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04-20-2016, 02:17 PM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Capactence fuel sender and GRT EIS question
I am helping a buddy upgrade his plane from steam gauges and a Vision Microsystems engine monitor system to a GRT EFIS and GRT EIS.
The last (Hopefully last) issue is the EIS fuel level doesn't seem to be reading info from the sender from the Vision Micro .
The Vision Micro used a capacitance sender, with three wires coming out of a large threaded hex fitting. I have no idea if there is a built in converter in the actual probe or not, or if the Vision Micro unit was designed to read the sender output directly without any kind of converter.
Anybody out there dealt with this in the past, and what/how did you get the two units to play nicely with each other? I searched the archives, found multiple references to the problem, but not to the solution.
Any source or part number for the converter box------pretty sure one is needed-----to make this setup work.
Changing out the capacitance probe to a float is the last option, really do not want to even think about it.
Thanks in advance...
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
Last edited by Mike S : 04-20-2016 at 02:21 PM.
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04-20-2016, 03:26 PM
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Join Date: Oct 2006
Location: Garden City, Tx
Posts: 5,120
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The way capacitance senders work, inside the tank, uses only two wires - one is the airframe itself, and the other one is connected to the plates which are insulated from the airframe. If you have more than those two connections, then you already have some type of converter between those wires and the plates.
The trick may be figuring out which converter, and which wires do what. It's likely they are power, ground, and signal.
__________________
Greg Niehues - SEL, IFR, Repairman Cert.
Garden City, TX VAF 2020 dues paid 
N16GN flying 700 hrs and counting; IO360, SDS, WWRV200, Dynon HDX, 430W
Built an off-plan RV9A with too much fuel and too much HP. Should drop dead any minute now.
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04-20-2016, 05:00 PM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Quote:
Originally Posted by airguy
The way capacitance senders work, inside the tank, uses only two wires - one is the airframe itself, and the other one is connected to the plates which are insulated from the airframe.
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Well, the unit is a tube with a wire inside it, and the tank is fiberglass.
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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04-20-2016, 09:46 PM
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Join Date: Aug 2007
Location: Ontario, Canada
Posts: 2,280
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Mike - there is a frequent poster on this site, Reggie Smith (FasGlass or similar user name) who his a guru on Vision Microsystems stuff. Look him up - he will be able to tell you how the VM fuel probes work, and what adaptation may be required to go to the GRT EIS system.
His website: http://vmsupport.weebly.com/
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04-21-2016, 07:44 AM
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Join Date: Oct 2006
Location: Garden City, Tx
Posts: 5,120
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Quote:
Originally Posted by Mike S
Well, the unit is a tube with a wire inside it, and the tank is fiberglass.
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Interesting design, I hadn't seen those - but the operating principle is the same. You essentially are building a capacitor consisting of two conductive elements, with a dielectric between them. That's only two wires, any way you cut it. The converter puts an AC signal on those two wires to charge/discharge the capacitor rapidly and deduces the dielectric constant by virtue of the amount of charge the capacitor will take. Part of the dielectric is air (or fuel vapor, which has a very similar dielectric constant) and part is fuel (which is quite different from air or fuel vapor). The net dielectric constant will change considerably with the amount of the capacitor that is submerged, which changes the amount of charge the capacitor will take. The converter figures this out, and converts it to a voltage level output to your instruments, similar to what a float gauge would give.
__________________
Greg Niehues - SEL, IFR, Repairman Cert.
Garden City, TX VAF 2020 dues paid 
N16GN flying 700 hrs and counting; IO360, SDS, WWRV200, Dynon HDX, 430W
Built an off-plan RV9A with too much fuel and too much HP. Should drop dead any minute now.
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04-21-2016, 09:39 AM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Quote:
Originally Posted by Canadian_JOY
Mike - there is a frequent poster on this site, Reggie Smith (FasGlass or similar user name) who his a guru on Vision Microsystems stuff. Look him up - he will be able to tell you how the VM fuel probes work, and what adaptation may be required to go to the GRT EIS system.
His website: http://vmsupport.weebly.com/
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Got it-------thanks.
BTW, just in case someone else needs to contact him, his login name is Glas467.
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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04-21-2016, 10:54 AM
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Join Date: Jan 2011
Location: Olympia, WA
Posts: 227
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Mike,
Greg Niehues did a nice job of explaining the principle of operation of a capacitance probe.
Here's some info specific to the VMS VM1000 implementation:
1) 3 wire probe with an internal oscillator circuit. Red and black wires are for 5V DC excitation, white wire is the output signal which is a 5V AC square wave with frequency proportional to the capacitance and hence fuel level. The white wire also shares the black wire ground reference.
2) The VMS DPU outputs regulated 5V DC to the probe and converts the returning frequency to a fuel level based on a lookup table hard burned into the main program chip.
3) The conversion circuitry is inside the VM1000 DPU, not inside the probe.
First step I'd recommend is to test the probe to make sure it is good:
1. With power applied to VM1000 instrument system, perform the following DC voltage tests at the transducer wires:
a. BLK (meter com) to RED (meter +) (s/b = 5.00 VDC) . = ________
b. BLK (meter com) to WHT (meter +) (s/b > 1.9 VAC). = ________
c. BLK (meter com) to WHT (meter +) (s/b 1.9 to 2.4 VDC). = ________
2. With probe disconnected from EC100 or IO PCB, measure resistance between probe wires as follows:
a. BLK (meter com) and WHT (meter +) wires. (s/b approx 14500 ohms) . Resistance = ________
b. BLK (meter com) and RED (meter +) wires. (s/b approx 9100 ohms) . Resistance = ________
c. WHT (meter com) and RED (meter +) wires. (s/b approx 5500 ohms) . Resistance = ________
Next, determine if the GRT is able to read a frequency based capacitance probe. If so, it should be a matter of getting the settings just right. If the GRT requires 0-5V output (or other voltage based signal) from the probe, the only way to do this is through a frequency to voltage converter circuit.
Several folks here on VAF have had good luck using the Princeton converter mentioned previously in this thread.
Hope this helps,
Reggie
http://vmsupport.weebly.com/
__________________
Reggie Smith ______
RV-8 Wish List/RV-4 Experience
Glasair 1-RG Flying
Vision Microsystems EPI800 & VM1000 support:
http://vmsupport.weebly.com/
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04-21-2016, 11:16 AM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Quote:
Originally Posted by Glas467
Here's some info specific to the VMS VM1000 implementation:
1) 3 wire probe with an internal oscillator circuit. Red and black wires are for 5V DC excitation, white wire is the output signal which is a 5V AC square wave with frequency proportional to the capacitance and hence fuel level. The white wire also shares the black wire ground reference.
2) The VMS DPU outputs regulated 5V DC to the probe and converts the returning frequency to a fuel level based on a lookup table hard burned into the main program chip.
3) The conversion circuitry is inside the VM1000 DPU, not inside the probe.
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OK, so the circuitry is split between the probe and the DPU. The GRT does have a 5v output as I recall, so that should be good to drive the internals of the probe.
Quote:
Originally Posted by Glas467
First step I'd recommend is to test the probe to make sure it is good:
1. With power applied to VM1000 instrument system, perform the following DC voltage tests at the transducer wires:
a. BLK (meter com) to RED (meter +) (s/b = 5.00 VDC) . = ________
b. BLK (meter com) to WHT (meter +) (s/b > 1.9 VAC). = ________
c. BLK (meter com) to WHT (meter +) (s/b 1.9 to 2.4 VDC). = ________
2. With probe disconnected from EC100 or IO PCB, measure resistance between probe wires as follows:
a. BLK (meter com) and WHT (meter +) wires. (s/b approx 14500 ohms) . Resistance = ________
b. BLK (meter com) and RED (meter +) wires. (s/b approx 9100 ohms) . Resistance = ________
c. WHT (meter com) and RED (meter +) wires. (s/b approx 5500 ohms) . Resistance = ________
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Looks like this is straight out of the manual he has-------cant do test 1, a b c as the VM1000 is no longer in the plane. Will have him do the others.
Quote:
Originally Posted by Glas467
Next, determine if the GRT is able to read a frequency based capacitance probe. If so, it should be a matter of getting the settings just right. If the GRT requires 0-5V output (or other voltage based signal) from the probe, the only way to do this is through a frequency to voltage converter circuit.
Several folks here on VAF have had good luck using the Princeton converter mentioned previously in this thread.
Hope this helps,
Reggie
http://vmsupport.weebly.com/
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Hope it helps??? understatement of the day  Immense help, and very much appreciated.
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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04-21-2016, 12:08 PM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Quote:
Originally Posted by bullojm1
Mike,
Give GRT a call. They have a version of their Princeton Capacitive converters that operate via a probe:
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Ya'know, If I had only paid attention to what you said---------- They have a version of Their---------
GRT and Princeton---------same people, or at least half of GRT.
http://grtavionics.com/contact.html
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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