Dongan WJ-5: Difference between revisions
Appearance
Content deleted Content added
No edit summary |
m →top: Removed overlinked country wikilink and general fixes (task 2) |
||
(17 intermediate revisions by 13 users not shown) | |||
Line 1: | Line 1: | ||
{|{{Infobox |
{|{{Infobox aircraft begin |
||
|name = |
|name = WJ-5 |
||
|image = Xian Y7 Air Changan B-3475 PEK March 1997.jpg |
|||
|image = |
|||
|caption = A Xian Y-7-100 powered by Dongan WJ-5 turboprop engines |
|||
|caption = |
|||
}}{{Infobox Aircraft Engine |
}}{{Infobox Aircraft Engine |
||
|type=Single-shaft [[Turboprop]] |
|type=Single-shaft [[Turboprop]] |
||
Line 12: | Line 12: | ||
|} |
|} |
||
The '''Dongan |
The '''Dongan WJ-5''' is a Chinese single-shaft turboprop aero engine built by the [[Dongan Engine Manufacturing Company]] for the [[Xian Y-7]] twin-engined transport. |
||
==Variants== |
==Variants== |
||
;WJ-5A |
|||
;WJ5A |
|||
:Main production variant of 2162 ekW (2900 ehp)<ref name="Taylor563">Taylor 1996, p 563</ref> |
:Main production variant of 2162 ekW (2900 ehp)<ref name="Taylor563">Taylor 1996, p 563</ref> |
||
;WJ-5E |
|||
;WJ5E |
|||
:Improved variant for the [[Xian Y-7|Xian Y-7-200]] sometimes referred to as the |
:Improved variant for the [[Xian Y-7|Xian Y-7-200]] sometimes referred to as the WJ-5A-1G.<ref name="Taylor563" /> Developed with the help of [[General Electric]]<ref>{{cite web | title=Dongan | url=http://www.flightglobal.com/articles/1996/10/09/9434/dongan.html | publisher=Flight International | date=9 October 1996 | access-date=2009-06-13}}</ref> |
||
;WZ-5 |
|||
;WZ5 |
|||
:A turboshaft version of the |
:A turboshaft version of the WJ-5, which failed to progress beyond the prototype stage. |
||
==Application== |
==Application== |
||
Line 27: | Line 27: | ||
==References== |
==References== |
||
===Notes=== |
===Notes=== |
||
{{reflist}} |
{{reflist}} |
||
Line 32: | Line 33: | ||
===Bibliography=== |
===Bibliography=== |
||
{{refbegin}} |
{{refbegin}} |
||
*{{cite book |
*{{cite book|last= Taylor|first= Michael J. H.|title= Brassey's World Aircraft & Systems Directory|year= 1996|publisher= Brassey's|location= London, England|isbn= 1-85753-198-1|url-access= registration|url= https://archive.org/details/brasseysworldair0000unse}} |
||
{{refend}} |
{{refend}} |
||
{{People's Republic of China military aeroengines}} |
{{People's Republic of China military aeroengines}} |
||
{{aviation lists}} |
|||
[[Category: |
[[Category:1970s turboprop engines]] |
Latest revision as of 14:03, 7 January 2022
WJ-5 | |
---|---|
A Xian Y-7-100 powered by Dongan WJ-5 turboprop engines | |
Type | Single-shaft Turboprop |
National origin | China |
Manufacturer | Dongan Engine Manufacturing Company |
Major applications | Xian Y-7 |
The Dongan WJ-5 is a Chinese single-shaft turboprop aero engine built by the Dongan Engine Manufacturing Company for the Xian Y-7 twin-engined transport.
Variants
[edit]- WJ-5A
- Main production variant of 2162 ekW (2900 ehp)[1]
- WJ-5E
- Improved variant for the Xian Y-7-200 sometimes referred to as the WJ-5A-1G.[1] Developed with the help of General Electric[2]
- WZ-5
- A turboshaft version of the WJ-5, which failed to progress beyond the prototype stage.
Application
[edit]References
[edit]Notes
[edit]Bibliography
[edit]- Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.