RedMercury
Junior Member
Perhaps part of the answer is the name. Note it is not WS-10, but FWS-10. I wonder what the F stands for.
When I first joined this forum the first thing I posted about was the different number of static vanes in the WS-10 engine from that billboard at the 2006 Zhuhai airshow and the one that was on
display at the 2008 airshow.
The billboard photo of the WS-10 in 2006 had 15 static vanes.
Two years later (after design certification) it had 17 static vanes.
The engine in the photo above only has 15, so this engine is a pre-2008 design.
In fact, there are a lot of differences between this engine and the 2008 WS-10a. Perhaps this is the pre-2006 WS-10?
Good news. Just as what u wanted.
"It mention it is an local develop advance turbofan which priority will be equipping J-10. It can also equip J-11B. Presently , it has enter mass produced phase."
More or less, we will see J-11B chunk out like hot cakes soon and J-10a start using WS-10A.
This is not the engine that was displayed in 2008. It has many differences.
I think FWS-10(a) is the official designation. WS-10(a) is just the shortened and more common name.
I wouldn't doubt that some of WS-10a's technology comes from the AL-31F/CFM-56.
But these engines are notably different. That is what is confusing.
Actually, the more I think about it, the more I think that the differences we are seeing might have something to do with the plane that each engine is designed for. After all, the J-11's have AL-31F and J-10's have AL-31FN's. They are both the same engine, but modified to suit specific needs. How can the WS-10a suit the needs of two types of aircraft? The engines would need to have modifications, and thus have different designations to distinguish them.
I know its not likely, but is it possible that WS-10 is the name of the engine for the J-11B and WS-10a is for J-10?