What distinguished the Clerget rotary engine from its rivals was that the Clerget had normal intake and exhaust valves unlike the Gnome, and the connecting rod arrangement was much simpler than the Le Rhone. A source of failure among the Clerget engines were the special-purpose piston rings, called obturator rings. These were located below the gudgeon or wrist pin, to block heat transfer from the combustion area to the lower part of the cylinder and overcome their subsequent distortion. These rings were often made from brass and only had a lifespan of a few hours. The Clerget engines were considered reliable but they cost more per unit to produce than their rivals. Unlike other contemporary rotaries in which the ignition system was either switched on or off to provide a rudimentary form of engine speed control, the Clerget featured a throttle. The Bentley BR1 and Bentley BR2 rotaries were designed as improvements of the Clerget, while sharing some of the earlier engine's distinctive design features.
The inlet and exhaust valves were mechanically operated by means of separate cams, tappets and rocker arms.
The direction of rotation was counter -clockwise as seen from the propeller-end of the engine. Between any two consecutive firing strokes, the engine turned through 80 degrees. Like many other rotary engines of the period they were made chiefly of steel, for strength and lightness.
based at Old Warden Aerodrome in the UK, operate an airworthy late production Sopwith Triplane' fitted with an original 9B as well as an airworthy late production Sopwith Camel ' fitted with an original long-stroke 9Bf. These aircraft can be seen displaying at home air displays through the summer months.
Radial 'X' engines
;Clerget 16X
Diesel radial engines
In the 1920s Pierre Clerget designed static diesel radial engines, the earliest were based on his rotary designs. ;Clerget 9A 100 hp Nine-cylinder, single row radial engine. ;Clerget 9B: ;Clerget 9C: Produced under licence by Hispano-Suiza as the Hispano-Suiza 9T ;Clerget 14F-01 14-cylinder, two-row radial engine, flown in a Potez 25 biplane. ;;Clerget 14F-02: ;;Clerget 14Fcs:
H-16 engine
Clerget's final engine design was an H-16 known as the Type Transatlantique. It developed 2,000 hp through the use of four turbochargers.