1930s French piston aircraft engine
ThePotez 4D was a four-cylinder, inverted inline aircraft engine. It was first built shortly beforeWorld War II , but did not enter full production until1949 . Like the other D-series engines, the cylinders had a bore of 125 mm (4.9 in) and a stroke of 120 mm (4.7 in). Power for different models was in the 100 kW-190 kW (140 hp-260 hp) range.
4D-00 127 kW (170 hp) 4D-01 119 kW (160 hp) 4D-30 179 kW (240 hp) 4D-31 164 kW (220 hp) 4D-32 179 kW (240 hp) 4D-33 119 kW (160 hp) 4D-34 194 kW (260 hp) 4D-36 194 kW (260 hp) 4D-34 with aerobatic oil system Specifications (Potez 4-D 01)[ edit ] Data from Jane's All The World's Aircraft 1953-54. [ 1]
General characteristics Type: Four-cylinder air-cooled inverted inline engineBore : 125 mm (4.92 in)Stroke : 120 mm (4.72 in)Displacement : 5.85 L (352 in³)Length: 1,207.5 mm (47.5 in)Width: 510 mm (20.1 in)Height: 668.5 mm (26.3 in)Dry weight : 143 kg (314.6 lb)
Components Valvetrain : Two valves per cylinder with sodium cooled exhaust valvesFuel system: One Zenith carburettorFuel type: 80 octane minimumOil system: Dry sump with one pressure and two scavenge pumpsCooling system: air-cooled
Performance Comparable engines
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Potez 4D .
Bridgman, Leonard, ed. (1953).Jane's All The World's Aircraft 1953-54 . London: Jane's. Bridgman, Leonard, ed. (1961).Jane's All The World's Aircraft 1961–62 . London: Sampson Low, Marston & Company, Ltd. Gunston, Bill (1986).World Encyclopedia of Aero Engines . Wellingborough: Patrick Stephens. p. 107.
Inline engines Horizontally opposed engines Radial engines