Fiat A.20

From Wikipedia, the free encyclopedia

The Fiat A.20 was an Italian aero-engine of the 1920s. It was a water-cooled V12 engine that was used by early versions of the Fiat CR.20 fighter and the Macchi M.41 seaplane.

In 1923, FIAT built the A.15, a 430 hp (320 kW) water-cooled V12 engine. While no production of the A.15 ensued, it formed the basis for the Fiat A.20, which differed in being a Monobloc engine, and delivered a similar power despite a reduction in capacity from 20.3 to 18.7 L (1,239 to 1,141 in3).[1]

Applications

Specifications

Data from The Fiat A.20 [5]

General characteristics

  • Type: Water-cooled V12 engine
  • Bore: 115 mm (4.5 in)
  • Stroke: 150 mm (5.9 in)
  • Displacement: 18.7 L (1,141 in3)[6]
  • Length: 1,645 mm (64.8 in)
  • Width: 645 mm (25.4 in)
  • Height: 845 mm (33.3 in)
  • Dry weight: 317.5 kg (699 lb)

Components

  • Fuel system: twin carburettorss
  • Cooling system: water-cooled

Performance

See also


Related lists

References

  1. Gunston 1986, pp. 55–56.
  2. 2.0 2.1 2.2 2.3 2.4 2.5 "Fiat A.20". www.aviogroup.com. Retrieved 5 March 2010.
  3. Taylor 1981, p.54.
  4. Angelucci 1981, p.124.
  5. Flight 6 May 1926, p.275.
  6. Flight 9 December 1926, p.807.
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.