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There is another phenomina that exists that would
be very subtle. People can design fluid flow 'flip-flop' circuits, that will
take two streams that merge into one outlet, and can make them draw from either
side with the momentary application of a side pressure. Once started, the flow
continues from the given side until it is purposely reversed. I can envision
(but don't know how to design) a situation where there is a subtle difference
that encourages that behavior.
Bill Schertz KIS Cruiser # 4045
----- Original Message -----
Sent: Thursday, February 24, 2005 9:35
PM
Subject: [FlyRotary] Re: Vapor Lock
Paul, Paul wrote:
Hi, Jim....is it
possible there is a restriction in one of the fuel lines? Are there any
bends in the aluminum fuel line that might have kinked during the bending
process?
This problem drove me NUTS for
two years. I tried everything. For example, I checked the vents as
best I could, leveled the airplane (checked the ball to ensure it was centered
- it was), disconnected the fuel line from the engine side of the firewall and
let it drain into a bucket. I turned off one strake at a time (with
manual maintenance valve) and timed how long it took for the other strake to
gravity drain ten gal of fuel into the sump, out of the sump through the boost
pump, through the filter and then through the firewall into the
bucket(s). Then I turned it off and did the same thing with the left
tank. They both drained 10 gal each within 5% of the same
time. Then I reconnected all the plumbing, taped over the fuel caps so
there's no possible way they could leak and went flying. Right tank
drained 20 gal while the left tank maybe 2 or 3. Level balanced flight
on a cross country. All fuel lines, vent lines, etc. are as identical as
I am able to make them. To this day, I've not met anybody who can
explain what happened. I tried everything. Back and forth
on the Velocity list much longer than you've been inquiring after your vapor
lock. NOTHING. I figured out a workaround - I installed electric
shutoff valves in place of the manual maintenance valves between the strake
and the sump. Now, when one tank doesn't transfer, I turn off the tank
that does and let the "reluctant" tank catch up. The pump sucks it
through the system just fine (the head pressure of 6" of fuel is about 0.16
psi - a problem that would inhibit that flow you can't even MEASURE.
Assymmetric transfer is common as dirt in the Velocity community (but not
nearly as persistent as mine). It was also a problem a long time with
the Vari-EZ.
Lastly, have you tried
blowing backwards into the two fuel lines to see if either had more
restriction than the other? Just looking for possible reasons for your
uneven fuel flow. Even my Cessna 172 and 150 had fairly even fuel
consumption from the two gravity fed tanks.
I understand that Cessnas had a lot of trouble around this
too.
Just searching for
answers. Paul Conner
----- Original Message ----- From: "Jim
Sower" <canarder@frontiernet.net>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Thursday, February 24, 2005 5:57 PM Subject: [FlyRotary] Re:
Vapor Lock
In my Velocity the strakes gravity feed to the
sump. About a foot of 3/8" Al / rubber fuel line on each side, downhill
all the way. I can run one tank plumb dry and have only a gallon or two
gone out of the other. Like when there's a slight leak in a fuel cap or
something. If they're significantly uneven, you WILL get air if you
select "Both" ... Jim S.
Bulent Aliev wrote:
If you're almost home and have "Both" selected, and one
tank runs dry, what do you end up with in the fuel line? I
believe mostly air. Late in the trip (traffic pattern?)
where trouble shooting time is at a premium. Use L or R.
Not B.
I don’t think so: connect two tanks (one full with water
and one empty) to gravity feed Into Y connection. Than suck on the end
and try to breathe. Let me know how it works :) Buly
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