According to some not entirely reliable sources, the reason UADF did not adopt 2D TVC is due to the lower reliability of a single engine compared to dual engines. I think this explains why we see it on the J-XDS but not on the UADF. I believe that as reliability improves, we will see it in subsequent batches of test aircraft.
Potentially due to the ability of UADFs to be more attritable (if not expandable) than manned platforms (even at comparably lower degrees for high-tier UADFs versus mid/low-tier UADFs) as well.
The more sophisticated and expensive a platform becomes, the less capable it is for the operator (in this case, the PLAAF) to accept attrition of such platforms due to the inherent cost, effort and resource consumption challenges from its development, procurement and deployment.
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