ULPower UL260i explained

The ULPower UL260i is a family of aircraft engines, produced by ULPower in Belgium.

Design

The UL260i series are all lightweight, four-cylinder, four-stroke, horizontally-opposed, air-cooled, direct drive engine designs that feature FADEC with multipoint fuel injection and dual ignition systems.[1]

Variants

UL260i
  • Base model, fuel injection, compression ratio of 8.16:1, producing 970NaN0[1] [2]
    UL260iS
  • Model with a higher compression ratio of 9.10:1, fuel injection, producing 1070NaN0[3]
    UL260iSA
  • Aerobatic model with a higher compression ratio of 9.10:1, fuel injection, producing 1070NaN0[4]
    UL260iF
  • Model with a higher compression ratio of 9.10:1, fuel injection, producing 1000NaN0, due to French regulatory requirements.[5]

    See also

    Related development
    Lists
    Comparable engines

    Notes and References

    1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262-263. Flying Pages Europe SARL, 2015.
    2. Web site: UL260i. ULPower Aero Engines. ulpower.com. 21 April 2018.
    3. Web site: UL260iS. ULPower Aero Engines. ulpower.com. 21 April 2018.
    4. Web site: UL260iSA. ULPower Aero Engines. ulpower.com. 21 April 2018.
    5. Web site: UL260iF . ULPower Aero Engines. ulpower.com. 21 April 2018.

    This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "ULPower UL260i".

    Except where otherwise indicated, Everything.Explained.Today is © Copyright 2009-2024, A B Cryer, All Rights Reserved. Cookie policy.