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 Variants  





3 Applications  





4 Specifications (Titan I)  



4.1  General characteristics  





4.2  Components  





4.3  Performance  







5 See also  





6 References  



6.1  Notes  





6.2  Bibliography  
















Bristol Titan






Español
فارسی
Italiano
Русский
 

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
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


Titan
The Bristol Titan
Type Piston aero engine
Manufacturer Bristol Aeroplane Company
Designer Roy Fedden
First run c.1928
Major applications Avro 504N
Bristol Primary Trainer
Developed into Bristol Neptune

The Bristol Titan was a British five-cylinder air-cooled radial engine, designed and built by the Bristol Aeroplane Company in the late 1920s. It had the same size cylinders as the earlier Bristol Mercury engine, 5.75 in × 6.5 in (146 mm × 165 mm) (displacing 844 cu in (13.83 L)), and produced between 200–240 hp (150–180 kW). Later versions of the Bristol Titan also used a Farman-style reduction gear produced by Gnome-Rhône.

Design and development[edit]

The engine was designed as a five-cylinder radial, to use as many parts of the Bristol Jupiter as possible. Cylinders, pistons, articulated connecting rods, crankshaft and other minor parts were interchangeable with the Jupiter.[1]

The major significance of the Titan was that it was licensed to Gnome-Rhône and became the pattern for the Gnome-Rhône 5B and 5K. In 1927 Gnome-Rhône was looking for ways out of its licence agreement with Bristol for the Jupiter engine of 1920 and began to produce the Gnome-Rhône 5B and 5K without royalties.

Gnome-Rhône was not satisfied with simply producing Bristol designs under licence, and started a major design effort based around the mechanics of the Titan engine. The results were introduced in 1927 as the K-series, spanning the 260 hp (190 kW) Gnome-Rhône 5K Titan, the seven-cylinder 370 hp (280 kW) Gnome-Rhône 7K Titan Major, and the nine-cylinder 550 hp (410 kW) Gnome-Rhône 9K Mistral. With the introduction of the K-series, Gnome-Rhône finally ended royalty payments to Bristol, the Gnome-Rhône 5K being built in much greater numbers than the original Bristol Titan. By 1930 they had delivered 6,000 Jupiters, Mistrals and Titans, making them the largest engine company in France.

Variants[edit]

Titan I
(1928) - 205 hp (153 kW)
Titan IIF
Modified valve gear.
Titan II (Special)
Titan IV
(1928) - 205 hp (153 kW), 0.5:1 reduction gear from Bristol Jupiter.
Gnome et Rhône 5B
Gnome et Rhône 5Ba
Gnome et Rhône 5Bc
Gnome et Rhône 5K Titan
licence-built Titan II, 230 hp (170 kW)
Gnome et Rhône 7K Titan Major
enlarged seven-cylinder Titan with many detail improvements, produced by Gnome-Rhône without licence.

Applications[edit]

Specifications (Titan I)[edit]

Data from Lumsden.[2]

General characteristics

Components

Performance

See also[edit]

Related development

Comparable engines

Related lists

References[edit]

Notes[edit]

  • ^ Lumsden 2003, p.102.
  • 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_Titan&oldid=1218528583"

    Categories: 
    Aircraft air-cooled radial piston engines
    Bristol aircraft engines
    1920s aircraft piston engines
    Hidden categories: 
    Articles needing additional references from April 2018
    All articles needing additional references
    Use dmy dates from December 2016
    Use British English from December 2016
     



    This page was last edited on 12 April 2024, at 07:15 (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