Seen some on Weibo claiming that the AEP500 = WJ-10, and we've also seen that the WJ-10 has 8 blades instead of only 6. Could this be a further development of the WJ-6 family, or some new type of turboprop engine that we may have seen somewhere that isn't related to both WJ-6 and WJ-10/AEP-500?
I believe this is the case. The aircraft is engine testbed to certify AEP-500. There is almost zero chance that it is related to WJ-6 because the much larger intake size and arrangement meaning air flow rate is vastly differnt, so are the compressors etc. etc., has to be a different engine.2. it could be the military variant of AEP-500 aka WJ-10.
The 8 blades concept was from PW150C, I believe that when AECC made their poster they took the same idea of propellers for AEP500. Anyway I think number of blades is not part of definition of an engine but part of aircraft.Seen some on Weibo claiming that the AEP500 = WJ-10.
Besides, a couple years ago, we've came across this poster by AECC(?) that the WJ-10 has 8 propeller blades instead of 6.
Could this be a further development of the WJ-6 family, or some new type of turboprop engine that we may have seen somewhere that isn't related to both WJ-6 and WJ-10/AEP-500?
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AEP-500 has 8 blades but military variant WJ-10 will also have 8 blades ?? this one nobody knows.
WJ-6C has over 3200KW maximum thrust
AEP-500 has 5000KW maximum thrust
this engine has to be somewhat AEP-500 related or completely new variant of WJ-6 family.. it couldn't be a totally new turboprop engine outside AEP-500/WJ-6 because this doesn't make sense..
I believe this is the case. The aircraft is engine testbed to certify AEP-500. There is almost zero chance that it is related to WJ-6 because the much larger intake size and arrangement meaning air flow rate is vastly differnt, so are the compressors etc. etc., has to be a different engine.
i have heard this AEP-400 engine but hardly any authentic information i get about this project. the biggest hurdle about ''Turboprop/Turboshaft'' is lack of authentic information due to nature of the project. when it comes engine news, turbofan stands tall.Saw some comments on Twitter and Weibo recently which suggested/claimed that the new engine seen on the Y8 testbed could be a derated version of AEP-500, known as AEP-400. Following the namesake, the AEP-400 will have a power output of 4000kW instead of 5000kW.
The AEP-400 is said to be meant for:
- Y-9; and/or
- KJ-600 (either).
Whereas the AEP-500 is said to be meant for:
- MA700;
- KJ-600 (either); and/or
- China's next-gen medium airlifter (namely Y-30)
Is this anywhere true/likely?
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