Hirth F-33

Source: Wikipedia, the free encyclopedia.

Hirth F-33
Type Single cylinder
two-stroke aircraft engine
National origin Germany
Manufacturer Hirth

The Hirth F-33 is a

ultralight aircraft, including powered paragliders and ultralight trikes. the engine is noted for its extremely light base weight of 35 lb (16 kg). It is manufactured by Hirth of Germany.[1][2][3]

Development

The F-33 was intended to fill the niche previously occupied by the now out-of-production 28 hp (21 kW)

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-33 produces 22 hp (16 kW) at 5200 rpm and 28 hp (21 kW) at 6500 rpm.[1][2]

Applications

Specifications (F-33)

Data from Recreational Power Engineering[2]

General characteristics

  • Type: Single cylinder, two-stroke, aircraft engine
  • Bore: 76 mm (3.0 in)
  • Stroke: 69 mm (2.7 in)
  • Displacement: 313 cc (19.1 cu in)
  • Length: 300 mm (11.8 in)
  • Width: 299.5 mm (11.8 in)
  • Height: 380 mm (15.0 in)
  • Dry weight
    :
    31 lb (14.1 kg) (base weight) 45 lb (20.4 kg) (with electric start and reduction drive)

Components

  • Valvetrain: Reed valve, piston-ported
  • Fuel system: 1 X Bing 34mm slide or optional diaphragm type carburetor or fuel injection
  • 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

Performance

References

  1. ^
  2. ^ a b c d e Recreational Power Engineering (n.d.). "F-33 2 cycle 28hp". Retrieved 17 January 2013.

External links