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Fuel Flow Discussion, Moved from Float Mounting
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The one that Mark sells has 1/4 NPT ports on it. 1/4 NPT is what about every fuel selector I've seen is to.
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Yes, I think it's the gaskelater. I'll be looking into the one Mark sells and checking port size
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Are you using a gascolator? Looking at how restrictive they are I've been wondering if that's why folks aren't seeing a difference between single tank and BOTH fuel flow rates.
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I was also expecting more flow on Both. Possibly something after the fuel valve restricts more flow on Both. One Pump on, I have 43 gph. I ran the motor, all four injectors working and WOT, tied to my truck (brakes won't hold it) with no issues other than some fine tuning. It really barks now.
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The 15 gph was the last 5 gal. that emptied the tanks. I have no intentions of letting the tanks get that low. It was just interesting that the flow was less.
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Please clarify......I think you were doing a fuel flow test. And I think your GPH figures is a calculation of volume of fuel flowing into a bucket divided by time.
When you got the 15 GPH result, is it possible that you had uneven fuel levels in the two tanks?
I wonder........
1) When the tank levels are not even the fullest tank has the highest fuel pressure at the TEE of the fuel selector.
2) When the two tanks are interconnected when you select BOTH, then the differential pressure between the two tanks will want to equalize and fuel will cross feed through the fuel valve.
3) It seems to me that any flow across the TEE will reduce flow to the engine.
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Normally more fuel flow is seen with a BOTH setting. That has been my experience in all my planes. Not sure why you would not see that also Elden. Mark
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Today I put 10 gallons in each tank for a total of 20.
at the pump inlet on Both, I had 23 GPH. Switch to left tank only, 23 GPH. Right tank only, 23GPH. I then went back to Both, the remaining 5 gallons was 15 GPH. Not sure why, head pressure I would guess. Previously I had only checked right and left, not both or both with near empty fuel.
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Originally posted by alaskabearhawk View PostCessna has a pretty elaborate venting system with check valves in the tanks, Vents going from outboard tank to opposite tank outboard side, etc, etc. The one issue I can see with interconnecting the tanks inboard is if you parked on a slope with full tanks. The tanks would be in essence one tank. With full tanks the downslope tank has a hole in it, namely the fuel cap vent. Mean ol' Mr. Gravity would have his way and the fuel would flow out of the downslope cap. The only way to mitigate that with the tanks interconnected like that is to install an inline valve in the interconnecting vent line and turn it off when parked. However, one more thing to remember to turn on and a potential point of failure.
I think parking on a slope is a strange enough event, that I always think "I better close that valve", and I have never lost fuel yet. I do lose fuel to freshly filled tanks on hot days though.
I can imagine, were I under a lot of stress or very distracted, I could forget to select the fuel to "off". But for normal ops, it has proven to be an insignificant risk for me personally.
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Yeah, more complex, but sounds like Cessna's is as well. They have been doing this for a long time and have discovered all kinds of Gremlins over the years.
The other option might be to try to figure out how to put a vent pipe internally in the tank to the upper/outboard end, from the inboard side. Lots of tanks of have internal piping for many different purposes, including venting. "Standpipes" are a pretty common feature.
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Cessna has a pretty elaborate venting system with check valves in the tanks, Vents going from outboard tank to opposite tank outboard side, etc, etc. The one issue I can see with interconnecting the tanks inboard is if you parked on a slope with full tanks. The tanks would be in essence one tank. With full tanks the downslope tank has a hole in it, namely the fuel cap vent. Mean ol' Mr. Gravity would have his way and the fuel would flow out of the downslope cap. The only way to mitigate that with the tanks interconnected like that is to install an inline valve in the interconnecting vent line and turn it off when parked. However, one more thing to remember to turn on and a potential point of failure.
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Really nice video. I already had a couple of bungs welded to the inboard side of the tanks to use as fuel return ports. I added a header tank and want to use them for vents for the header tank, and to cross vent the tanks.. After looking at a bunch of fuel system designs I noticed Cessna had a preference for venting the tanks from the outboard side, vs the inboard. With only 1 degree of dihedral, this is only a very slight difference in height on the outboard. Obviously, higher is better, but in the case it isn't much.
Is there any other advantage to using the outboard location for the vents? I wonder if I could run a vent line internally in the tank, to the outboard edge of the tank, to the high point.
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Yep, I agree. The front rib lightening holes are relatively easy to access so that shouldn’t be a problem to retrofit later.
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