Rotax 277

277
Type Piston aero-engine
National origin Austria
Manufacturer Rotax
Major applications Ultralight aircraft



The Rotax 277 is a 26 hp (19 kW), single-cylinder, two-stroke aircraft engine, that was built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft.[1][2]

Development

The Rotax 277 features a single piston ported, air-cooled cylinder head and cylinder, utilizing either a fan or free air for cooling. Lubrication is pre-mixed fuel and oil. The 277 has a single Bosch flywheel magneto generator 12 volt ignition system and is equipped with a 36 mm Bing double float carburetor, with either a hand lever or cable choke.[1][2]

The Rotax 277 is no longer in production.[1]

Applications

Specifications (277)

Data from ROTAX 277 UL Data Sheet[1]

General characteristics

Components

Performance

See also


References

  1. 1 2 3 4 BRP-Rotax GmbH & Co. KG (n.d.). "ROTAX 277 UL - 26 hp Fan Cooled" (PDF). Retrieved 2009-03-14.
  2. 1 2 Raisner, William: LEAF catlog, pages 6-105. Leading Edge Airfoils, 1995.


This article is issued from Wikipedia - version of the Saturday, December 05, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.