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{|{{Infobox Aircraft Begin
{|{{Infobox aircraft begin
|name = WJ-5
|name = WJ-5
|image = Xian Y7 Air Changan B-3475 PEK March 1997.jpg
|image = Xian Y7 Air Changan B-3475 PEK March 1997.jpg
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|}
|}


The '''Dongan WJ-5''' is a [[China|Chinese]] single-shaft turboprop aero engine built by the [[Dongan Engine Manufacturing Company]] for the [[Xian Y-7]] twin-engined transport.
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==
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: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
;WJ-5E
: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 | work= | publisher=Flight International | date=9 October 1996 | accessdate=2009-06-13}}</ref>
: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
;WZ-5
:A turboshaft version of the WJ-5, which failed to progress beyond the prototype stage.
:A turboshaft version of the WJ-5, which failed to progress beyond the prototype stage.
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==References==
==References==

===Notes===
===Notes===
{{reflist}}
{{reflist}}
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===Bibliography===
===Bibliography===
{{refbegin}}
{{refbegin}}
*{{cite book |last=Taylor |first= Michael J. H.|authorlink= |coauthors= |title= Brassey's World Aircraft & Systems Directory|year=1996 |publisher= Brassey's|location= London, England |isbn=1-85753-198-1|pages=}}
*{{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:Turboprop engines 1970–1979]]
[[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]
  1. ^ a b Taylor 1996, p 563
  2. ^ "Dongan". Flight International. 9 October 1996. Retrieved 2009-06-13.

Bibliography

[edit]
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