A-7-R is 7-cylinder, static, radial, air-cooled engine developing 150 hp. at 1800 r.p.m.; compensating rocker boxes maintain given tappet clearances regardless of temperature; cam rollers installed in roller arms to eliminate side thrust; push-rod housings and other accessories mounted on rear of engine to reduce wind resistance; weights 430 lb. without propeller hub; 4 1/2-in. bore and 5 1/2-in. stroke with 612.15 cu. in. displacement; 8.6 gal. gasoline and .35 gal. oil per hour. (see also Aero Digest, vol. 12, no. 3, Mar. 1928, p. 382, 1 fig.; and West. Flying, vol. 4, no. 3, Mar. 1928, pp. 32 and 93, 1 fig.)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The Floco aviation engine


    Weitere Titelangaben:

    Aviation


    Erschienen in:

    Aviation ; 24 , n 10


    Erscheinungsdatum :

    1928


    Format / Umfang :

    2 pages


    Anmerkungen:

    3 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aviation engine development

    Sherbondy, E.H. | Engineering Index Backfile | 1917


    AVIATION ENGINE DEVELOPMENT

    SHERBONDY, E. H. | SAE Technical Papers | 1917


    British aviation engine inspection

    Bagnall-Wild, R.K. | Engineering Index Backfile | 1918


    Art of aviation engine

    Banks, C.R. | Engineering Index Backfile | 1948


    Wisconsin adds aviation engine

    Engineering Index Backfile | 1916