The Lancia Tipo 4 was an Italian aircraft engine constructed by Lancia in the mid-1910s.
| Tipo 4 | |
|---|---|
| |
| Type | V-12 aero engine |
| Manufacturer | Lancia |
| First run | 1916 |
History edit
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]
Applications edit
Specifications edit
Data from Old Machine Press.[1]
General characteristics
- Type: V-12 piston engine
- Bore: 120.7 mm (4.75 in)
- Stroke: 180.1 mm (7.09 in)
- Displacement: 24.7 L (1,508 cu in)
- Dry weight: 340 kg (740 lb)
Performance
- Power output: 280 kW (380 hp) at 1,420 rpm
See also edit
Comparable engines
Related lists
References edit
- ^ a b "Lancia Tipo 4 and Tipo 5 V-12 Aircraft Engines". Old Machine Press. Retrieved 2018-07-11.
- Lancia Michael Frostick Published by Dalton Watson Ltd., London (1976)