Liberty L-4

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by FrescoBot (talk | contribs) at 21:46, 25 September 2022 (Bot: link syntax). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Liberty L-4
Liberty L-4 aircraft engine
Type Piston aero engine
National origin United States
Manufacturer Hudson Motor Car Company
Designer Jesse G. Vincent and Elbert J. Hall
First run 1917
Number built 2
Variants Liberty L-6, Liberty L-8, Liberty L-12

Created in 1917, the Liberty L-4 was a four-cylinder water-cooled inline aircraft engine developed in the United States during World War I. The Liberty L-4 was an experimental engine of 102 hp (76 kW), which was built by the Hudson Motor Car Company and primarily intended for use in training airplanes. Only two examples were produced, since other types of engines were available and already in production. While the engine was ground-tested, it is unknown if the L-4 was ever test-flown. The L-4 was created as part of a US aircraft engine development effort which also created the six-cylinder Liberty L-6, eight-cylinder Liberty L-8 and twelve-cylinder Liberty L-12.

Specifications

General characteristics

  • Type: Four-cylinder inline piston engine
  • Bore: 5 in. (127mm)
  • Stroke: 7 in. (177.8mm)
  • Displacement: 549.8 cuin (9.0 L)

Components

  • Cooling system: Water-cooled

Performance

  • Power output: 102 hp (76 kW)

See also

Related lists

References

This article incorporates text from Liberty L-4, a public domain work of the United States Government.

  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 106.