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Wright 4 / Vertical 4



The Wright Vertical 4 engine was an early aircraft piston engine with four inline cylinders.
Among other aircraft the Vertical 4 powered the U.S. Navy's first Wright aircraft, the B-1 "hydroaeroplane".




Type: 4-cylinder, liquid-cooled inline piston aircraft engine
Displacement: 240 cubic inches (3.9 l)
Length: 25 inches (635 mm)
Width: 14 inches (356 mm)
Height: 35 inches (890 mm)
Dry weight: 180 pounds (81.6 kg)
Cooling system: liquid-cooled
Power output: 36 horsepower (27 kW) at 1600 rpm






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