It look like the power turbine rpm can be regulated via throttle bodies at the bleed air ducts instead of using a constant speed drive at the gearbox unit, but I'm not sure what the benefits this system provides over an IDG since it introduces extra turbines and exhausts. Maybe they needed to keep the gearbox unit at the gas turbine as compact as humanly possible for some reason, or maybe this is just a patent for the sake of acquiring more patents? Is there a longer version of this paper or a discussion over some Chinese mechanical forum that we can translate and learn more from? I tried to look for info on it online without much luck. Wikipedia does say that early aircraft used bleed air and turbines for electrical power, but the reference link is long gone so I can't make the differences between the two systems.