AeroElectric-List Digest Archive

Wed 06/08/22


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 08:58 AM - Re: 30A PM alternator and Z101? (user9253)
     2. 09:53 AM - Re: 30A PM alternator and Z101? (johnbright)
     3. 03:41 PM - Re: Re: 30A PM alternator and Z101? (Robert L. Nuckolls, III)
     4. 05:01 PM - Re: Re: 30A PM alternator and Z101? (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 08:58:24 AM PST US
    Subject: Re: 30A PM alternator and Z101?
    From: "user9253" <fransew@gmail.com>
    If it is desired to shut off the alternator during flight and there is concern about causing an over voltage event, just close the throttle first. Speaking of a thermos bottle, never fill one with boiling hot coffee that is intended to be opened during flight. Due to the lower atmospheric pressure at altitude, the very hot coffee will turn to instant steam, burning the pilot and filling the cockpit with fog which fogs the windows. -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=507153#507153


    Message 2


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    Time: 09:53:37 AM PST US
    Subject: Re: 30A PM alternator and Z101?
    From: "johnbright" <john_s_bright@yahoo.com>
    I created a new pdf file (Elec Schem with Monkworkz MZ-30L as backup and Z101 as a template rev draft 4.pdf, too large to attach so https://drive.google.com/file/d/1Pg2Jg5Q-qNAFjQ4kux7Ugcsj3QxKQv74/view?usp=sharing) with five configurations for brainstorming. The configuration I posted on June 6, 2022 (Elec Schem with Monkworkz MZ-30L as backup and Z101 as a template rev draft 3.pdf) is now called Configuration 1. Bob: I don't understand why the regulator would generate a voltage spike if disconnected from the battery while delivering a significant level of current. Bill Judge of Monkworkz said "It's possible that the OVP would be triggered by switching off the relay when there is significant current flowing. No damage will occur but you only get three of those per engine start. Around 15.3 V is where an OV event is registered, and the duration needs to be on the order of 10 ns or more, way faster than DO-160 requires." I was trying to address his concern by adding the diode across the relay. The voltage spike has not been demonstrated on the bench to my knowledge. Alternator backup mode: I understand that it's not necessary. The crew will get an indication on the EFIS or panel light if the alternator wakes up from backup mode when the voltage drops to 13.7. Ref the Active High connection on the regulator. The only configuration that has any sort of switch sequencing SOP is Configuration 1 where the progressive battery alternator off / connect / on switch should not be moved quickly from on to off in order that the hypothetical voltage spike would not be created. If this switch is moved quickly from on to off and if the hypothetical voltage spike is a real thing, the diode across the relay will shunt said spike to the battery. Joe: AFAIK the 1N5822 diode is rated at 3A (IF(AV) under certain standard conditions) which is OK because the alternator is off when the relay contacts are open. I don't have a Monkworkz alternator to experiment with rather I'm trying to plan ahead in case this product proves itself in the field. I see it as being in the early adopter stage at present. -------- John Bright, RV-6A, at FWF, O-360 Z-101 single batt dual alt SDS EM-5-F. john_s_bright@yahoo.com, Newport News, Va https://drive.google.com/folderview?id=1u6GeZo6pmBWsKykLNVQMvu4o1VEVyP4K Read this topic online here: http://forums.matronics.com/viewtopic.php?p=507155#507155


    Message 3


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    Time: 03:41:38 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: 30A PM alternator and Z101?
    At 10:57 AM 6/8/2022, you wrote: > >If it is desired to shut off the alternator during flight and there >is concern >about causing an over voltage event, just close the throttle first. > >Speaking of a thermos bottle, never fill one with boiling hot coffee >that is intended >to be opened during flight. Due to the lower atmospheric pressure at >altitude, the very hot coffee >will turn to instant steam, burning the pilot and filling the >cockpit with fog which fogs the windows. Airplanes I fly don't achieve that kind of atmospheric delta-p. Further, in recognition of McD's famous pension for serving drive-up coffee capable of bodily harm . . . I don't bottle it up that hot for terrestrial travel much less at 10K (boiling point 195F). Bob . . . Un impeachable logic: George Carlin asked, "If black boxes survive crashes, why don't they make the whole airplane out of that stuff?"


    Message 4


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    Time: 05:01:40 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: 30A PM alternator and Z101?
    >Bob: >I don't understand why the regulator would generate a voltage spike >if disconnected from the battery while delivering a significant >level of current. This is an oft cited but seldom encountered condition which the automotive circle call an "alternator load dump" event. The worst-case pre-event condition is as follows: You have a really robust alternator (modern vehicle loads often call for alternators in 100A class!). Your battery is badly discharged . . . maybe you ran it down having left something on over night. You get the car started and the alternator goes to work stuffing energy back into the battery . . . i.e. regulator running nearly full field in an attempt to get things back in order. So now we have a BATTERY demanding alternator output while vehicle demands are low. Now . . . for what ever reason . . . the battery becomes disconnected from the vehicle's distribution system. The alternator suddenly becomes lightly loaded and the battery's willingness to absorb alternator transient surges is gone. Take a peek at this document from Texas Instruments: https://tinyurl.com/2ymdwrcj Figure 4 illustrates the automotive load dump parameters, this is an analog to the DO-160 40v surge favored by aviation in 14v systems. Figure 3 illustrates the condition that precipitates the event. Figure 8 illustrates performance of a over-voltage disconnect circuit (figure 6) when placed in the supply lead of an at risk product. We had a hopeful supplier to Beech offering heated seat inserts being proposed for some of our high-end heavy-iron. They were unable to pass the 80v surge for qualification on our 28v aircraft. I suggested and almost identical but simpler h.v. disconnect circuit which they incorporated with success . . . don't know if they ever made it onto our airplanes. Long story short, what is the likelihood of suffering a disconnect of depleted battery at rpms high enough to be producing heavy output thus setting up an alternator load-dump event? Further, the automotive load-dump ALWAYS involves a wound-field alternator driven by a regulator with a purposefully limited response struggling to bring a fully fielded, suddenly unloaded alternator back under control while it's b-lead is still connected to potential victims of the o.v. event. It's not clear to me how a PM alternator's rectifier/regulator would suffer a similar characteristic with the 'b-lead' relay. >Bill Judge of Monkworkz said "It's possible that the OVP would be >triggered by switching off the relay when there is significant >current flowing. No damage will occur but you only get three of >those per engine start. Around 15.3 V is where an OV event is >registered, and the duration needs to be on the order of 10 ns or >more, way faster than DO-160 requires." This makes no sense to me. Switching off the 'b-lead' relay can suddenly unload the alternator which will undoubtedly experience some magnitude of load dump surge. But where will it go and what risk for damage exists? He of all people should know. >I was trying to address his concern by adding the diode across the relay. >The voltage spike has not been demonstrated on the bench to my knowledge. Perhaps it would be well for him to explore this question? >Alternator backup mode: >I understand that it's not necessary. >The crew will get an indication on the EFIS or panel light if the >alternator wakes up from backup mode when the voltage drops to 13.7. >Ref the Active High connection on the regulator. > >The only configuration that has any sort of switch sequencing SOP is >Configuration 1 where the progressive battery alternator off / >connect / on switch should not be moved quickly from on to off in >order that the hypothetical voltage spike would not be created. If >this switch is moved quickly from on to off and if the hypothetical >voltage spike is a real thing, the diode across the relay will shunt >said spike to the battery. I'm concerned that any such band-aid would be useful along with any requirement placed on the pilot for positioning of switches. >Joe: AFAIK the 1N5822 diode is rated at 3A (IF(AV) under certain >standard conditions) which is OK because the alternator is off when >the relay contacts are open. If it's 'off' where does the surge come from, how high, how long and if the diode were not there, what are the risks? >I don't have a Monkworkz alternator to experiment with rather I'm >trying to plan ahead in case this product proves itself in the >field. I see it as being in the early adopter stage at present. If you're being recruited as part of the Monkworkz product development team, then one would want to do some bench testing to confirm/deny the hypothesis. I've got a AN20000 drive pad test stand whereupon such questions could be explored. Bob . . . Un impeachable logic: George Carlin asked, "If black boxes survive crashes, why don't they make the whole airplane out of that stuff?"




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