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#1
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I put a voltmeter on the alternator output and measured between 32-35 AC
volts at moderate load and moderate RPM. Looks like some diodes have decided to give up. Does anyone have any info on the Plane-Power alternators? There is a PMA'd replacement for my aircraft, and I will go that direction if there are no big disadvantages. Thanks, JKG |
#2
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Jonathan Goodish writes:
I put a voltmeter on the alternator output and measured between 32-35 AC volts at moderate load and moderate RPM. Looks like some diodes have decided to give up. Maybe. Voltmeters are a really bad way to look at how much non-sine AC ripple there is on a DC bus. Unless it's a known-good "True RMS" meter with AC-only coupling, it will lie. I've lost track; do you have audible whine in the audio? Does it change with load? -- A host is a host from coast to & no one will talk to a host that's close........[v].(301) 56-LINUX Unless the host (that isn't close).........................pob 1433 is busy, hung or dead....................................20915-1433 |
#3
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In article ,
David Lesher wrote: I put a voltmeter on the alternator output and measured between 32-35 AC volts at moderate load and moderate RPM. Looks like some diodes have decided to give up. Maybe. Voltmeters are a really bad way to look at how much non-sine AC ripple there is on a DC bus. Unless it's a known-good "True RMS" meter with AC-only coupling, it will lie. I've lost track; do you have audible whine in the audio? Does it change with load? David, I suspect that the meter isn't going to be 32 volts AC off the mark, even though it isn't a True RMS meter. The recommended threshold for AC voltage from the alternator is anywhere from 0.8 to 1.0 volts, based on the documentation I've read and my discussions with an engineer at ElectroSystems. However, I have alternator whine in the audio which changes with RPM and load. I've tried just about everything else to get rid of the whine, so this is about the last thing I know to do. JKG |
#4
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On Wed, 19 Apr 2006 12:06:37 -0400, Jonathan Goodish
wrote: In article , David Lesher wrote: I put a voltmeter on the alternator output and measured between 32-35 AC volts at moderate load and moderate RPM. Looks like some diodes have decided to give up. Maybe. Voltmeters are a really bad way to look at how much non-sine AC ripple there is on a DC bus. Unless it's a known-good "True RMS" meter with AC-only coupling, it will lie. I've lost track; do you have audible whine in the audio? Does it change with load? David, I suspect that the meter isn't going to be 32 volts AC off the mark, even though it isn't a True RMS meter. The recommended threshold for AC voltage from the alternator is anywhere from 0.8 to 1.0 volts, based on the documentation I've read and my discussions with an engineer at ElectroSystems. However, I have alternator whine in the audio which changes with RPM and load. I've tried just about everything else to get rid of the whine, so this is about the last thing I know to do. Does your plane have a split master switch? If so, shut down the alternator while flying and see if whine goes away. -Nathan |
#5
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In article ,
Nathan Young wrote: However, I have alternator whine in the audio which changes with RPM and load. I've tried just about everything else to get rid of the whine, so this is about the last thing I know to do. Does your plane have a split master switch? If so, shut down the alternator while flying and see if whine goes away. Yep, it goes away completely. |
#6
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![]() Jonathan Goodish wrote: I put a voltmeter on the alternator output and measured between 32-35 AC volts at moderate load and moderate RPM. Looks like some diodes have decided to give up. Do you have access to an oscilloscope? That will tell you the "truth" about what is happening on the bus. Go look at the waveforms I posted in your earlier thread... Is your A/C 14V or 28V. If your A/C is 28V, and your meter doesn't block dc, then the 32V reading might sort of make sense? If I were to hook my true-RMS Fluke 77 DVM to my 14V Cessna, under charge, the ripple would be less than 0.25Vac. |
#7
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In article .com,
"mikem" wrote: Do you have access to an oscilloscope? That will tell you the "truth" about what is happening on the bus. Go look at the waveforms I posted in your earlier thread... Is your A/C 14V or 28V. If your A/C is 28V, and your meter doesn't block dc, then the 32V reading might sort of make sense? If I were to hook my true-RMS Fluke 77 DVM to my 14V Cessna, under charge, the ripple would be less than 0.25Vac. Mike, Unfortunately, I do not have access to an oscilloscope. I've begged and pleaded but can't find anyone local who has one. As a result, I would be taking a risk by replacing the alternator, but it's cheaper than buying an oscilloscope. :-) My A/C is 14V. My meter is a Greenlee, and it does block DC. JKG |
#8
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I have no explanation for the 32V reading.
Here is another idea. Take the alternator off the airplane, and take it to an automotive shop that has an alternator test bench. For example, the Pep Boys store about 1/2mi from my house has one. They can spin it up, apply field current through a rheostat, apply a load, check its output current and ripple. If it has a blown diode, they should be able to tell you. You will have to make up some story about why they cant sell you an "exchange" Take your core, and either have it repaired, o/h, or trade your core for one that is already rebuilt by a FAA repair station. If there is nothing wrong with yours, you can work with your mechanic to reinstall it on the aircraft. I have had the Ford Prestolite alternator in my 182 develop "open diode" ripple. In my case, the one of the stator wires became disconnected from the diode stack due to vibration. It was "repaired". I got charged about $100, and it was returned with a yellow tag.. |
#9
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In article . com,
"mikem" wrote: I have no explanation for the 32V reading. I had an opportunity to poke around some more this evening. Despite Greenlee's insistence that my meter blocks DC when measuring AC volts (and vice versa), that appears to not be the case. The meter reads 26 volts AC when measured on the straight battery--no alternator. It appears to read AC correctly, and DC correctly, but not AC ripple on a DC bus. I have a 20 year old Beckman meter that was out of calibration, but I calibrated for AC and DC volts against the new Greenlee. The Beckman appears to block DC when reading AC volts. Both meters show around 12.8v at the battery, and almost exactly 14.0 volts DC when the alternator is charging, both at the battery and the bus. I've determined that the Greenlee's AC reading on the DC bus is highly inaccurate, but the Beckman shows almost zero AC volts (0.008) on the DC bus--I assume because the battery is absorbing the ripple. However, at the alternator, the Beckman shows approximately 0.30 volts AC, which increases to a maximum of 0.65 volts AC under full load and max static RPM. These look more like reasonable numbers. Could the voltage regulator be at fault? Load seems to amplify the noise, but the bus voltage is almost exactly 14.0 volts, regardless of load or RPM. I would think if the regulator was failing, I'd see some fluctuation, especially under full load. Could I be missing something? I know that it may very well still be a ground loop. There are some oddities that I still can't explain, however, like the intermittent static/crackling when the copilot keys the PTT and transmits. The landing light causes occasional crackle in the audio, but a corroded connector may be contributing to that problem, not sure. JKG |
#10
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"mikem" writes:
Jonathan Goodish wrote: I put a voltmeter on the alternator output and measured between 32-35 AC volts at moderate load and moderate RPM. Looks like some diodes have decided to give up. Do you have access to an oscilloscope? That will tell you the "truth" about what is happening on the bus. Go look at the waveforms I posted in your earlier thread... What He Said. Can you finagle any scope at all? That, and a major load will reveal bad diodes. Also, look at mikem's diagrams. Note how he put values in for all the ground connections. Maybe he'll do them again with 'bad ground' values. Poor Ground Shall Cause Grief. -- A host is a host from coast to & no one will talk to a host that's close........[v].(301) 56-LINUX Unless the host (that isn't close).........................pob 1433 is busy, hung or dead....................................20915-1433 |
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