Details of Mark III 4-cylinder vertical air-cooled aircraft engine introduced by A. D. C. Aircraft Ltd.; alternative and interchangeable engine for use when more power is desirable than provided in Mark II; new cylinder heads, larger valves, modified valve gear, and connecting rods designed for higher speeds; 85 b.hp. developed at 1900 r.p.m.; bore 110 mm.; stroke 130 mm.; compression ratio 5.4 to 1; 280 lb. weight, dry. (See also Aeroplane vol. 35, no. 11, Sept. 12, 1928 p. 472, 2 figs; and Aviation, vol. 25, no. 22, Nov. 24, 1928, pp. 1620, 1640 and 1642, 3 figs)
The cirrus Mark III engine
Flight
Flight ; 20 , n 35
1928
2 pages
2 Figs.
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1928
Engineering Index Backfile | 1928
Engineering Index Backfile | 1926
Engineering Index Backfile | 1945
Engineering Index Backfile | 1945