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Question TCW IBBS (3AH) volts?

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Neal

Forums Chief Pilot
Staff member
Joined
Oct 31, 1996
Posts
1,533
Type aircraft owned
Carbon Cub FX-3
Base airport
KFCI
Ratings
COMM, IFR, MEL, SEL
Everything has been working great, had an enjoyable golden hour flight tonight, OAT 60F, perfect conditions. I turned on IBBS and saw 12.7V wondering what the state of my IBBS battery is. That seems a bit low if it is in fact a LiFePO4 battery. Maybe it's because I haven't flown enough to get it charged? So I'm curious from others, when you turn on IBBS, realizing it's under load, what voltage are you seeing?

During flight I saw a max of 13.3 which seems odd as my other two LiFePO4 (EarthX) batteries show 14.1V at full charge. Maybe it's not charged yet? Maybe the battery has a bad cell? What are you seeing for a fully charged TCW IBBS battery?
 
My FX-3 AFM supplement includes the following text -

"The normal IBBS charging cycle has IBBS volts gradually increasing to about 14.2 V then gradually dropping to about 13.3 V where the charging cycle starts again. IBBS will not be at maximum capacity until IBBS Volts has risen, at least once, to about 14.2 V after engine start."

and this graphic -

IBBS charge cycle graph.PNG


In flight the main battery and ignition battery display MAIN bus volts which is not a useful indication of battery condition. IBBS volts is the actual battery pack voltage not MAIN bus volts.
 
In flight the main battery and ignition battery display MAIN bus volts which is not a useful indication of battery condition
Not sure I fully agree. For example my backup ignition (EarthX ETX-104) doesn't just peg at 14.1V when on the main bus. The state of charge is not 100%. The voltage rises for example yesterday from 13.7 to 14.1. Granted, off charge the volts would show more like 13.0-13.3 and not 13.7. But there is still indication of a charge and then it peaks at 100% state of charge.

The IBBS is interesting. So what is your state of charge which is what I wish we would see instead of volts. This is how my RV (motorhome) is wired using a shunt to measure the current flow. Regardless of charging amps I see the actual state of charge of the battery. So with the IBBS I'm curious what the state of charge is and for those using it as a backup ignition battery this is important to know for what you can expect should you need to use it.
 
Not sure I fully agree. For example my backup ignition (EarthX ETX-104) doesn't just peg at 14.1V when on the main bus. The state of charge is not 100%. The voltage rises for example yesterday from 13.7 to 14.1.

The ignition battery voltage readout is MAIN bus volts less any drop across the Schottky diode. Ignition volts will only be significantly different from MAIN volts is the battery charge current is very large. That does not happen with the standard 2 AH AGM battery. I have no data for your non-standard ignition battery.
 
My ignition battery matches the behavior of my starter battery. The odd ball is IBBS.
 
So with the IBBS I'm curious what the state of charge is and for those using it as a backup ignition battery this is important to know for what you can expect should you need to use it.

State of charge can be 100% meaning that it cannot be charged any more. That does not tell you much about its capacity since capacity reduces as the battery ages.

The only way to know the battery capacity is to fully charge it and then run a discharge test. That tells you the capacity at the date and time of the test.

For an IBBS battery in good condition I assume the battery is not fully charged until the voltage rises over 13.2 V. I alert if alternator output is available and IBBS voltage is not greater than 13.2 V. I see this alert after engine start if IBBS was used for long time before starting. It has always gone away before I'm ready for takeoff.

More text from my AFM supplement -

"IBBS Volts - The color bands of the IBBS Volts scale have two different configurations. One set of bands is used when alternator output is available for IBBS charging. The other set of bands is used when alternator output is not available.

The upper end of the amber range of the charging scale has been selected to provide early warning that IBBS is either not charging or may not be fully charged. If IBBS was used for an extended time before engine start then voltage in the amber range and CAS alert IBBS VOLTS should be expected. The time it takes for this alert to be cleared will depend on how deeply the IBBS was discharged. Flight planning should assume that full IBBS capacity is not available while the IBBS VOLTS alert is displayed."
 
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My ignition battery matches the behavior of my starter battery. The odd ball is IBBS.

The IBBS battery pack is not charged as a series group. Each cell is charged individually. The battery pack voltage is not the IBBS charge terminal voltage.
 
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A while ago I accidentally deep discharged my IBBS battery. Long story shortened - the battery pack had one dead cell that appeared as a short circuit to a single cell charger.

I replaced the battery pack with a new one but IBBS voltage did not increase over 12.9 V in flight.

I sent the IBBS in for repair and an open circuit solder connection was found on one component.

I speculate that the IBBS internal charging circuit had, while attempting to charge the shorted cell, overheated a surface mount component and compromised its solder connection. (This was a rev G IBBS and current design is rev J or later).
 
Using voltage to determine battery charge state is very hard for lithium based batteries which is why when I was working in the mobile phone business, the “BMS” always included a “charge counter” that measured the current in and out of the battery. Due to “drift” in this measurement, you needed to fully discharge the battery every few months to “reset” the charge counting.

With the IBBS, the best way that I can see of determining full charge is make sure that a full charge cycle (bulk - constant current, absorption - constant “high” voltage, float - lower voltage) has been completed not just that the “bulk” charge phase has completed (e.g. the voltage has increased to the high level).
 
With the IBBS, the best way that I can see of determining full charge is make sure that a full charge cycle (bulk - constant current, absorption - constant “high” voltage, float - lower voltage) has been completed not just that the “bulk” charge phase has completed (e.g. the voltage has increased to the high level).

I have spent some time trying to understand the details of the IBBS but have not yet made any attempt to instrument it to reveal the detail of how it charges the individual cells.

All I know about the battery pack charging is how the total voltage of all cells in series changes with time. I shared that earlier. That data appears to show that charging ceases when voltage reaches 14.2 V and resumes again when voltage has dropped to 13.2 V. Of course the charging period would be much longer for a discharged IBBS but I have not explored region ( I do have data but have not examined it).

Please share any knowledge you have of the IBBS internal charger and the charge profile(s) it uses.
 
Of course the charging period would be much longer for a discharged IBBS but I have not explored region ( I do have data but have not examined it).

This is what IBBS charging looked like after intentional discharge of a new battery pack to 11 V.

IBBS charge after discharge.PNG
 
My experience comes from my motorhome with a Victron LiFePO4 stack. LiFePO4 battery charging is managed by the BMS including cell balancing. It is the most critical element of LiFePO4 health as well as temperature awareness to charge within params. My ETX-900 only lasted two years but as I flew often and never had a problem with cranking the engine I rarely had it on a charger. That will be different this time around as the charger I believe is necessary for getting the battery to 100% state of charge (SOC) and keeping cells balanced. Letting LiFePO4 batteries discharge, you can typically go down to 10% SOC but you only need to let them drop slightly, such as 80% SOC and then let them charge to 100% will ensure cells are balanced. There is a myth out there from iPhones about keeping "Lithium" batteries at 80% prolongs the life. This myth has been questioned of late and also it depends on the battery chemistry. My understanding and belief is that does not apply to LiFePO4.

TCW offers a plugin charger for the IBBS, I bought one when my last plane had IBBS issues when the wire came off the breaker that I found 6 months later. Wonder how discharged that battery became but it never had an issue operating. As mentioned in another post they recommend putting it on the charger if not in use 6-9 months I believe it was, this is something kit builders need to know to keep batteries healthy while not in use. It's not ideal to get to the IBBS to manually charge it but it's possible if needed.

 

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