AeroElectric-List Digest Archive

Tue 05/02/17


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 06:25 AM - Re: Overvoltage event (non-lithium battery) (Robert L. Nuckolls, III)
     2. 06:29 AM - Re: Overvoltage event (non-lithium battery) (Robert L. Nuckolls, III)
     3. 06:36 AM - Re: Overvoltage event (non-lithium battery) (Alec Myers)
     4. 11:00 AM - Re: Overvoltage event (non-lithium battery) (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 06:25:00 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Overvoltage event (non-lithium battery)
    At 10:23 PM 5/1/2017, you wrote: >I have met a couple pilots who insist on starting the engine with >the alternator off. I seem to remember that this was to protect the >alternator. I'm not sure from what. Has anyone ever seen an >alternator that has been damaged (or stressed or worn) by being on >during start? That can't happen either. Energy input to the alternator is RPM x Torque. Torque is absolutely proportional to output current. Field current rise from a de-energized state rises on the classic t=l/r time constant curve over a period of tens of milliseconds. It's a gentle increase in alternator effort with no sudden 'peaks' in mechanical or electrical stress. Those worries were never given foundation in physics. >Also Bob, please forgive what is probably a silly question that I >should think about rather than asking but if an alternator can't >raise bus voltage enough to damage avionics why am I building a >crowbar disconnect over voltage module? An alternator driven by a failed regulator has full bus voltage applied to the field. At cruise rpms, the alternator goes into a current limited runaway for voltage. If your airplane needs say 15A from the alternator in normal flight . . . then a 60A alternator will produce something on the order of 50-60 amps of EXCESS battery charge current. The voltage will begin to rise as the battery grunts the excess energy production. In tens to a couple hundred milliseconds after the failure event, the bus voltage will rise above the ov protection trip point . . . generally 32 to 33 volts in a 28v airplane. were it not for the BATTERY, the bus voltage could rise much more rapidly with an upper bound of 100 to 200 volts. In this case, the ov protection system is still expected to bring the alternator to heel in a time frame LESS than 100 milliseconds. Given that your supplier speaks of a 50 volt ov protection system, I suspect the appliance is qualified to DO-160 Category A for abnormal DC surge voltage. Quoting from DO-160 we find. Emacs! These numbers give rise to a design goal for ov protection systems to LIMIT a runaway alternator's output voltage to less than those values in the time frames cited. >Or is it just this particular avionic that cannot be damaged by an >alternator but others are vulnerable? Or something to do with it >being a 28V system instead of 14V? No. If your battery was on line at the time of the radio's failure . . . then there was no way that bus voltage would rise to levels claimed by the radio technician. If the battery were off line, then you would have experienced a trip of the ov protection system in an magnitude/time frame that was UNDER the envelope cited in DO-160. You are not the first owner/operator of an aircraft to be told that "a spike from your airplane killed your radio" . . . but in fact, if your battery was on line and you did not experience an ov trip, then there is no way that your airplane put any stress on the radio that it was NOT designed to deal with. 14 volt appliances use 1/2 the 28v qualification levels. I've always designed to Category Z. Emacs! Emacs! Note that category Z considers the extra hazard for having a very small or no battery at all. It's not hard to do . . . Bob . . .


    Message 2


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    Time: 06:29:17 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Overvoltage event (non-lithium battery)
    At 12:36 AM 5/2/2017, you wrote: > > > >>Also Bob, please forgive what is probably a silly question that I > should think about rather than asking but if an alternator can't > raise bus voltage enough to damage avionics why am I building a > crowbar disconnect over voltage module? > >A defective regulator can raise the bus voltage high enough to >damage the battery. A battery that is well maintained. I.e. periodically cap and load checked, will be taken out of the airplane when it no longer meets design goals for battery only endurance. Such a battery will grunt the alternator's abusive output during a runaway event for the time it takes to activate the ov protection system. In virtually EVERY ov event I have deliberately generated in 28v systems on the test bench, the bus voltage has NEVER exceeded 33 volts. The battery was not damaged and no appliances were harmed in the making of the video. Bob . . .


    Message 3


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    Time: 06:36:10 AM PST US
    Subject: Re: Overvoltage event (non-lithium battery)
    From: Alec Myers <alec@alecmyers.com>
    If the OV protection is absent, a defective regulator regulating the bus voltage to 18V (for a 12V system) will eventually damage the battery, but not the avionics. So isn't it fair to characterize the battery as being there to protect the avionics, and the OV crowbar being there to protect the battery? On 2May2017, at 9:26 AM, Robert L. Nuckolls, III <nuckolls.bob@aeroelectric.com> wrote: At 12:36 AM 5/2/2017, you wrote: > > > > >>Also Bob, please forgive what is probably a silly question that I should think about rather than asking but if an alternator can't raise bus voltage enough to damage avionics why am I building a crowbar disconnect over voltage module? > > A defective regulator can raise the bus voltage high enough to damage the battery. A battery that is well maintained. I.e. periodically cap and load checked, will be taken out of the airplane when it no longer meets design goals for battery only endurance. Such a battery will grunt the alternator's abusive output during a runaway event for the time it takes to activate the ov protection system. In virtually EVERY ov event I have deliberately generated in 28v systems on the test bench, the bus voltage has NEVER exceeded 33 volts. The battery was not damaged and no appliances were harmed in the making of the video. Bob . . .


    Message 4


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    Time: 11:00:27 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Overvoltage event (non-lithium battery)
    At 08:33 AM 5/2/2017, you wrote: > > >If the OV protection is absent, a defective regulator regulating the >bus voltage to 18V (for a 12V system) will eventually damage the >battery, but not the avionics. Yyeeaah . . . sort of. A battery that's in good condition will willingly and ably stand off most alternators until the ov protection system can react. If the ov protection is absent, voltage will rise with a rate dependent on battery condition and magnitude of the 'overcharge' current. We've seen cases of sustained ov on a good battery . . . and yes, it's really hard on the battery. But this event took a long time . . . perhaps hours, perhaps more than one flight to evolve to this condition. Emacs! . . . and yes, the battery was trashed. I don't recall if any other system components were damaged . . . >So isn't it fair to characterize the battery as being there to >protect the avionics, and the OV crowbar being there to protect the battery? No . . . batteries are there to start engines and back up alternators. A properly designed ov protection system will arrest a runaway alternator before the damages propagate to other components in the system . . . whether the battery is on line or not. It's a happy coincidence that a robust battery contributes to a graceful recovery from an ov event . . . but there is no expansion of a battery's primary role of offering a reversible chemical energy source. Bob . . .




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