4-1}}

Development

The F-23 is intended to compete with the {{convert|50|hp|kW|0|abbr=on}} 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.

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

The F-23 produces {{convert|50|hp|kW|0|abbr=on}} at 6150 rpm and {{convert|40|hp|kW|0|abbr=on}} at 5500 rpm.

Applications

Specifications (F-23)

{{pistonspecs|

|ref=Recreational Power Engineering

|type=Twin cylinder, two-stroke, aircraft engine

|bore={{convert|72|mm|in|1|abbr=on}}

|stroke={{convert|64|mm|in|1|abbr=on}}

|displacement=521 cc (31.8 cu in)

|length={{convert|247|mm|in|1|abbr=on}}

|diameter=

|width={{convert|570|mm|in|1|abbr=on}}

|height={{convert|338|mm|in|1|abbr=on}}

|weight={{convert|84|lb|kg|1|abbr=on}} including reduction unit, full exhaust system and electric start

|valvetrain= piston-ported

|supercharger=

|turbocharger=

|fuelsystem=2 X Bing 34mm slide or optional diaphragm type carburetor or fuel injection

|fueltype=unleaded 93 octane auto fuel

|oilsystem=50:1 fuel/oil premix

|coolingsystem=free air

|power={{convert|50|hp|kW|0|abbr=on}} at 6150 rpm

|specpower=

|compression=9.5:1

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=

|designer=

|reduction_gear= cog belt with 1.8:1, 2.2:1 and 2.5:1 ratios optional

|general_other=

|components_other=

|performance_other=

}}

{{aircontent

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|related=

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}}

References

{{Reflist}}