What's not clear is how the linkage still connects to the flight controls. The idea seems to be that the one which is moving wins. What is clear is that, if your side becomes disconnected, your yoke doesn't do anything. No wonder one pilot was frantic. It seems that you get reconnected by moving the disconnected yoke to agree with the one in control. Then the pin falls into the notch and the yokes are connected again. Not sure about that. You can see the pin and notch in the patent drawings.
This is independent of the fly-by-wire system. That's downstream from these mechanical devices.
I wonder if pilot training includes knowledge that yoke disconnection is possible.
Probably, I've heard https://www.youtube.com/c/MentourPilotaviation talk about it as well.
That still leaves the question of how to interpret opposing inputs for the physical control surfaces, though
Here's an article stating exactly that: https://english.alarabiya.net/News/world/2022/04/28/Pilots-p...
> If opposing forces on the two columns pass a certain limit, the link between them is deactivated or “desynchronized” to prevent accidents in the case of one side getting jammed.