Bill Jepson
No doubt that Tracy could design a injection system that
uses a mass flow sensor - after all, as you know, the system only
wants to know (and doesn't care how) how much air mass is in the
combustion chamber in order to determine the fuel to meet your desired A/F
ratio.
However, unless there was some significant market
demand for such, I doubt it would be worth his investment to do so. I
have not given it any thought, but there might be reliability/safety issues
using a air mass flow sensor vice a manifold pressure sensor in aircraft
application.
For one thing it would be a bit more of a hassle to
have two air flow sensors (for redundancy) spacewise and perhaps plumbing
wise (air) than with the two pressure sensor. -The pressure sensor can be
stuck any place including inside the EC2 box in the cockpit area with just
two small hoses running to them - not so with two air mass flow
sensors.
The Alpha-N system based on Throttle position and rpm
might be more suitable, but as Bill indicated the fuel map might be
more complex as there would be no direct indication of engine load such as
manifold pressure or air flow would give. Another challenge would be
to have a Throttle position sensor which would be compatible with all the
variety of TB that folks use.
So it certainly could be done, but unless there was
some market demand for it, I don't foresee it coming.
Just my 0.02 worth and I certainly don't speak for
Tracy
Ed
Ed