Details of 4 cylinder vertical air-cooled in-line engine suitable for use in light airplanes of Moth type; bore 114 mm.; stroke 128 mm.; compression ratio 5 to 1; weight 285 lb.; 90 b.hp. developed at 1900 r.p.m.; maximum of 100 b.hp. developed at 2100 r.p.m.; fuel consumption 0.59 pints per hp-hr.; separate detachable cylinder heads of aluminum alloy; inlet and exhaust ports on port-side engine. (See also Aeroplane vol. 36, no. 2, Jan. 9, 1929 p. 94, 2 figs)


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    Title :

    The De Havilland Gipsy engine


    Additional title:

    Flight


    Published in:

    Flight ; 21 , n 29


    Publication date :

    1929


    Size :

    2 pages


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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