Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Design and development  





2 Specifications  



2.1  General characteristics  





2.2  Components  





2.3  Performance  







3 See also  





4 References  














Liberty L-6






Italiano
 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 




In other projects  



Wikimedia Commons
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 

(Redirected from Hall-Scott L-6)

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
Designer 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

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

[edit]
Rear view of restored Liberty Six engine

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

General characteristics

Components

Performance

See also

[edit]

Comparable engines

Related lists

References

[edit]

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


Retrieved from "https://en.wikipedia.org/w/index.php?title=Liberty_L-6&oldid=1145212185"

Categories: 
1910s aircraft piston engines
Straight-six engines
Hidden categories: 
Articles with short description
Short description matches Wikidata
Commons category link from Wikidata
 



This page was last edited on 17 March 2023, at 20:49 (UTC).

Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



Privacy policy

About Wikipedia

Disclaimers

Contact Wikipedia

Code of Conduct

Developers

Statistics

Cookie statement

Mobile view



Wikimedia Foundation
Powered by MediaWiki