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Contents

   



(Top)
 


1 Applications  





2 Specifications (Neptune I)  



2.1  General characteristics  





2.2  Components  





2.3  Performance  







3 See also  





4 References  



4.1  Notes  





4.2  Bibliography  
















Bristol Neptune






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From Wikipedia, the free encyclopedia
 


Neptune
The Bristol Neptune
Type Radial aircraft engine
Manufacturer Bristol Aeroplane Company
First run 1930
Major applications Bristol Type 110
Developed from Bristol Titan

The Bristol Neptune was a seven-cylinder air-cooled radial engine developed in 1930. It had the same size cylinders as the earlier Mercury and Titan engines, 5.75 in (146 mm) x 6.5 in (165 mm) which gave a displacement of 1,182 cu in (19.3 L) and produced a maximum of 320 horsepower (239 kW). The Neptune was effectively a seven-cylinder version of the Titan.[1]

Applications

[edit]

Specifications (Neptune I)

[edit]

Data from Lumsden. [1]

General characteristics

Components

Performance

See also

[edit]

Related development

Comparable engines

Related lists

References

[edit]

Notes

[edit]
  1. ^ a b Lumsden 2003, p.103.

Bibliography

[edit]
  • Lumsden, Alec. British Piston Engines and their Aircraft. Marlborough, Wiltshire: Airlife Publishing, 2003. ISBN 1-85310-294-6.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Bristol_Neptune&oldid=1018265435"

Categories: 
Aircraft air-cooled radial piston engines
Bristol aircraft engines
1930s aircraft piston engines
Hidden categories: 
Articles with short description
Short description matches Wikidata
Use dmy dates from December 2016
Use British English from December 2016
 



This page was last edited on 17 April 2021, at 03:53 (UTC).

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