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Fuel system thoughts and questions
Since it is pretty easy to have issues with cavitation/air bubbles, etc. with long suction lines in our fuel systems, would it not be a good idea to locate the fuel pump close to or even in the tanks? This way the pump would push the fuel instead of pulling it. The advantage I can see doing it this way is the fuel would always be under positive pressure eliminating the cavitation/air bubble problem. Modern cars are plumbed this way with their fuel pumps located in the gas tank. Since I'm new to turbine-powered airplanes, I've been searching through old posts trying to get up to speed on these beasts, and it seems that the fuel systems cause their fair share of grief. I realize that an in-tank pump idea would require a redesign of the pump, but the close-to-the-tank idea seems plausable to me. What are your thoughts?
Thanks, Luckyflyer |
RE: Fuel system thoughts and questions
If you use 6mm O.D (4mm I.D) pvc tubing up to the pump and make sure all the tank fittings, clunks and tubing are also 4mm I.D you won't go far wrong. The only time I would be happy to have a bore less than 4mm is either when I use a small engine or I have two parallel tanks of the same size feeding a hopper which has a 4mm I.D feed to the UAT.
Jason |
RE: Fuel system thoughts and questions
I don't see a sumberged pump as practical, and I don't think cavitation is a common issue with large fuel lines, but u may be on to something when u suggest putting the pump next to the tank, eliminating the UAT as a possible cavitator.
One would have to use something more substantial than a simple plug to cap the line used for fueling though ! Interesting idea. Oops, just thought of a problem. One had best use a rigid UAT, lest the thing cause response lags as it expands/contracts under varied pump pressures. |
RE: Fuel system thoughts and questions
ORIGINAL: highhorse One would have to use something more substantial than a simple plug to cap the line used for fueling though ! |
RE: Fuel system thoughts and questions
ORIGINAL: luckyflyer ORIGINAL: highhorse One would have to use something more substantial than a simple plug to cap the line used for fueling though ! |
RE: Fuel system thoughts and questions
Most jets have a shut off valve to use in an emergency & there was some discussion in another thread on whether the valve should go on the suction or discharge side of the pump.
The main objection to the valve being on the discharge side of the pump was the valve & fuel lines would be subject to the considerable pressure fuel pumps are capable of generating & the risk of a line or fitting bursting spraying fuel everywhere. With what you are proposing the entire fuel system would have to withstand this pressure. As Jason said, a lot of work has gone into the current system & the bugs are pretty well ironed out, lessons learnt the hard way mostly. But new ideas are always welcome! :D Since I'm new to turbine-powered airplanes |
RE: Fuel system thoughts and questions
The pressure problem could be solved by adding a by-pass to the shut-off valve, this would return the fuel to the main tank without stressing the system.
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RE: Fuel system thoughts and questions
ORIGINAL: Boomerang1 Most jets have a shut off valve to use in an emergency & there was some discussion in another thread on whether the valve should go on the suction or discharge side of the pump. The main objection to the valve being on the discharge side of the pump was the valve & fuel lines would be subject to the considerable pressure fuel pumps are capable of generating & the risk of a line or fitting bursting spraying fuel everywhere. With what you are proposing the entire fuel system would have to withstand this pressure. As Jason said, a lot of work has gone into the current system & the bugs are pretty well ironed out, lessons learnt the hard way mostly. But new ideas are always welcome! :D Since I'm new to turbine-powered airplanes |
RE: Fuel system thoughts and questions
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What we are using currently when done right works perfectly. It is easly to do PM on the system as well as the install is pretty straight forward. I have over 200 flights and never a hickup from fuel delivery. Don't need to re-invent the wheel here. A clean install really makes the differance.
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RE: Fuel system thoughts and questions
But the two scenarios are different, right? Then there's no 'relief', the pump would be pushing against the second tank & the UAT if fitted. The first (main?) tank is, of course, vented. - John. |
RE: Fuel system thoughts and questions
Lots of fuel.... Electricity.....
I keep the pump close to the engine. All electricity well away from the fuel. I rather spend more time dealing with cavitation then with a fire hazard. |
RE: Fuel system thoughts and questions
Given that most of the cavitation issues mentioned in the recent thread on the topic occur at the UAT...I think the idea has merit, and that someone (else) should give it a try :-)
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RE: Fuel system thoughts and questions
ORIGINAL: highhorse Given that most of the cavitation issues mentioned in the recent thread on the topic occur at the UAT...I think the idea has merit, and that someone (else) should give it a try :-) Mike |
RE: Fuel system thoughts and questions
ORIGINAL: BaldEagel ORIGINAL: highhorse Given that most of the cavitation issues mentioned in the recent thread on the topic occur at the UAT...I think the idea has merit, and that someone (else) should give it a try :-) Mike |
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