Lancia Tipo 4
From Wikipedia, the free encyclopedia
| Tipo 4 | |
|---|---|
 | |
| Type | V-12 aero engine |
| Manufacturer | Lancia |
| First run | 1916 |
The Lancia Tipo 4 was an Italian aircraft engine constructed by Lancia in the mid-1910s.
This water-cooled V-12 aircraft engine was built in 1916 and had a 50-degree angle between the cylinder banks. The Tipo 4 had a 120.7 mm (4.75 in) bore and a 180.1 mm (7.09 in) stroke. The engine’s total displacement was 24.7 L (1,508 cu in). It produced 240 kW (320 hp) at 1,380 rpm and 280 kW (380 hp) at 1,420 rpm. The Tipo 4 engine was direct drive and weighed 340 kg (740 lb). The engine shipped to the United States in late 1917.[1]