Details of two radial air-cooled aircraft engines; Challenger has 6 cylinders with 5 1/8-in. bore and 4 7/8-in. stroke; 180 hp. developed at 1800 r.p.m.; weight 420 lb.; two-throw 180-deg. single-piece counterbalanced crankshaft. Chieftain has 12 cylinders with two banks of six cylinders in lines of two; bore 5 5/8 in.; stroke 5 1/2 in.; 615 hp. developed at 2200 r.p.m.; 900 lb. weight.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Curtiss challenger (R, 600) and Curtiss Chieftain (H 1640) engines


    Weitere Titelangaben:

    Aeroplane


    Erschienen in:

    Aeroplane ; 35 , n 9


    Erscheinungsdatum :

    1928


    Anmerkungen:

    4 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Curtiss "Chieftain" engine

    Hildesheim, E. | Engineering Index Backfile | 1928


    Curtiss. Curtiss Robin

    Engineering Index Backfile | 1928


    Curtiss. New curtiss hawk army pursuit plane

    Engineering Index Backfile | 1929


    Curtiss ascender

    Perry, H.W. | Engineering Index Backfile | 1945


    Curtiss crusader

    Engineering Index Backfile | 1929