Hello Paul,
I am trying to determine the size of the return lines and volume of fuel
returned as I plan for my EFI 13B. I may have to create a header tank to
handle
the return and the question is, how big does it have to be? Any rules of
thumb?
Thanks,
William Hagood
Most people use AN6 lines for fuel.
The volume of fuel returned will be inversely proportional to the HP
being generated. At idle and taxi it could be 80% of the fuel
pumped. So the header tank will fill rapidly. The question then
becomes what do you do with the header tank overflow?
At take off and climb the fuel pumped is a max so the flow to the tank
may be as little as 10 to 20 percent of the fuel pumped.
Done wrong fuel can be pumped over board in short order through
the tank vents.
The traditional and safest way is use 2 tanks and a two level
valve and send the return fuel to the tank it is pumped from.
A header tank, if used should be able to flow fuel back
into the tank it came from. One gallon should be sufficient.
Defective fuel systems are a major cause of engine
stoppage and crashes. Particularly in low wing airplanes.
They are tricky to design and they appear simple but are tricky
to do right. The lowly vent system design is very important.
One of the big mistakes is pointing the vents in the
direction of flight as dynamic pressure above 100 MPH
will push the fuel out of the tank in a direction
you may not want it to go. That is the same pressure fed
to the air speed indicator by the pitot tube.
Another mistake is having the vent lines coming out below
the level of the fuel causing a siphon under certain
circumstances.
A third mistake is using a LEFT, RIGHT, BOTH & OFF
fuel selector valve on a low wing airplane.
Low wing airplanes should use only a LEFT, RIGHT & OFF
fuel selector valve.
The best and safest way is to copy certified aircraft
fuel injection systems if possible.
Paul Lamar
Paul,
The engine test stand you will get has an automotive tank with submerged
fuel pump, just as it came out of the car, no return, so you will get an
opportunity to see how that works. One of the last things that we were
adjusting was fuel pressure with the engine running, you may have to tweak
that a little. milo
OK Milo, We can handle it. No worries mate.
Paul Lamar
Copyright 1998-2010 All world wide rights reserved.
I'm confused. For the return fuel to exceed the capacity of the header tank,
more fuel would have to be introduced to the header tank. Example, worst
case scenario, if the engine is not running and the fuel pumps are on, isn't
all of the fuel that is going out of the header tank being returned to the
header tank through the fuel rail? Thus the net result in fuel is a wash and
no overflow....right? If the engine is running, then there is less fuel
being returned than is being pumped out....again no overflow. What am I
missing?
Sandy McNabb
Renesis in a Glass Goose
High mounted wing tanks are always easier to deal with.
Normally the high wing airplane type header tanks fill to the top
by gravity feed from both higher mounted Glass Goose wing tanks
so in your case everything is fine. Keep the header tank tall and
skinny. No double layer valves needed.
Run the header tank vent line up to the top of the cowl.
Perry Mick uses one header tank on his Long EZ but the bottom of the tank is
exposed to a cold blast of air. You may have fuel heating problems
when you get down to the last gallon or so in the header tank,
Paul Lamar
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