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 Survivors  





5 Specifications (Potez 6D-02)  



5.1  General characteristics  





5.2  Components  





5.3  Performance  







6 See also  





7 References  














Potez 6D






Тоҷикӣ
 

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
 


Potez 6D
Potez 6D on display at Musée de l'Aviation de Lyon-Corbas
Type Six cylinder air-cooled inline piston engine
National origin France
Manufacturer Société de Avions et Moteurs Henry Potez
Major applications Morane-Saulnier Alcyon

The Potez 6D is a French six cylinder inverted inline aircraft engine put into production after World War II in normal and supercharged versions. Unsupercharged, it produced a take-off power of 179 kW (240 hp) at 2,530 rpm.

Design and development[edit]

In the 1930s Potez planned a series of new engines to replace their Anzani-derived radial engines. The Potez 4D, a four-cylinder inverted inline engine ran before World War II but did not reach production until the late 1940s, when it was joined by another inverted inline, the six cylinder 6D, and an eight-cylinder inverted-V, the Potez 8D. The D-series engines had much in common, most obviously sharing pistons and cylinders, with the same stroke, bore and valve gear. The inlines also shared connecting rods and lubrication systems and were offered in normally aspirated or supercharged versions.[1]

Variants[edit]

Data from Jane's All the World's aircraft 1956-57 pp. 430–1.[1]

6D-00
6D-02
Similar to 6D-30A without supercharger and 2x Hobson A1.55/j downdraught carburettors - 179 kW (240 hp) at 2,530 rpm
6D-30A
Supercharged version with a centrifugal blower (14.0:1 drive ratio) mounted horizontally on top of engine and with fuel injection, giving a normal power of 194 kW (260 hp) with 227 kW (305 hp) for take-off.
6D-30B
Supercharger drive ratio 15.5:1, 254 kW (340 hp) for take-off at 2,400 rpm.

Applications[edit]

Survivors[edit]

Specifications (Potez 6D-02)[edit]

Data from Jane's All the World's aircraft 1956-57 pp.430-1.[1]

General characteristics

Components

Performance

See also[edit]

Related lists

References[edit]

  1. ^ a b c Bridgman, Leonard (1956). Jane's All the World's Aircraft 1956-57. London: Jane's All the World's Aircraft Publishing Co. Ltd. pp. 430–1.
  • ^ Partington, Dave (201). European registers handbook 2014. Air Britain (Historians) Ltd. ISBN 978-0-85130-465-6.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Potez_6D&oldid=1126684029"

    Categories: 
    Potez aircraft engines
    1940s aircraft piston engines
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Commons category link from Wikidata
     



    This page was last edited on 10 December 2022, at 18:01 (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