The determination of the minimum fuel octane required for an aircraft engine, utilizes detonation equipment and test techniques developed prior to World War II. These procedures were designed to provide a 12% margin of safety on traditional leaded aviation fuels which met the lean and rich ratings as listed in the applicable ASTM specification. Now, due to a possible phase out of leaded fuels, it appears necessary for aircraft engine manufacturers and STC applicants to re-evaluate these techniques and procedures to determine if they are applicable for unleaded fuels. And to re-evaluate existing engines to determine the minimum acceptable requirements for a new unleaded aviation gasoline. This paper reviews these techniques and looks at possible requirements for an unleaded aviation gasoline.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Determination of Minimum Fuel Octane Number Piston Aircraft Engines


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    General, Corporate & Regional Aviation Meeting & Exposition ; 1993



    Publication date :

    1993-05-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Fundamentals of aircraft piston engines

    Borden, N. E. / Cake, W. J. | TIBKAT | 1971


    Octane rating fits fuel to aero engines

    Engineering Index Backfile | 1946


    Aircraft piston engines on-condition exploitation

    Glowacki, Pawel Jan | Emerald Group Publishing | 2018


    High octane safety fuel for aircraft

    Engineering Index Backfile | 1945


    Acoustic Characteristics of Aircraft Piston Engines

    Moshkov, P. A. | Springer Verlag | 2020