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Fuel System Manager

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911pete

Joined: 09 Aug 2018
Posts: 6

Posted: Thu Feb 19, 2026 9:57 am Post subject: Fuel System Manager

Hi



My airplane project requires a fuel system manager, or AFC (Auto Fuel Computer).  The System consists of 2 wing tanks and a center main tank.  The engine feeds from the main tank only.  It is a 28VDC system



The electrical components of the system are a High Pressure solenoid, 2 low pressure solenoids (1 for each wing tank), a high level sensor and a low level sensor.  2 3 position  switches (Off,Manual,Auto) and a low level or "bingo" light.  There is also a jet pump (non electrical) that uses high pressure fuel from the engine to "siphon" fuel from the wing tanks to the main tank.



All the solenoid valves are Normally Open and require power to close. The fuel level sensors are NC or Normally closed.  The planned sensors FU-ll25-03 from SMD Fluid Controls.  I have attached a copy of the data sheet.



LPFS is Low Pressure Fuel Solenoid

HPFS is High Pressure Fuel Solenoid

 



Auto Mode Single-  		

When the pilot selects the “Auto” mode on either transfer switch the fuel computer reads the level inputs from the fuel level sensors.  If the fuel is below the low sensor the AFC will remove power from that selected LPFS, allowing it to feed fuel into center tank.  It will continue this until the high sensor tells the AFC that the center tank is filled to its location.  At that point, the AFC will apply power to the selected LPFS to close it.  



Auto Mode Double-   		

When the pilot selects “Auto” mode for both transfers, both LPFS’s are controlled as above.



Manual Mode Single-    		

When the pilot selects either transfer in “Manual” mode then the selected LPFS will have no power and therefore be open.  The HPFS has no power any time that either LPFS has no power. 

  

Manual Mode Double-   	

When the pilot selects both transfers in “Manual” mode then both LPFS’s and the HPFS will have no power and therefore will be open. 



Off Mode Single-		

When the pilot selects one transfer switch into the “Off” position the selected LPFS will be powered closed.  No fuel will transfer from that wing.



Off Mode Double-		

When the pilot selects both transfer switches into the “Off” position then both LPFS’s and the HPFS will be powered closed.  This is the position for start up of the engine



Finally if there is an 20 second uninterrupted signal from the low level sensor the low level light is activated.



Originally this was operation was controlled by the use of a PLC (Programmable Logic Computer) system.  I can't get anyone to provide me with it.  Can a system like this be implemented using other means?



Any help would be appreciated



Pete

Ultrasonic Fluid sensor.pdf

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Last edited by 911pete on Thu Feb 19, 2026 3:17 pm; edited 2 times in total

user9253

Joined: 28 Mar 2008
Posts: 1951
Location: Riley TWP Michigan

Posted: Thu Feb 19, 2026 2:09 pm Post subject: Re: Fuel System Manger

What is the make and model of this aircraft?

Is it factory made or experimental?

Is the fuel gasoline or diesel?

What fuel pressure does the engine require?

Have you considered using a manual 4 position fuel valve; left, right, both, off?

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Joe Gores

911pete

Joined: 09 Aug 2018
Posts: 6

Posted: Thu Feb 19, 2026 2:18 pm Post subject: Re: Fuel System Manger

The airplane is a Viperjet, experimental.  The fuel is Jet-A.  There is a boost pump after the main tank to supply the fuel control and isn’t part of this system. This system is just to move fuel from the wings to the main tank. A manual fuel valve wouldn’t work in this application 



Pete

user9253

Joined: 28 Mar 2008
Posts: 1951
Location: Riley TWP Michigan

Posted: Fri Feb 20, 2026 8:08 am Post subject: Re: Fuel System Manager

Below are a couple of links to websites about the Viper Jet for anyone interested.



https://youtu.be/t_QnUYNVE-U



https://en.wikipedia.org/wiki/Viper_Aircraft_ViperJet

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Joe Gores

user9253

Joined: 28 Mar 2008
Posts: 1951
Location: Riley TWP Michigan

Posted: Fri Feb 20, 2026 9:42 am Post subject: Re: Fuel System Manager

Pete, I made a diagram of the Viper Jet fuel system based on my interpretation 

of your description.  It is unlikely that I got it right.  Please make corrections.  

Understanding how the system is supposed to work is the first step in designing 

the electrical fuel controls.

I used a very simple CAD program called Express.sch

Pete Viper Jet_.png

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Joe Gores

Last edited by user9253 on Fri Feb 20, 2026 9:51 am; edited 1 time in total

911pete

Joined: 09 Aug 2018
Posts: 6

Posted: Fri Feb 20, 2026 9:46 am Post subject: Re: Fuel System Manager

Ok, but I don’t see a diagram

911pete

Joined: 09 Aug 2018
Posts: 6

Posted: Fri Feb 20, 2026 10:07 am Post subject: Re: Fuel System Manager

Now I see it



Pretty close. The main tank is vented.  The fuel lines from the wing tanks go to the pump.  The pump is not electrical, it is a jet pump that uses high pressure fuel from the engine to create low pressure to draw fuel from the wings to the main tank. In your diagram the fuel would flow from the  wings through the pump to the main tank. Fuel also flows from the engine in your diagram through the solenoid (when open) and pump to the tank. The fuel supply to the engine isn’t depicted and doesn’t need to be. There are also one way check valves between the wing tank solenoids and the pump so fuel can only come out of the wing tanks. The main tank has a high and low level sensor to signal when the valves should open or close. The goal is to always keep the main tank full until the wings are empty



Pete

Eric Page

Joined: 15 Feb 2017
Posts: 263

Posted: Fri Feb 20, 2026 11:10 am Post subject: Re: Fuel System Manager

A few more questions:



1. With a vented main tank, can we assume that even in MANUAL mode, the Main Tank High Level sensor should close the LPFSs to prevent main tank over-filling and fuel loss via the vent?  Or, is the main tank vented to one or both wing tanks?



2. Is there: a) one jet pump, powered by the high pressure return line from the engine-driven pump and supplied by the two low pressure lines from the wing tanks, -or- b) two jet pumps, one in each wing tank, sharing the high pressure return?



3. If 2.a. is true, can the pump favor one wing tank over the other due to minor differences in head pressure?  If this happens, causing one wing tank to empty first and its fuel feed line to unport, will the jet pump suck air instead of fuel, making the fuel remaining in the other wing tank unusable?

911pete

Joined: 09 Aug 2018
Posts: 6

Posted: Fri Feb 20, 2026 11:52 am Post subject: Re: Fuel System Manager

1.  Yes I would want the high level sensor to close the LPFS to prevent overfilling. The tank is vented to atmosphere via a vent line exiting the bottom of the fuselage.



2. There is only want jet pump mounted in the cockpit with both wings feeding into it 



3.  The possibility exists for the tanks to feed unevenly. It is my understanding that if one tank is dry it would still feed from the other tank. If not then that tanks transfer switch could be placed in off with the other side in Manual or Auto which should close the LPFS for the empty tank. 



In the event of electrical failure all solenoids open since they are NO which would over fill the main tank to the point of venting but allow the main tank to remain full until all wing fuel is gone giving you time to land before fuel exhaustion

Eric Page

Joined: 15 Feb 2017
Posts: 263

Posted: Fri Feb 20, 2026 12:57 pm Post subject: Re: Fuel System Manager

OK, great.



Regarding the switches, I'm assuming they're SPDT toggles; if not, what are they?  Can you describe how they're wired?  Are all three terminals connected to the PLC, or is the common (middle) terminal connected to 28V or to ground?  Exactly which mode corresponds to each toggle position?



Maybe the wiring isn't done yet...  Is this a finished aircraft that's grounded due to fuel controller failure, or an in-progress build project?

911pete

Joined: 09 Aug 2018
Posts: 6

Posted: Fri Feb 20, 2026 1:19 pm Post subject: Re: Fuel System Manager

Your second thought is correct. This is a plane under construction. Viperjet ceased operations and I never got their fuel computer so no wiring is done, but I’m at that stage now.



I have all the parts except the “brain” to control them. 



Joe asked me to draw a fuel system schematic and he will make it pretty and post it. 



The switches are Honeywell 2TL1-10 and not wired up at all. Should I post the info on them?  As envisioned by Viperjet down is off middle is manual and up is auto.



Pete

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