Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Liberty L-6

From Wikipedia, the free encyclopedia
Six-cylinder water-cooled inline aircraft engine
Liberty L-6
Liberty L-6 aircraft engine on display at theNational Museum of the United States Air Force
TypePistonaero engine
National originUnited States
ManufacturerWright Aeronautical,Thomas-Morse Aircraft
DesignerJesse G. Vincent andElbert J. Hall
First runabout 1917
Major applicationsEngineering Division TW-1
Number built52
VariantsLiberty L-4,Liberty L-8,Liberty L-12

TheLiberty L-6 was a six-cylinderwater-cooledinlineaircraft engine developed in the United States duringWorld War I.

Design and development

[edit]
Fokker D.VII with Liberty L-6 engine fitted for trials

The Liberty L-6, which developed 200–215 hp, was built by theThomas-Morse Aircraft Corp. andWright Aeronautical Corp. Since it was based on the same engine design as the more successfulLiberty L-12V-12 liquid-cooled aviation engine, the L-6's resemblance to theMercedes D.III German aviation engine, the source for the Liberty V-12's own cylinder and valvetrain design, resulted in the American L-6 engine design bearing a close visual resemblance to the German straight-six aviation powerplant in a number of respects, with at least one L-6 even being mounted postwar into a capturedFokker D.VII fighter for testing in the US. The Liberty L-6's smaller displacement of some 825 cu. in. (13.5 liters) versus the late-war German Mercedes D.IIIaü's 903 cubic inches (14.8 liters) do not seem to have handicapped the American straight-six design, however, as the "Liberty Six" possessed a 5.42:1CR, while the D.IIIaü had only a 4.64:1 CR, explaining a good bit of the American powerplant's output level—in addition to the 735.5 watt level for GermanPferdestärke metric horsepower, versus the then solely-American-basedSAE organization's standard of almost 746 watts per one horsepower.

Since the L-6 was too large for mail airplanes and other engines were available, the L-6 was canceled after only 52 had been built. In 1920 10 more L-6 engines were ordered, designated L-825, several of which were installed in theCurtiss PN-1, (only two built), and theEngineering Division TW-1, (only six built).

Hall-Scott also produced a six-cylinder engine using Liberty L-12 components, as theHall-Scott L-6.

Specifications

[edit]
Rear view of restored Liberty Six engine

Data fromU.S. Army Air Service Information Circular – Performance Test of Fokker D-VII with Liberty Six Engine

General characteristics

Components

Performance

  • Power output: 215 hp (162.6 kW) @ 1,700 rpm
  • Compression ratio: 5.42:1
  • Fuel consumption: 0.49 lb/HP-hour
  • Oil consumption: 0.0256 lb/HP-hour

See also

[edit]

Comparable engines

Related lists

References

[edit]
Wikimedia Commons has media related toLiberty L-6.

This article incorporates text fromLiberty L-6, a public domain work of the United States Government.

  • Gunston, Bill (1986).World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 106.
Piston engines
Retrieved from "https://en.wikipedia.org/w/index.php?title=Liberty_L-6&oldid=1145212185"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp