Of horizontally opposed type, engine has two air-cooled cylinders of 90 mm. bore by 96.5 mm. stroke, cylinder center lines' being 1 3/16 in. offset; all valve gear is below crankshaft and consequently center of gravity is below center line of engine; rated at 31 hp. at normal speed of 2900 r.p.m., actual power developed is from 31 to 32 b.hp. at normal speed.
The Bristol-Cherub aero engine
Automobile Engr
Automobile Engineer ; 17 , n 226
1927
3 pages
9 Figs.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
The bristol "cherub" flat twin aero engine
Engineering Index Backfile | 1923
The Bristol "cherub" flat twin aero engine
Engineering Index Backfile | 1923
The bristol "cherub" flat twin aero engine
Engineering Index Backfile | 1923
Engineering Index Backfile | 1924
Bristol "hercules" aero-engine
Engineering Index Backfile | 1941