Salmson 9

Salmson 9
Salmson AD 9
Type Radial engine
Manufacturer Salmson
First run 1917

The term Salmson 9 refers to any of a number of nine-cylinder, radial aircraft engines that were developed from 1910 onwards and built by Société des Moteurs Salmson in France. All Salmson engines produced after 1920 were air-cooled.[1]

Contents

Design and development

The designation Salmson 9 merely refers to the number of cylinders and the different series of engines were identified by the letter suffixes. Like most radials, later versions were air-cooled, but early Salmson engines were famous for being the only series-produced water-cooled radials. In common with other engines produced by this manufacturer, Salmson 9s featured the unorthodox Canton-Unné internal arrangement that dispensed with a master rod in favour of a cage of epicyclic gears driving the crankpin. Production ended in 1951 with the liquidation of the manufacturing company.

Variants

Variants of the Salmson 9 included:

Applications

Specifications (9 AB)

Data from Tsygulev[3]

General characteristics

Components

Performance

Specifications (9 NC)

Data from Tsygulev[3]

General characteristics

Components

Performance

See also

Notes

  1. ^ Gunston 1986, p. 158.
  2. ^ a b c * Cuny, Jean. “Latécoère - Les Avions et Hydravions”.Paris. Docavia/Editions Lariviere. 1992. ISBN 2-90 70 51-01-6
  3. ^ a b Tsygulev (1939). Aviacionnye motory voennykh vozdushnykh sil inostrannykh gosudarstv (Russian: Авиационные моторы военных воздушных сил иностранных государств). Moscow: Gosudarstvennoe voennoe izdatelstvo Narkomata Oborony Soyuza SSR. http://base13.glasnet.ru/text/aviamotory/t.htm. 

References