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 description in Flight, vol. 21, no. 29, July 18, 1929, pp. 712-713, 1 fig)
The de Havilland gipsy engine
Aeroplane
Aeroplane ; 36 , n 2
1929
2 Figs.
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1928
Engineering Index Backfile | 1929
Engineering Index Backfile | 1938
Engineering Index Backfile | 1938
Engineering Index Backfile | 1938