wild speculation: a have a hypothesis that ws15 may be a 2-2,5 ton engine (russian way of measuring engine weight- western way) with a diameter of around 1,4 or so meters. And that current j20 are flying with structural interface between engine and inner fuselage (ballasts) around al31 to simulate the extra weight distribution.
There is little doubt that the J-20 has been designed around the dimensions of the larger engine, but it is unlikely that the prototype carries extra ballast, as it is NOT fitted out with all the heavy radar and fire control equipement that is located forward, when the WS-15 is installed it will likely be on an LRIP aircraft rather than one of the prototypes. brat