Jump to content

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.

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

Performance

  • Power output: 280 kW (380 hp) at 1,420 rpm

See also

[edit]

Comparable engines

Related lists

References

[edit]
  1. ^ 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)