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Two significant things missing from the comments below are 1. Measured battery capacity depends significantly on discharge current 2. Measured battery capacity dependssignificantly on temperature (esp. for lead acid batteries) These two things cause most of the confusion I see glider pilots having understanding battery run time For #1. A 12 Ah battery is not 12 amps for one hour, far from it. For lead acid batteries the standard is to measure the discharge over a 20 hour period. That is at a constant discharge current of 0.05 x C (where C is the capacity in Ah). If you draw higher current from a battery you get less total energy out, the extra energy has gone into ohms law heating in the internal resistance (I squared R). The internal resistance is only the simplest model of what is going on, there are other effects that increase losses as the current increases significantly. Understanding the dependency of the measured battery capacity on the discharge current/capacity ratio also explains things like why a single 12 Ah battery can provide more capacity than 2 x 7Ah batteries discharged one after the other. A higher current/capacity ratio is being drawn from the 7Ah batteries. If you want to measure how many amps x hours you really will get our of a battery then you need to measure it near the actual discharge current it will have (and near the actual temperature it will be at). The reason that (as mentioned in the posting) that discharge curves measure down to different voltages depending on the current/capacity ratio the measuremnt is made at is due to internal resistance. Higher discharge currents cause more of an internal voltage drop across the internal resistance so the external voltage you measure the discharge down to has to be lower. The easiest way to get the correct cut off voltage is to look at a discharge graph on a manufactueres spec sheet. While the measuremnt cut-off voltage (usually around 10 to 10.5 volts for typical glider battery measurements) may be too low for some older electronics it is likely to be high enough to power modern avionics/toys found in gliders (I know some of the older transponders and radios that really prefer to run at ~14 volt alternator voltrages may have issues). For those more interested in capacity measurements and discharge curves should Google Peukert's equation that describves a useful emperical relationship between discharge currents and battery capacity.The "Peukert number" for a battery describes how immune its capacity is to changes in the discharge current. You have to calcualte this number yourself from meaurements, manufacters won't usually quote it. Battery capacity measuremnts usually start with a fully charged battery. Using a trusted charger and leaving the thing on charge for a long time is a good way to do this in practice. The open circuit voltate when you take the battery off charge will measure above 12.5 volts or so but that is an aberation caused by surface charge. You will see the voltage rapidly drop of (usually in seconds to tens of seconds depending on the measurement current) as you measure voltage under load. In practice this surface charge represents no significant battery capacity. In the measurement mentioned below there should really be no need to let batteries sit for a day or so before a discharge test. BTW as mentioned below even a partial discharge cycle can show up problems. Again it is internal resistance that is likely dominating the measurements. Cells that are sick or damanged or just old often have higher internal resistance than a healthy cell and will cause the voltage to drop quickly. For those reasons discharge tests at currents much higher than you will operate the batteries can be useful since the higher currents will show up internal restance problems quickly (resistive power losses are proportional to the square of the current) -- even if the measuremnts don't mean much for calculating expected battery life under any particular load. For #2 Temperature effects, that is a longer topic, but be the standard is to measure lead acid batteries at 20 C. AGM battery capacities approximately halve down to around -20 to -25C where the electrolyte can start to freeze. And yet again internal resistance (decreasing conductivity of the electrolyte vs temperature) explains a lot of this behavior. I show a few capacity vs. temp curves in the slide talks I linked to in another reply in this thread. One of the curves shows the rapid voltage drop of a cell freezing as it discharges (some thing to worry about on that next really long and cold wave flight :-) Cheers Darryl Ramm DG-303 6DX COLIN LAMB wrote: Testing AH of batteries Battery capacity is measured using a defined minimum voltage. That voltage may or may not correspond to the minimum voltage your glider equipment will operate on. If you use diodes, that minimum voltage will move slightly. Capacity also depends upon a starting voltage - which is significantly higher than 12 volts. I often need to test batterys used in our search and rescue radios and have found that I can test battery capacity quickly without a full discharge. I charge the batteries, then let them sit for a day. Then, I put a load on them and simply watch the decay of voltage over time. In a very short time, you can make a graph that will indicate the trend of the battery and compare with a new battery. A battery with reduced capacity will drop voltage much more quickly. You can determine the capacity of the battery during charge, too. Capacity is the ability of the battery to resist change. That applies either way. it means the battery will drop in voltage or charge more slowly. So, you can simply time the charge of two batteries and learn the comparative capacity of each. Colin |
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