ChineseTiger1986
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What's WS-13E mentioned in the article?
Maybe an improved variant?
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What's WS-13E mentioned in the article?
Maybe an improved variant?
How much thrust ?
Maybe at least 100kN in afterburner thrust.
WS-13A is targeted to deliver 100kN in afterburner thrust.
I think 115-120kN is realistic for this engine which would be a generation ahead.
When will PLAAF be fully equipt with WS-10A, WS-10B, WS-15, WS-20s and this engine?
Until 2020 for the previous one, and after 2020 for this one.
This is the successor of WS-13, just like WS-15 to WS-10.
It will power for the late variant of J-31.
国家科技重大专项—高档数控机床与基础制造装备
I haven't heard of this before. How did the designation leak out so early?
I haven't heard of this before. How did the designation leak out so early?
What's WS-13E mentioned in the article?
"用户使用VMT80加工了包括用户使用VMT80加工了包括离心叶轮、XX17涡扇航空发动机风扇整体叶盘、某型轴流风机多种型号叶轮、XX13E涡扇航空发动机整体叶盘、某型涡轴航空发动机离心叶轮等多种零件。加工零件均满足设计精度指标要求,通过了用户验收"
What @ChineseTiger1986 's quote above has indicated because of the advancement in machinery (该课题完成了VMT80和VMT100两款4台样机的研制), tools and industrial tech it helps improve the precision in producing contrufugal impellers, fan blades etc