<<<Norm,
I have some questions ...>>>
I understand why you have questions. Until I got one on the bench to do some testing, I wasn't really sure how they were plumbed and wired up. I have been through the factory where these valves are built, and talked to the people that designed them, but that was 10 years ago.
If you want a system with redundancy, three tanks, multi control modes, etc, you are going to end up with some level of complexity. I have a design with a reserve tank that can be switched in for last ditch, but everytime I mention it I get flamed with the complexity argument.
Here is the skinny-
If you fly a plane that doesn't return fuel, you can argue for days about common sump, valve type, and placement, and never come to consensus about the ultimate system.
If you choose to fly an engine that returns a significant amount of fuel, you must have a fuel managment scheme that allows for deaereation of the returned fuel, temperature dissipation, valving for return fuel, valving or some other tank selection criteria, plus all of the issues associated with the trivial non-return design in the previous paragraph. Propose any solution, and it will be attacked with arguments of complexity and non-reliability.
These forums are interesting and entertaining, but seem to be of minimal value for advancing the art of the design. Ultimately, the designer of the system needs to make their decisions, design, test, evaluate, and live with it. Looking for intelligent feedback from a forum group is like asking my flight physical doctor for feedback on my charging system design for the airplane.
The information that is of value comes from those people who have made an intelligent decision, have built it, and have pushed the state of the art forward. I apreciate how Tracy has put his system together, and how it has worked out. It is of 100 times greater information value than what the rest of us might sketch on napkins. Of course, 100 opinions are much easier to get than one flying example.
I suppose I could go find that valve selector and carve it open and do some motor stall tests. But I don't intend to fly with one, so I don't think I will go any further with that concept. I have offered to send the valve down to John for his enjoyment.
My fuel system is pretty much by the book, right up to the boost pump. I am running the Airflow Performance package which uses a scheme that is also debateable ad nauseaum. I just had the oil cooler lines and two fuel lines crimped up Saturday. $78 total. Dang that aircraft stuff is expensive. (Watch for the 666 lines and fittings on eBay soon!)
Regards-
Norm