In the PPT, the moon version does not have escape tower, but the LEO version does.921 rocket now called CZ-5DY. Latest design appears to have no launch abort tower compared to previous. I'm guessing it's integrated into the new space capsule?
I don't always trust too much of the PPT even if it is presented by Long Lehao. I have seen many apparent inconsistencies in PPTs from CASC. They seems to not bother too much of it. For example, in the new PPT, LH/LO 2nd stage of CZ-9(11) is open cycle engine, but the recent announced test was close cycle staged engine.
Regarding the abort system of the moon version, we need to remember that the spacecraft is the same as the LEO version using the same propulsion rocket. The rocket's acceleration characteristic remains the same. If the LEO version has to use escape tower, the moon version has to do the same.