Hirth 3701 Explained

The Hirth 3701 is an in-line three-cylinder, two-stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft and small homebuilts. It is manufactured by Hirth of Germany.[1] [2]

Development

The 3701 was developed as a liquid-cooled and narrower installation alternative to the four-cylinder Hirth F-30 air-cooled engine of 85to.

The 3701 features triple Bing 34 mm slide carburetors or optionally fuel injection. The cylinder walls are electrochemically coated with Nikasil. Standard starting is electric start and recoil start is not available as an option. The reduction drive system available is the G-50 gearbox, with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1.

The engine runs on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil, or optionally 100:1 oil injection.

Variants

3701 high-torque/low-rpm engine
  • Three-cylinder in-line, two-stroke aircraft engine with three Bing 34 mm slide carburetors or fuel injection. Low piston port timing produces 840NaN0 at 4950 rpm with a very flat torque curve.
    3701 high performance engine
  • Three-cylinder in-line, two stroke aircraft engine with three Bing 34 mm slide carburetors or fuel injection. High piston port timing produces 1000NaN0 at 6000 rpm with a steep torque curve.

    External links

    Notes and References

    1. Web site: 3701S – 2 cycle 100hp . 18 December 2009 . Recreational Power Engineering . https://web.archive.org/web/20060311024349/http://www.recpower.com/3701.htm . 11 March 2006 . dead .
    2. Web site: 3701–2 cycle – 100hp . 18 December 2009 . Ultraligero.Net.