Hirth F-33

{{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-33

| image=HirthF33.jpg

| caption=

}}{{Infobox Aircraft Engine

|type=Single 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-33 is a single cylinder, two stroke, carburetted aircraft engine designed for use on ultralight aircraft, including powered paragliders and ultralight trikes. the engine is noted for its extremely light base weight of {{convert|35|lb|kg|0|abbr=on}}. 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-33%202%20cycle%2028hp.htm|title = F-33 2 cycle 28hp |access-date = 17 January 2013|last = Recreational Power Engineering |year = n.d.}}Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 72. BAI Communications. {{ISBN|0-9636409-4-1}}

Development

The F-33 was intended to fill the niche previously occupied by the now out-of-production {{convert|28|hp|kW|0|abbr=on}} Rotax 277. The F-33 uses free air cooling, dual capacitor discharge ignition and reed valve induction, with a single Bing 34mm slide or optional diaphragm type carburetor. 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-33 produces {{convert|22|hp|kW|0|abbr=on}} at 5200 rpm and {{convert|28|hp|kW|0|abbr=on}} at 6500 rpm.

Applications

Specifications (F-33)

{{pistonspecs|

|ref=Recreational Power Engineering

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

|bore={{convert|76|mm|in|1|abbr=on}}

|stroke={{convert|69|mm|in|1|abbr=on}}

|displacement=313 cc (19.1 cu in)

|length={{convert|300|mm|in|1|abbr=on}}

|diameter=

|width={{convert|299.5|mm|in|1|abbr=on}}

|height={{convert|380|mm|in|1|abbr=on}}

|weight={{convert|31|lb|kg|1|abbr=on}} (base weight) {{convert|45|lb|kg|1|abbr=on}} (with electric start and reduction drive)

|valvetrain=Reed valve, piston-ported

|supercharger=

|turbocharger=

|fuelsystem=1 X Bing 34mm slide or optional diaphragm type carburetor or fuel injection

|fueltype=Minimum of unleaded 93 octane auto fuel

|oilsystem=50:1 fuel-oil premix

|coolingsystem=free air

|power={{convert|28|hp|kW|0|abbr=on}} at 6500 rpm

|specpower=

|compression=9.5:1

|fuelcon=

|specfuelcon=

|oilcon=

|power/weight=0.8

|designer=

|reduction_gear=four element cog belt

|general_other=

|components_other=

|performance_other=

}}

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

References

{{Reflist}}