So you still don't understand.
ok.
There are a lot of assumptions made in the premise. VGs have their applications but aren't a magic panacea to all things airfoil related. You don't see VGs on Mooney / Lancair / Cirrus / Gulfstream / Citation X / etc. wings.. You seem them on STOL equipped planes, and their primary job there is to aide in the slow and high AoA environments. They also aren't magically tightening the airflow, all they do is create a small vortex that goes down the "wing" - it takes energy to "spin" the air up like that.. that's got to come from somewhere. There's a big assumption to be made that the energy it takes to "charge up" the air like that does enough drag reduction to make the whole thing worth it
the whole thing with this prop VG is an assumption that it adds enough aerodynamic efficiency to gain 50 static RPM and an increase in cruise speed
The OP asked if we thought it was snake oil... I'm dubious of the overall idea that prop VGs are meaningful, primarily because, out of all the efficiency gains people seek out of their planes and advances we've seen in prop design, composites, etc., we don't see anyone doing this, and like the other poster said, they've been around for a long time
*However, I am not part of an anti-prop VG lobby, and don't really care one way or the other. If people want to drop money on putting tape on the leading edge of their props more power to them
PS - the FIKI and non FIKI Cirrus don't have any different published cruising speeds (assume same conditions, etc.).. however the FIKI Cirrus has a fairly aggressive rubber liner going down the front first third of the blade with deep grooves in it for TKS channels. I would imagine if this was as sensitive of an airfoil area as it is claimed to be, we'd see different published performance figures for planes with and without the prop FIKI