The Liberty L-6 was a six-cylinder water-cooled inline aircraft engine developed in the United States during World War I.

Liberty L-6
Liberty L-6 aircraft engine on display at the National Museum of the United States Air Force
Type	Piston aero engine
National origin	United States
Manufacturer	Wright Aeronautical, Thomas-Morse Aircraft
Designed by	Jesse G. Vincent and Elbert J. Hall
First run	about 1917
Major applications	Engineering Division TW-1
Number built	52
Variants	Liberty L-4, Liberty L-8, Liberty L-12

Design and development

The Liberty L-6, which developed 200–215 hp, was built by the Thomas-Morse Aircraft Corp. and Wright Aeronautical Corp. Since it was based on the same engine design as the more successful Liberty L-12 V-12 liquid-cooled aviation engine, the L-6's resemblance to the Mercedes 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 captured Fokker 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 5.42:1 CR, 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 German Pferdestärke metric horsepower, versus the then solely-American-based SAE 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 the Curtiss PN-1, (only two built), and the Engineering Division TW-1, (only six built).

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

Specifications

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

General characteristics

• Type: Six-cylinder inline piston engine
• Bore: 5.00 in (127 mm)
• Stroke: 7.00 in (177.8 mm)
• Displacement: 824.67 in³ (13.51 litres)
• Dry weight: 567.5 lb (257.4 kg)

Components

• Valvetrain: SOHC (Single overhead cam)
• Fuel system: Twin updraft Stromberg N.A.-S5 carburetors
• Cooling system: Water-cooled

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

Comparable engines

• Austro-Daimler 6
• BMW III
• Hiero 6
• Mercedes D.III
• SPA 6A

Related lists

• List of aircraft engines

References

Wikimedia Commons has media related to Liberty L-6.

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

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

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