ElectricSpidey
- Joined Dec 2, 2017
- 2,786
Load drivers sure are useful little buggers.
I've been using them as industrial-strength combinational logic since the 70'.Load drivers sure are useful little buggers.
HiHi Eric
I designed the circuit. You’re right - if there’s no AC input to the counter, and from there into the 555, it won’t latch. I designed it that way. But by starting the pump, via the relay, fuel will flow and the AC input will be activated.
The momentary switch manually activates the 555, and via the transistor, it closes the relay, which not only powers the pump but also feeds current into counter and the 555. Doing so basically the puts whole thing live. I guess you could say it’s a latching circuit If you then release the momentary switch, it stays live until the first missing pulse sets the 555 output low, which then opens the relay, killing power to the counter and the 555, and that way the whole system dies until you start it again.
I didn’t want to use a pulse-based relay because I want the system to stop pumping if there is any fault at all - it’s for an aeroplane and theres no room for error. It’s better for fuel not to pump
Than for it to carry on pumping when it shouldn’t. So I only want it to pump while there’s current to the relay.
The circuit functions exactly as designed - which is a small miracle, given my inexperience.
I’m now trying to design some fault tolerance into it and the one potential pitfall I see is if there’s a break in the line from the fuel flow transducer into the circuit. (The transducer is right at the front of the fuselage and my instrument panel where this circuit will be housed is about 2m towards the tail).
Hence my post.
I hope that makes sense?
Thanks!
yes...thank you.Hi eT
This circuit will be used in a fuel transfer system, pumping fuel from a wing tank to a center tank.
If the source tank runs dry, flow rate would drop and therefore the system should shut down the pump. If there was an error and the pump continued to run once the source tank ran dry, then the pump would continue pumping air. For a few seconds at a time that’s not a problem but over longer periods it can cause the pump to heat up. Not good on an aircraft fuel system, as you can imagine.
If it the reduced flow rate was caused by a blockage in the fuel pipe, as another example, then the pump would be straining, leading to heat build up. Also not good.
Does this answer your question?
Are you sure your transistor model hasn't been inadvertently replaced by an NPN one?On my model, the minute I add that R7 connection from the trigger to positive rail, that’s what happens.
by Duane Benson
by Jake Hertz
by Jake Hertz