1930s French piston aircraft engine
The Potez 4D was a four-cylinder, inverted inline aircraft engine. It was first built shortly before World War II , but did not enter full production until 1949 . 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.
Variants
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
Applications
Specifications (Potez 4-D 01)
Data from Jane's All The World's Aircraft 1953-54. [ 1]
General characteristics
Type: Four-cylinder air-cooled inverted inline engine
Bore : 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 valves
Fuel system: One Zenith carburettor
Fuel type: 80 octane minimum
Oil system: Dry sump with one pressure and two scavenge pumps
Cooling system: air-cooled
See also
Comparable engines
Related lists
Notes
References
Wikimedia Commons has media related to
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