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________________________________________________________________________________
Date: 
Oct 05, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Voltmeter & Ammeter normal ranges
      
      At 08:32 AM 9/24/2017, you wrote:
      >Exactly. Joe could you please confirm that the jpeg below is 
      >visible? If so it's obvious that while the voltage seems to be 
      >moving around a tiny bit, it never gets to the point which would 
      >allow the amperage shown. It's always above 14V. Also I checked some 
      >data with the engine shut down and while the amperage still wanders 
      >around it's 1 A or less (-5.5 to -6.5 A)
      
        Digital data acquisition is fraught with
        opportunity for confusion/error.  Depending
        on how the variable is sampled, pre-filtered
        and software filtered, data displayed or plotted
        can take on the appearance of instability.
      
        Unless you're measuring the output from something
        like a battery . . . or a laboratory power supply,
        the stimulus being observed will have some noise
        on it. This is especially true of signals gathered
        from the DC power system of any vehicle.
      
        When I'm gathering data on relatively low frequency
        events, my DAS pre-filtering is usually rolled
        off at 10 Hz. Then interpretation software is
        designed to do a 'rolling average' on sampled values.
        For a DAS set up to gather 100 samples/second, we'll
        buffer 16 samples in a memory stack, take the sum
        of those values then divide by 16 for an average
        of that 'packet' of data. When the next sample comes
        in, we add the new value, throw away the oldest value
        and do the average again.
      
        This pre/post processing of data does a nice job
        of ignoring the high frequency perturbations that
        are riding on top of the value of interest. The
        processed data plots are nice smooth lines that
        are more meaningful.
      
        I suspect that data plots taken from most
        EIS systems have little pre-processing and no
        post processing . . . so the traces are understandably
        'ragged'. So while the voltage traces might
        be interpreted as 'unstable', it's probable
        that the system is operating normally.
      
        Just for grins, I took the 'scope out to peek at
        the 14v bus in Dr. Dee's '87 GMC Sierra. With
        the 'scope set to 2.5S/div H and 2V/div V, we
        get the following trace when cranking the engine.
      []
      
      
         Figure 1.
      
         Note that battery voltage starts to sag from
         about 12.8 volts but takes a steeper slope
         as the starter contactor is energized followed
         by a profound drop to 8 volts as the contactor
         closes.  A few milliseconds later, the voltage
         rises to about 10v until the engine catches
         approx 1.2S later and the alternator kicks
         in . . . whereupon but bus rises to about
         14.6V
      
      []
      
         Figure 2.
      
         In the next plot we see that the bus is 'steady'
         at about 14.7V with the occasional perturbation
         combined with some little 'spikes' with an amplitude
         of 1 to 2 volts.
      
         To get a closer look at the voltage in the
         next plot, we need to turn up the 'scope sensitivity
         and to to AC coupling:
      
      []
      
        Figure 3.
      
        With a vertical scale of 0.5V/div and horizontal
        of 0.05S/div we can get a better look at the 'noise'.
        This particular trace caught a 1.5v transient amongst
        about 10 smaller artifacts.
      
        We see that even when there are no obvious
        transients, the horizontal line has 'thickness'.
        Zooming in closer:
      
      []
      
        Figure 4.
      
        We find that the horizontal line is 'fuzzy' with
        positive and negative going transients on the
        order of 300mV peak.
      
        Depending on where your digital data acquistion
        system takese a 'snapshot', the sampled votlage
        might appear to 'wobble' by as much as +/-0.5V.
      
        Spreading out the major transients by a factor
        of 20 . . .
      
      
      []
      
        Figure 5.
      
      
        Shows that they're about 400 microSeconds wide. These
        plots offer a small peek into the nature of DC power
        systems on vehicles.  A few weeks ago, a thread on
        another list server offered this image suggesting
        that the full-wave, rectified 3-phase alternator
        would produce wave forms something along these lines . . .
      
      []
      
      
        Figure 6.
      
        Theoretically true, but  I've never seen so 'clean'
        a picture in the wild . . .
      
        Referring to Mil-Std-704 we learn that DC power systems
        demonstrate a certain amount of noise (distortion)
        under normal conditions. The document cites
        the following plot for a 28v system (cut the
        numbers in half for 14 volts).
      
      []
      
      
         Figure 7.
      
         Over the range of 1000 Hz (1 milliSecond period) and
         10,000 Hz (100 uSecond), we should expect artifacts
         of noise up to 0.5 VRMS (1.5 volts pk-pk) on a 14V bus.
      
         Above and below those frequencies, the allowable/exoected
         noise levels fall off. When you hook an oscilloscope to
         the bus, the best you can do is sample small features
         of the noise as illustrated in the first 5 figures. Further,
         you'll never see the pristine plots hypothesized in Figure 6.
      
      
      Emacs!
      
      Figure 8.
      
         The most significant attribute of a DC power system is VOLTAGE.
         Referring again to Mil-STD-704 we find the plot above. Again,
         cut the voltage levels in half for a 14v system.
      
         This figure suggests that any voltage vs. time condition
         below the upper trace . . . and above the lower trace . . .
         is a condition to be expected for designing and operating
         appliances powered from the DC system.
      
         It's my wish that this narrative will give you some tools
         for critical review of any data presented by either operating
         or diagnostic instruments. Understanding characteristics
         signals present on the bus -AND- limits on the measuring
         instrument will go to better design, operation and diagnosis
         of your ship's DC power system.
      
      
         Bob . . .  
      
________________________________________________________________________________
Subject: 
Daily List Digest Question
From: 
"jrevens" <jrevens(at)comcast.net>
Date: 
Oct 05, 2017
      
      
      I'm pretty sure that this has been brought up before, but not sure if any answers
      were provided.  I receive the Daily List Digest via email, and today's digest
      contained 9 messages. Following message number 9, from Charles Rogers, there
      were pages and pages and pages of unreadable "code".  It takes a couple of minutes
      just to scroll through all of it.  It seems to have been awhile since this
      has happened, but sometimes it happens frequently.  Is this possibly an issue
      with my iPad, my ISP, etc., or does it originate with the sender?  Does anyone
      else experience this?
      
      --------
      John Evens
      Thorp T-18 N71JE (built & flying)
      Kitfox SS7 N27JE (building)
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473367#473367
      
      
________________________________________________________________________________
Subject: 
Re: Dual batteries or dual alternators?
From: 
"Flying Patagonia" <tintiescobar(at)hotmail.com>
Date: 
Oct 05, 2017
      
      
      Thanks!
      Do you have this diagram in better quality? It cant see very well..
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473370#473370
      
      
________________________________________________________________________________
Subject: 
Re: Dual batteries or dual alternators?
From: 
"Flying Patagonia" <tintiescobar(at)hotmail.com>
Date: 
Oct 05, 2017
      
      
      Bob, or anybody else to help how to wire a dual EFII, into the Z-12 diagram...?
      Thanks!
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473371#473371
      
      
________________________________________________________________________________
From: 
Alec Myers <alec(at)alecmyers.com>
Date: 
Oct 05, 2017
Subject: 
alternator whine
      
      
      Hi Bob and others,
      
      My 182 has a noticeable alternator whine, about 5kHz (Im guessing) at cruise rpm.
      I think its worse recently than it used to be.
      
      Where and what should I start investigating?
      
      
________________________________________________________________________________
Subject: 
Re: alternator whine
From: 
"user9253" <fransew(at)gmail.com>
Date: 
Oct 05, 2017
      
      
      Check the AC (Alternating Current) component of the alternator output.  If it is
      more than 1 volt, suspect a bad diode.
      
      --------
      Joe Gores
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473379#473379
      
      
________________________________________________________________________________
From: 
Bob Verwey <bob.verwey(at)gmail.com>
Date: 
Oct 06, 2017
Subject: 
Re: Voltmeter & Ammeter normal ranges
      
      Absolutely facinating and insightful to a neophyte like myself 
      
      On 05 Oct 2017 7:17 PM, "Robert L. Nuckolls, III" <
      nuckolls.bob(at)aeroelectric.com> wrote:
      
      > At 08:32 AM 9/24/2017, you wrote:
      >
      > Exactly. Joe could you please confirm that the jpeg below is visible? If
      > so it's obvious that while the voltage seems to be moving around a tiny
      > bit, it never gets to the point which would allow the amperage shown. It's
      > always above 14V. Also I checked some data with the engine shut down and
      > while the amperage still wanders around it's 1 A or less (-5.5 to -6.5 A)
      >
      >
      >  Digital data acquisition is fraught with
      >  opportunity for confusion/error.  Depending
      >  on how the variable is sampled, pre-filtered
      >  and software filtered, data displayed or plotted
      >  can take on the appearance of instability.
      >
      >  Unless you're measuring the output from something
      >  like a battery . . . or a laboratory power supply,
      >  the stimulus being observed will have some noise
      >  on it. This is especially true of signals gathered
      >  from the DC power system of any vehicle.
      >
      >  When I'm gathering data on relatively low frequency
      >  events, my DAS pre-filtering is usually rolled
      >  off at 10 Hz. Then interpretation software is
      >  designed to do a 'rolling average' on sampled values.
      >  For a DAS set up to gather 100 samples/second, we'll
      >  buffer 16 samples in a memory stack, take the sum
      >  of those values then divide by 16 for an average
      >  of that 'packet' of data. When the next sample comes
      >  in, we add the new value, throw away the oldest value
      >  and do the average again.
      >
      >  This pre/post processing of data does a nice job
      >  of ignoring the high frequency perturbations that
      >  are riding on top of the value of interest. The
      >  processed data plots are nice smooth lines that
      >  are more meaningful.
      >
      >  I suspect that data plots taken from most
      >  EIS systems have little pre-processing and no
      >  post processing . . . so the traces are understandably
      >  'ragged'. So while the voltage traces might
      >  be interpreted as 'unstable', it's probable
      >  that the system is operating normally.
      >
      >  Just for grins, I took the 'scope out to peek at
      >  the 14v bus in Dr. Dee's '87 GMC Sierra. With
      >  the 'scope set to 2.5S/div H and 2V/div V, we
      >  get the following trace when cranking the engine.
      > [image: []]
      >
      >   Figure 1.
      >
      >   Note that battery voltage starts to sag from
      >   about 12.8 volts but takes a steeper slope
      >   as the starter contactor is energized followed
      >   by a profound drop to 8 volts as the contactor
      >   closes.  A few milliseconds later, the voltage
      >   rises to about 10v until the engine catches
      >   approx 1.2S later and the alternator kicks
      >   in . . . whereupon but bus rises to about
      >   14.6V
      >
      > [image: []]
      >   Figure 2.
      >
      >   In the next plot we see that the bus is 'steady'
      >   at about 14.7V with the occasional perturbation
      >   combined with some little 'spikes' with an amplitude
      >   of 1 to 2 volts.
      >
      >   To get a closer look at the voltage in the
      >   next plot, we need to turn up the 'scope sensitivity
      >   and to to AC coupling:
      >
      > [image: []]
      >  Figure 3.
      >
      >  With a vertical scale of 0.5V/div and horizontal
      >  of 0.05S/div we can get a better look at the 'noise'.
      >  This particular trace caught a 1.5v transient amongst
      >  about 10 smaller artifacts.
      >
      >  We see that even when there are no obvious
      >  transients, the horizontal line has 'thickness'.
      >  Zooming in closer:
      >
      > [image: []]
      >  Figure 4.
      >
      >  We find that the horizontal line is 'fuzzy' with
      >  positive and negative going transients on the
      >  order of 300mV peak.
      >
      >  Depending on where your digital data acquistion
      >  system takese a 'snapshot', the sampled votlage
      >  might appear to 'wobble' by as much as +/-0.5V.
      >
      >  Spreading out the major transients by a factor
      >  of 20 . . .
      >
      >
      > [image: []]
      >  Figure 5.
      >
      >
      >  Shows that they're about 400 microSeconds wide. These
      >  plots offer a small peek into the nature of DC power
      >  systems on vehicles.  A few weeks ago, a thread on
      >  another list server offered this image suggesting
      >  that the full-wave, rectified 3-phase alternator
      >  would produce wave forms something along these lines . . .
      >
      > [image: []]
      >
      >  Figure 6.
      >
      >  Theoretically true, but  I've never seen so 'clean'
      >  a picture in the wild . . .
      >
      >  Referring to Mil-Std-704 we learn that DC power systems
      >  demonstrate a certain amount of noise (distortion)
      >  under normal conditions. The document cites
      >  the following plot for a 28v system (cut the
      >  numbers in half for 14 volts).
      >
      > [image: []]
      >
      >   Figure 7.
      >
      >   Over the range of 1000 Hz (1 milliSecond period) and
      >   10,000 Hz (100 uSecond), we should expect artifacts
      >   of noise up to 0.5 VRMS (1.5 volts pk-pk) on a 14V bus.
      >
      >   Above and below those frequencies, the allowable/exoected
      >   noise levels fall off. When you hook an oscilloscope to
      >   the bus, the best you can do is sample small features
      >   of the noise as illustrated in the first 5 figures. Further,
      >   you'll never see the pristine plots hypothesized in Figure 6.
      >
      >
      > [image: Emacs!]
      > Figure 8.
      >
      >   The most significant attribute of a DC power system is VOLTAGE.
      >   Referring again to Mil-STD-704 we find the plot above. Again,
      >   cut the voltage levels in half for a 14v system.
      >
      >   This figure suggests that any voltage vs. time condition
      >   below the upper trace . . . and above the lower trace . . .
      >   is a condition to be expected for designing and operating
      >   appliances powered from the DC system.
      >
      >   It's my wish that this narrative will give you some tools
      >   for critical review of any data presented by either operating
      >   or diagnostic instruments. Understanding characteristics
      >   signals present on the bus -AND- limits on the measuring
      >   instrument will go to better design, operation and diagnosis
      >   of your ship's DC power system.
      >
      >   Bob . . .
      >
      
________________________________________________________________________________
Subject: 
Re: Digital Industrial Scales Outlets
From: 
"juancax" <publiwebmaxter(at)gmail.com>
Date: 
Oct 06, 2017
      
      
      Great post. thanks for sharing us. pornofavela.com (http://pornofavela.com/)
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473383#473383
      
      
________________________________________________________________________________
Date: 
Oct 06, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: alternator whine
      
      At 08:37 PM 10/5/2017, you wrote:
      >
      >Hi Bob and others,
      >
      >My 182 has a noticeable alternator whine, about 
      >5kHz (I=99m guessing) at cruise rpm. I think 
      >it=99s worse recently than it used to be.
      >
      >Where and what should I start investigating?
      
         Does operation of any audio panel selector
         switch or setting of any radio or audio
         system volume control have an effect on
         the perceived noise?
      
      
         Bob . . . 
      
________________________________________________________________________________
Date: 
Oct 06, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Dual batteries or dual alternators?
      
      Hello my friends, thanks for the answers.
      Here I give more details so you can help me with my wiring...
      I'm building an RV-7, it is in the final process, I have just hang 
      the engine, an Aerosport Power WildCat IO382; with full FlyEFII 
      ignition and injection system, and dual Ecus.
      
      I consider batteries super confident, I have never had a battery 
      failure, but I have had an alternator failure 3 times in my life, 1 
      in the car and 2 in the aircraft... so I prefer 2 alternator, and one 
      odyssey battery.
      
          Generally speaking, B&C alternators are
          exceedingly long service lived. Failure
          rates are a tiny fraction of the fielded
          product. Most failures are due to installation
          error or external influences.
      
          A JUDICIOUSLY maintained battery is the
          single most reliable source of electrical
          energy in the airplane. A maintained battery
          simply doesn't fail in flight. When maintained
          batteries become unavailable in flight, it's
          a result of effects external to the battery.
      
      ... may be later if I desire to make a very long flight, or a very 
      difficult flight like going to the Antartica, then I would consider 
      going there with 2 batteries and 2 alternators, but not know... first 
      I have to put this machine in the air...
      
          With two alternators, the battery(ies)
          are no longer tasked with alternator-out
          endurance duties, hence they may be selected
          primarily for their ability to crank the
          engine and offer some stability to alternator
          performance.
      
      Said all this, I saw AeroElectric book and the Z-12 diagram. And I 
      already have all the components of that figure I bought everything in 
      B&C, including the stand by alternator for the vacuum pump (40 amps).
      
          The pad mounted alternator is fabricated from
          a 40A core . . . but if your pad is the
          legacy gear ratio to the crankshaft, then
          cruise rpm at the pad is on the order of 3700-
          3800 rpm . . . too low to realize the machine's
          full 40A output.
      
      My question is if this diagram would work with my dual Ecu's EFII, 
      how would I need to modify this, does anybody have a picture of the 
      distribution of the components into the aircraft, and the switches in 
      the cockpit??
      
         Is there a down-loadable installer's manual
         for your engine? It's difficult, if not
         foolish, to make recommendations without
         knowing the requirements/recommendations
         for all ship's electrical components, not
         the least of which is your engine.
      
      
         Bob . . . 
      
________________________________________________________________________________
From: 
Sebastien <cluros(at)gmail.com>
Date: 
Oct 06, 2017
Subject: 
Re: Voltmeter & Ammeter normal ranges
      
      Thank you Bob. Very good information and well presented. I'm looking
      forward to learning more about the capabilities and limits of these
      instruments.
      
      On Thu, Oct 5, 2017 at 10:03 PM, Bob Verwey  wrote:
      
      > Absolutely facinating and insightful to a neophyte like myself 
      >
      > On 05 Oct 2017 7:17 PM, "Robert L. Nuckolls, III" <
      > nuckolls.bob(at)aeroelectric.com> wrote:
      >
      >> At 08:32 AM 9/24/2017, you wrote:
      >>
      >> Exactly. Joe could you please confirm that the jpeg below is visible? If
      >> so it's obvious that while the voltage seems to be moving around a tiny
      >> bit, it never gets to the point which would allow the amperage shown. It's
      >> always above 14V. Also I checked some data with the engine shut down and
      >> while the amperage still wanders around it's 1 A or less (-5.5 to -6.5 A)
      >>
      >>
      >>  Digital data acquisition is fraught with
      >>  opportunity for confusion/error.  Depending
      >>  on how the variable is sampled, pre-filtered
      >>  and software filtered, data displayed or plotted
      >>  can take on the appearance of instability.
      >>
      >>  Unless you're measuring the output from something
      >>  like a battery . . . or a laboratory power supply,
      >>  the stimulus being observed will have some noise
      >>  on it. This is especially true of signals gathered
      >>  from the DC power system of any vehicle.
      >>
      >>  When I'm gathering data on relatively low frequency
      >>  events, my DAS pre-filtering is usually rolled
      >>  off at 10 Hz. Then interpretation software is
      >>  designed to do a 'rolling average' on sampled values.
      >>  For a DAS set up to gather 100 samples/second, we'll
      >>  buffer 16 samples in a memory stack, take the sum
      >>  of those values then divide by 16 for an average
      >>  of that 'packet' of data. When the next sample comes
      >>  in, we add the new value, throw away the oldest value
      >>  and do the average again.
      >>
      >>  This pre/post processing of data does a nice job
      >>  of ignoring the high frequency perturbations that
      >>  are riding on top of the value of interest. The
      >>  processed data plots are nice smooth lines that
      >>  are more meaningful.
      >>
      >>  I suspect that data plots taken from most
      >>  EIS systems have little pre-processing and no
      >>  post processing . . . so the traces are understandably
      >>  'ragged'. So while the voltage traces might
      >>  be interpreted as 'unstable', it's probable
      >>  that the system is operating normally.
      >>
      >>  Just for grins, I took the 'scope out to peek at
      >>  the 14v bus in Dr. Dee's '87 GMC Sierra. With
      >>  the 'scope set to 2.5S/div H and 2V/div V, we
      >>  get the following trace when cranking the engine.
      >> [image: []]
      >>
      >>   Figure 1.
      >>
      >>   Note that battery voltage starts to sag from
      >>   about 12.8 volts but takes a steeper slope
      >>   as the starter contactor is energized followed
      >>   by a profound drop to 8 volts as the contactor
      >>   closes.  A few milliseconds later, the voltage
      >>   rises to about 10v until the engine catches
      >>   approx 1.2S later and the alternator kicks
      >>   in . . . whereupon but bus rises to about
      >>   14.6V
      >>
      >> [image: []]
      >>   Figure 2.
      >>
      >>   In the next plot we see that the bus is 'steady'
      >>   at about 14.7V with the occasional perturbation
      >>   combined with some little 'spikes' with an amplitude
      >>   of 1 to 2 volts.
      >>
      >>   To get a closer look at the voltage in the
      >>   next plot, we need to turn up the 'scope sensitivity
      >>   and to to AC coupling:
      >>
      >> [image: []]
      >>  Figure 3.
      >>
      >>  With a vertical scale of 0.5V/div and horizontal
      >>  of 0.05S/div we can get a better look at the 'noise'.
      >>  This particular trace caught a 1.5v transient amongst
      >>  about 10 smaller artifacts.
      >>
      >>  We see that even when there are no obvious
      >>  transients, the horizontal line has 'thickness'.
      >>  Zooming in closer:
      >>
      >> [image: []]
      >>  Figure 4.
      >>
      >>  We find that the horizontal line is 'fuzzy' with
      >>  positive and negative going transients on the
      >>  order of 300mV peak.
      >>
      >>  Depending on where your digital data acquistion
      >>  system takese a 'snapshot', the sampled votlage
      >>  might appear to 'wobble' by as much as +/-0.5V.
      >>
      >>  Spreading out the major transients by a factor
      >>  of 20 . . .
      >>
      >>
      >> [image: []]
      >>  Figure 5.
      >>
      >>
      >>  Shows that they're about 400 microSeconds wide. These
      >>  plots offer a small peek into the nature of DC power
      >>  systems on vehicles.  A few weeks ago, a thread on
      >>  another list server offered this image suggesting
      >>  that the full-wave, rectified 3-phase alternator
      >>  would produce wave forms something along these lines . . .
      >>
      >> [image: []]
      >>
      >>  Figure 6.
      >>
      >>  Theoretically true, but  I've never seen so 'clean'
      >>  a picture in the wild . . .
      >>
      >>  Referring to Mil-Std-704 we learn that DC power systems
      >>  demonstrate a certain amount of noise (distortion)
      >>  under normal conditions. The document cites
      >>  the following plot for a 28v system (cut the
      >>  numbers in half for 14 volts).
      >>
      >> [image: []]
      >>
      >>   Figure 7.
      >>
      >>   Over the range of 1000 Hz (1 milliSecond period) and
      >>   10,000 Hz (100 uSecond), we should expect artifacts
      >>   of noise up to 0.5 VRMS (1.5 volts pk-pk) on a 14V bus.
      >>
      >>   Above and below those frequencies, the allowable/exoected
      >>   noise levels fall off. When you hook an oscilloscope to
      >>   the bus, the best you can do is sample small features
      >>   of the noise as illustrated in the first 5 figures. Further,
      >>   you'll never see the pristine plots hypothesized in Figure 6.
      >>
      >>
      >>
      >> [image: Emacs!]
      >> Figure 8.
      >>
      >>   The most significant attribute of a DC power system is VOLTAGE.
      >>   Referring again to Mil-STD-704 we find the plot above. Again,
      >>   cut the voltage levels in half for a 14v system.
      >>
      >>   This figure suggests that any voltage vs. time condition
      >>   below the upper trace . . . and above the lower trace . . .
      >>   is a condition to be expected for designing and operating
      >>   appliances powered from the DC system.
      >>
      >>   It's my wish that this narrative will give you some tools
      >>   for critical review of any data presented by either operating
      >>   or diagnostic instruments. Understanding characteristics
      >>   signals present on the bus -AND- limits on the measuring
      >>   instrument will go to better design, operation and diagnosis
      >>   of your ship's DC power system.
      >>
      >>   Bob . . .
      >>
      >
      
________________________________________________________________________________
Subject: 
Re: Daily List Digest Question
From: 
"David Lewis" <Davidlewisstart(at)gmail.com>
Date: 
Oct 06, 2017
      
      
      There are a couple of anomalies noticed when receiving the digest version of the
      list. One is the well understood and much discussed 'Emacs!' message in some
      of Bob's posts. Regarding the 'pages and pages' of unreadable text, I believe
      that may be associated with embedded images in a post that don't come through
      in the digest compilation.
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473398#473398
      
      
________________________________________________________________________________
From: 
GLEN MATEJCEK <fly4grins(at)gmail.com>
Date: 
Oct 07, 2017
Subject: 
Re: home wiring ground faults
      
      I've seen two pertinent miswirings.  One is having the ground and neutral
      connected together in a sub panel.  The other was putting one gfci
      downstream of another.  Both caused nuisance trips.  The first scenario is
      actually not uncommon with hot tubs.  All is well until the light is turned
      on, and then the gfci trips.  The second was a unique situation, and didn't
      manifest issues until years after the installation.
      
      Ymmv, few, yada yada...
      
________________________________________________________________________________
From: 
Alec Myers <alec(at)alecmyers.com>
Subject: 
Re: alternator whine
Date: 
Oct 07, 2017
      
      I did a little investigation yesterday - 
      No aircraft control affects the volume, except the volume control 
      directly on my headset. Even turning up the panel intercom volume 
      doesn=99t make any difference.
      
      
      > On Oct 6, 2017, at 10:30 AM, Robert L. Nuckolls, III 
       wrote:
      > 
      > At 08:37 PM 10/5/2017, you wrote:
      
      >> 
      >> Hi Bob and others,
      >> 
      >> My 182 has a noticeable alternator whine, about 5kHz (I=C3=A2=C2=C2=99
      m guessing) at cruise rpm. I think it=C3=A2=C2=C2=99s worse recently 
      than it used to be.
      >> 
      >> Where and what should I start investigating?
      > 
      >   Does operation of any audio panel selector
      >   switch or setting of any radio or audio
      >   system volume control have an effect on
      >   the perceived noise?
      > 
      > 
      >   Bob . . .
      > 
      
      
________________________________________________________________________________
Subject: 
Re: IR Alternator Voltage
From: 
"eschlanser" <eschlanser(at)yahoo.com>
Date: 
Oct 07, 2017
      
      
      > Sorry, I don't have the model specifics with me (can get later) but off
      > the top are there ways to adjust the output of IR type alternators or is
      > that a factory setting that cannot be changed? Is this an "it depends"
      > item?
      > 
      > 
      
      
      >  Probably not. I've never seen an adjustable regulator on
      >    an internally regulated machine. In fact, most external
      >    regulators were not adjustable either.
      
      
         
      > Before you take a wrench to the airplane, check the
      >    alternator output voltage at the alternator's b-terminal.
      >    The internal regulator senses b-terminal voltage and
      >    there MAY be a difference. You can probably buy a
      >    replacement regulator but depending on the alternator,
      >    it might be lest hassle/expense to trade it in.
      > 
      > 
      >    Bob . . .
      [/quote]
      
      I'm having the same need as the OP. That is, low displayed voltage from my IR alternator.
      I understand the directions but do not know how to implement them on
      a running airplane. This may be an electric 101 question. How do I physically
      check the alternator output voltage at the alternator's b-terminal? I don't
      have anyone willing to reach in and hold the voltmeter test leads on a running
      airplane.
      
      
      Eric
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473408#473408
      
      
________________________________________________________________________________
Date: 
Oct 07, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: alternator whine
      
      At 01:40 PM 10/7/2017, you wrote:
      >I did a little investigation yesterday -
      >No aircraft control affects the volume, except 
      >the volume control directly on my headset. Even 
      >turning up the panel intercom volume doesn=99t make any difference.
      
         Aha!  Good data.
      
         check to see if your headset jacks are grounded
         to airframe locally. Depending on age of your Cessna,
         that could have been standard practice at the factory.
      
         If grounded locally, mount the jack on an insulating
         washer and run a ground wire all the way back to
         the radio grounds.  You may find that there already
         is a ground wire but no washer . . . in which case
         adding the washer is likely to fix it.
      
      
         Bob . . . 
      
________________________________________________________________________________
Date: 
Oct 07, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: IR Alternator Voltage
      
      
      >
      >
      >I'm having the same need as the OP. That is, low displayed voltage 
      >from my IR alternator. I understand the directions but do not know 
      >how to implement them on a running airplane. This may be an electric 
      >101 question. How do I physically check the alternator output 
      >voltage at the alternator's b-terminal? I don't have anyone willing 
      >to reach in and hold the voltmeter test leads on a running airplane.
      >
      >
      >Eric
      
         Easy, don't PROBE the points of interest, CLIP them.
         I very seldom use 'probes' for any measurement, virtually
         all signals of interest need to be sampled while your
         hands are fully occupied with other tasks.
      
      Emacs!
      
      
         I have several dozen clip leads sets in the various
         tool boxes and workbenches. As a general rule, I make
         them up with a minimum 36" long. I have a couple of
         sets that are 10' long. I once built a special clip
         set about 40' long to watch a voltage in the 'hell hole'
         of a Beechjet whilst I was fiddling with knobs in
         the cockpit.
      
         Built yourself a 10' pair. Clip to points of interest
         under the cowl then sit in the cockpit taking voltage
         readings ar various rpm and loads. Tape the leads
         to under side of cowl to keep prop wash from shaking
         the wires so bad that it pulls the clips off . . .
         been there, done that.
      
      
         Bob . . . 
      
________________________________________________________________________________
From: 
Alec Myers <alec(at)alecmyers.com>
Date: 
Oct 07, 2017
Subject: 
Re: alternator whine
      
      Awesome. I=99ll give it a try, and report back.
      
      On Oct 7, 2017, at 19:33, Robert L. Nuckolls, III <nuckolls.bob@aeroelectric
      .com> wrote:
      
      At 01:40 PM 10/7/2017, you wrote:
      > I did a little investigation yesterday - 
      > No aircraft control affects the volume, except the volume control directly
       on my headset. Even turning up the panel intercom volume doesn=99t ma
      ke any difference.
      
        Aha!  Good data. 
      
        check to see if your headset jacks are grounded
        to airframe locally. Depending on age of your Cessna,
        that could have been standard practice at the factory.
      
        If grounded locally, mount the jack on an insulating
        washer and run a ground wire all the way back to
        the radio grounds.  You may find that there already
        is a ground wire but no washer . . . in which case
        adding the washer is likely to fix it.
      
      
        Bob . . .
      
________________________________________________________________________________
From: 
Charlie England <ceengland7(at)gmail.com>
Subject: 
Slobovia Pumpkin Drop!
Date: 
Oct 08, 2017
      
      Hoping to see y'all on Nov 4. Come on down!
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
________________________________________________________________________________
From: 
"Michael Easley" <mikeeasley(at)aol.com>
Subject: 
Dual Power Inputs, Dual Buss Electrical System
Date: 
Oct 11, 2017
      
      I'm redoing my panel in my aircraft which I built 15 years ago with a Z-14
      electrical system.  I'm installing a Garmin G3X panel and all the associated
      boxes.  Most of them have the capability to wire for 2 separate power
      sources.  With dual buss with crossfeed, I'm wondering if there is any
      significant benefit to having two CBs and two power feeds.  I can think of a
      couple failure modes, but they seem remote.  There is also a configuration
      using a backup battery on the second power feed, maybe that's a better
      choice.  Thanks in advance for the feedback.
      
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Dual Power Inputs, Dual Buss Electrical   System
      
      At 08:37 AM 10/11/2017, you wrote:
      >I'm redoing my panel in my aircraft which I built 15 years ago with 
      >a Z-14 electrical system.  I'm installing a Garmin G3X panel and all 
      >the associated boxes.  Most of them have the capability to wire for 
      >2 separate power sources.  With dual buss with crossfeed, I'm 
      >wondering if there is any significant benefit to having two CBs and 
      >two power feeds.  I can think of a couple failure modes, but they 
      >seem remote.  There is also a configuration using a backup battery 
      >on the second power feed, maybe that's a better choice.  Thanks in 
      >advance for the feedback.
      >
      
         With two batteries, two alternators and crossfeed,
         there is no value in exploiting the redundancy
         features you cited. Z14 has all that stuff built
         in.
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Constructing an automatic RCA video camera feed splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 11, 2017
      
      
      Hi Bob, et al.
      
      I recently purchased a GRT EFIS for the Long-EZ that I'm building.  The GRT EFIS
      has an option to connect up a single video feed to it via USB (in this case,
      my 4-port USB hub).  I've tested out some mini-video cameras I picked up off
      of Amazon that are about the size of a dime, and the picture quality is great
      for what I want to use them for.
      
      As I'm sure many of you know, most canard aircraft have fuel site gages in the
      back seat area.  Look inside these birds parked on the ramp and invariable you'll
      find a mirror, which is what canard pilots often use to check out their fuel
      site gages in the back.  I figured with such diminutive sizes on these cameras,
      why not hook one up focused on each site gage, and while I'm at it point
      a 3rd camera looking aft at the engine from atop the pilot head rest.  A 4th camera
      on the bottom CL looking aft would be round out my initial camera installation.
      
      
      My issue is that I would like to have a timed cycle display of each of these camera
      views in a little window on my EFIS (GRT has taken care of the EFIS display
      part), say 3-5 seconds per camera.  However, every RCA jack 4-into-1 video
      channel selector I have found --while cheap-- are bulky plastic housing a large
      mechanical switch to select the video channel.... mainly used by video gamers.
      I talked with GRT and any machinations going on with the video feed is fine,
      as long as only one physical RCA video jack is presented to their USB video
      input device.  
      
      I would like to construct a 4x (or more) channel IN and 1x RCA jack channel out
      device that is small, and automatically cycles through each camera view, again
      for 3-5 seconds.  Adjustable viewing times would be good, and maybe a manual
      pause or cycle button would be good as well.  
      
      Does anybody know of a device like this that exists?  Would the circuitry for something
      like this be too complicated?  Finally, is there any detriment to swapping
      out the thicker RCA cabling with 24 AWG shielded wire?
      
      Thanks!
      Wade
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473469#473469
      
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera feed
      splitter
      
      
         My Byte Thrasher in Chief (Paul Fisher) helped me craft
         a universal, 4 step timer chip described here:
      
      http://tinyurl.com/y96wc8rh
      
         I've used this chip on several applications and
         it's easily adapted to your task. The link
         above contains a description of the chip which
         can be supplied you to at no cost with what
         ever time intervals you wish programmed in.
         Further, there is a hold function on the chip
         that can be used to pause switching in the
         current state.
      
         Somewhere in the pile on my bench, I have some of the
         development ecbs shown on the linked page.
         You could assemble one with driver transistors
         and build an array of relays to handle video
         switching.
      
         Alternatively, could cut-n-paste the ECB
         artwork into a new board that would eliminate
         the driver transistors and drive some really
         small, surface mounted relays to handle
         video switching.
      
      http://tinyurl.com/ybhnq6m6
      
         It wouldn't take much time to lay out the
         board . . . but I'm up to my eyeballs right
         now in projects that need to be cleared
         off the bench. If anyone wants to take the
         data posted and lay out a new board, I'd
         be pleased to critique the work product before
         boards are ordered.
      
      
      Does anybody know of a device like this that exists?  Would the 
      circuitry for something like this be too complicated?  Finally, is 
      there any detriment to swapping out the thicker RCA cabling with 24 
      AWG shielded wire?
      
         That would be fine too. There are ECB
         mounted RCA jacks that could be incorporated
         into your video switcher board.
      
      
         Bob . . . 
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video     camera
      feed splitter
      
      
      >
      >   Somewhere in the pile on my bench, I have some of the
      >   development ecbs shown on the linked page.
      >   You could assemble one with driver transistors
      >   and build an array of relays to handle video
      >   switching.
      
         Found one . . .
      Emacs!
      
      
         Bob . . . 
      
________________________________________________________________________________
From: 
Joel Ventura <ventura(at)brandeis.edu>
Date: 
Oct 11, 2017
Subject: 
Re: Constructing an automatic RCA video camera  feed
      splitter
      
      What cameras are you using?
      
      Thanks. --Joel
      
      
      On Wed, Oct 11, 2017 at 12:05 PM, Airdog77  wrote:
      
      >
      > Hi Bob, et al.
      >
      > I recently purchased a GRT EFIS for the Long-EZ that I'm building.  The
      > GRT EFIS has an option to connect up a single video feed to it via USB (in
      > this case, my 4-port USB hub).  I've tested out some mini-video cameras I
      > picked up off of Amazon that are about the size of a dime, and the picture
      > quality is great for what I want to use them for.
      >
      >
      > Thanks!
      > Wade
      >
      > --------
      > Airdog
      > Wade Parton
      > Building Long-EZ 916WP
      > www.longezpush.com
      >
      >
      > Read this topic online here:
      >
      > http://forums.matronics.com/viewtopic.php?p=473469#473469
      >
      >
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video     camera
      feed splitter
      
      
      >   Somewhere in the pile on my bench, I have some of the
      >   development ecbs shown on the linked page.
      >   You could assemble one with driver transistors
      >   and build an array of relays to handle video
      >   switching.
      
         Poked around a bit in the residual components
         and assemblies from other tasks. Ran across this
         4-relay assembly that already has driver couplers
         and transistors. This board could be combined with
         the timer board (sans drivers) to get you
         75% of the way to video switching Nirvana . . .
      
      
      Emacs!
      
      
         You'd need to box the thing up with connectors
         to mate with your external components. I'd probably
         fabricate a box about 3.5 square by 1.0 thick with
         a d-sub connector on it.
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera  feed
      splitter
From: 
C&K <yellowduckduo(at)gmail.com>
Date: 
Oct 11, 2017
      
      
      I'm curious why you'd consider driving relays instead of a 4 into 1 
      analog switching chip.
      Ken
      
      On 11/10/2017 2:22 PM, Robert L. Nuckolls, III wrote:
      >>
      >>   Somewhere in the pile on my bench, I have some of the
      >>   development ecbs shown on the linked page.
      >>   You could assemble one with driver transistors
      >>   and build an array of relays to handle video
      >>   switching.
      >
      >   Found one . . .
      > Emacs!
      >
      >
      >   Bob . . .
      >
      
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera  feed
      splitter
      
      At 02:10 PM 10/11/2017, you wrote:
      >
      >I'm curious why you'd consider driving relays instead of a 4 into 1 
      >analog switching chip.
      
         If I were laying out a board and doing it myself,
         that's the first approach to be considered. Haven't
         played video lately so I'm unsure what the constraints
         might be for solid-state switching. Some applications
         and switch choices called for +/- power supplies
         which complicates the circuitry.
      
         The next choice to consider would be taking the barefoot
         chip and using digital outputs to drive low current
         form A relays directly. This would let us craft the
         1:4 sequential switcher with a grand total of 11
         parts and no concerns for DC levels on the video
         lines.
      
         The approach being offered is the short-path, minimum
         risk to success for a neophyte builder using junkbox
         parts.
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera  feed
      splitter
From: 
Charlie England <ceengland7(at)gmail.com>
Date: 
Oct 11, 2017
      
      
      On 10/11/2017 11:05 AM, Airdog77 wrote:
      >
      > Hi Bob, et al.
      >
      > I recently purchased a GRT EFIS for the Long-EZ that I'm building.  The GRT EFIS
      has an option to connect up a single video feed to it via USB (in this case,
      my 4-port USB hub).  I've tested out some mini-video cameras I picked up off
      of Amazon that are about the size of a dime, and the picture quality is great
      for what I want to use them for.
      >
      > As I'm sure many of you know, most canard aircraft have fuel site gages in the
      back seat area.  Look inside these birds parked on the ramp and invariable you'll
      find a mirror, which is what canard pilots often use to check out their
      fuel site gages in the back.  I figured with such diminutive sizes on these cameras,
      why not hook one up focused on each site gage, and while I'm at it point
      a 3rd camera looking aft at the engine from atop the pilot head rest.  A 4th
      camera on the bottom CL looking aft would be round out my initial camera installation.
      >
      > My issue is that I would like to have a timed cycle display of each of these
      camera views in a little window on my EFIS (GRT has taken care of the EFIS display
      part), say 3-5 seconds per camera.  However, every RCA jack 4-into-1 video
      channel selector I have found --while cheap-- are bulky plastic housing a large
      mechanical switch to select the video channel.... mainly used by video gamers.
      I talked with GRT and any machinations going on with the video feed is fine,
      as long as only one physical RCA video jack is presented to their USB video
      input device.
      >
      > I would like to construct a 4x (or more) channel IN and 1x RCA jack channel out
      device that is small, and automatically cycles through each camera view, again
      for 3-5 seconds.  Adjustable viewing times would be good, and maybe a manual
      pause or cycle button would be good as well.
      >
      > Does anybody know of a device like this that exists?  Would the circuitry for
      something like this be too complicated?  Finally, is there any detriment to swapping
      out the thicker RCA cabling with 24 AWG shielded wire?
      >
      > Thanks!
      > Wade
      >
      > --------
      > Airdog
      > Wade Parton
      > Building Long-EZ 916WP
      > www.longezpush.com
      >
      There was an article on a diy 8 channel video/audio using a bank of 
      solid state switches about 30 years ago in, if memory serves, Byte 
      Magazine. Much easier to buy off the rack these days.
      
      How about
      http://www.ebay.com/itm/4-CH-Channel-DVR-CCTV-Quad-Video-Camera-Processor-System-Kit-Splitter-Switcher-/391156611012?epid=1839817989&hash=item5b12c037c4:g:Op4AAOxyuR5TbcoS
      
      or
      http://www.ebay.com/itm/4-Channel-Automatic-Video-Switcher-for-Automotive-Cars-/172847332805?hash=item283e80fdc5:g:UW8AAOSwmhJZqR5f
      
      or, ask GRT why this won't work
      http://www.ebay.com/itm/4-Channel-BNC-RCA-To-USB-Converter-DVR-Adapter-Camera-Video-Switcher-/191162842864?hash=item2c82317ef0:g:D3MAAOSwstxVJd7K
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera  feed
      splitter
From: 
C&K <yellowduckduo(at)gmail.com>
Date: 
Oct 11, 2017
      
      
      Thanks for the explanation.
      I've never played with USB video but I think the D+  and D-  USB signals 
      are both normally only positive with respect to the power ground and 
      that the signal information is differential between those pins. Makes me 
      wonder if dual pole relays would be needed.
      Ken
      
      On 11/10/2017 5:28 PM, Robert L. Nuckolls, III wrote:
      > At 02:10 PM 10/11/2017, you wrote:
      >>
      >> I'm curious why you'd consider driving relays instead of a 4 into 1 
      >> analog switching chip.
      >
      >   If I were laying out a board and doing it myself,
      >   that's the first approach to be considered. Haven't
      >   played video lately so I'm unsure what the constraints
      >   might be for solid-state switching. Some applications
      >   and switch choices called for +/- power supplies
      >   which complicates the circuitry.
      >
      >   The next choice to consider would be taking the barefoot
      >   chip and using digital outputs to drive low current
      >   form A relays directly. This would let us craft the
      >   1:4 sequential switcher with a grand total of 11
      >   parts and no concerns for DC levels on the video
      >   lines.
      >
      >   The approach being offered is the short-path, minimum
      >   risk to success for a neophyte builder using junkbox
      >   parts.
      >
      >
      >   Bob . . .
      >
      
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera  feed
      splitter
      
      At 05:34 PM 10/11/2017, you wrote:
      >
      >Thanks for the explanation.
      >I've never played with USB video but I think the D+  and D-  USB 
      >signals are both normally only positive with respect to the power 
      >ground and that the signal information is differential between those 
      >pins. Makes me wonder if dual pole relays would be needed.
      >Ken
      
         I was driving off the original posting
         that talked about RCA connectors which
         I chased down the single-wire, analog
         rabbit hole.
      
         If were talking about USB digital data,
         yeah, that's easily managed in the +5v
         world . . .
      
      
         Bob . . . 
      
________________________________________________________________________________
Date: 
Oct 11, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera  feed
      splitter
      
      
      >There was an article on a diy 8 channel video/audio using a bank of 
      >solid state switches about 30 years ago in, if memory serves, Byte 
      >Magazine. Much easier to buy off the rack these days.
      >
      >How about
      
        
      
        These appear to be capable video switches. We'd
        still need to integrate some form of sequential switching
        timer . . .
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera  feed
      splitter
From: 
Charlie England <ceengland7(at)gmail.com>
Date: 
Oct 11, 2017
      
      On 10/11/2017 6:10 PM, Robert L. Nuckolls, III wrote:
      >> There was an article on a diy 8 channel video/audio using a bank of 
      >> solid state switches about 30 years ago in, if memory serves, Byte 
      >> Magazine. Much easier to buy off the rack these days.
      >>
      >> How about
      >
      > 
      >
      > These appear to be capable video switches. We'd
      > still need to integrate some form of sequential switching
      > timer . . .
      >
      >  Bob . . .
      >
      Don't remember if any of those links I sent include sequential 
      switching, but I saw at least one on ebay that did include that in its 
      functionality. Price point was in the same ~$50 range.
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera  feed
      splitter
From: 
chris smale <csmale(at)bak.rr.com>
Date: 
Oct 11, 2017
      
      
      On 10/11/17 09:05, Airdog77 wrote:
      >
      > Hi Bob, et al.
      >
      > I recently purchased a GRT EFIS for the Long-EZ that I'm building.  The GRT EFIS
      has an option to connect up a single video feed to it via USB (in this case,
      my 4-port USB hub).  I've tested out some mini-video cameras I picked up off
      of Amazon that are about the size of a dime, and the picture quality is great
      for what I want to use them for.
      >
      > As I'm sure many of you know, most canard aircraft have fuel site gages in the
      back seat area.  Look inside these birds parked on the ramp and invariable you'll
      find a mirror, which is what canard pilots often use to check out their
      fuel site gages in the back.  I figured with such diminutive sizes on these cameras,
      why not hook one up focused on each site gage, and while I'm at it point
      a 3rd camera looking aft at the engine from atop the pilot head rest.  A 4th
      camera on the bottom CL looking aft would be round out my initial camera installation.
      >
      > My issue is that I would like to have a timed cycle display of each of these
      camera views in a little window on my EFIS (GRT has taken care of the EFIS display
      part), say 3-5 seconds per camera.  However, every RCA jack 4-into-1 video
      channel selector I have found --while cheap-- are bulky plastic housing a large
      mechanical switch to select the video channel.... mainly used by video gamers.
      I talked with GRT and any machinations going on with the video feed is fine,
      as long as only one physical RCA video jack is presented to their USB video
      input device.
      >
      > I would like to construct a 4x (or more) channel IN and 1x RCA jack channel out
      device that is small, and automatically cycles through each camera view, again
      for 3-5 seconds.  Adjustable viewing times would be good, and maybe a manual
      pause or cycle button would be good as well.
      >
      > Does anybody know of a device like this that exists?  Would the circuitry for
      something like this be too complicated?  Finally, is there any detriment to swapping
      out the thicker RCA cabling with 24 AWG shielded wire?
      >
      > Thanks!
      > Wade
      >
      > --------
      > Airdog
      > Wade Parton
      > Building Long-EZ 916WP
      > www.longezpush.com
      >
      >
      > Read this topic online here:
      >
      > http://forums.matronics.com/viewtopic.php?p=473469#473469
      >
      >
      If you have some computer skill or know someone who has, the raspberry 
      pi can do what you want.
      
      csmale(at)bak.rr.com
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 12, 2017
      
      
      Thanks Bob.
      
      I'll take a look at all this and try to digest!  :)
      
      I see a number of responses to my question that I need to go through as well....
      normally I get an email update on a post, but didn't this time so I have some
      reading to do!
      
      Regards,
      Wade
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473489#473489
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 12, 2017
      
      
      Awesome, looks great!
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473490#473490
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 12, 2017
      
      
      Sorry for my delayed response back.  Again, didn't get any of the normal email
      notifications that responses were being made to my question... thanks all!
      
      The camera I'm using is a cheap 1/4" 600TVL from Amazon... the two I bought are
      no longer being sold, but this is close: https://tinyurl.com/yckqk3dh
      
      Yes, I'm looking at video RCA jack OUT feed that will then go into box that hooks
      to USB.  So I don't need to mess with anything USB as far as video is concerned.
      
      I need to dig into all this info to figure out a way ahead.
      
      Bob, how would I go about getting boards like the one you posted pics of?
      
      Regards,
      Wade
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473491#473491
      
      
________________________________________________________________________________
Date: 
Oct 12, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera
      feed splitter
      
      At 03:03 AM 10/12/2017, you wrote:
      >
      >Sorry for my delayed response back.  Again, didn't get any of the 
      >normal email notifications that responses were being made to my 
      >question... thanks all!
      >
      >The camera I'm using is a cheap 1/4" 600TVL from Amazon... the two I 
      >bought are no longer being sold, but this is close: 
      >https://tinyurl.com/yckqk3dh
      
         There's quite an array of products offered
         in these devices. I read some comments that
         complained of poor/no instructions. Also,
         some devices advertised as 3-12v supply were
         indeed 3.3 volts only . . . anything more
         smoked them.
      
      
      >Yes, I'm looking at video RCA jack OUT feed that will then go into 
      >box that hooks to USB.  So I don't need to mess with anything USB as 
      >far as video is concerned.
      >
      >I need to dig into all this info to figure out a way ahead.
      >
      >Bob, how would I go about getting boards like the one you posted pics of?
      
         Give me an address . . . I'll mail them
         to you. How are your soldering/fabrication
         skills? You'll have to chase down some
         parts and package the stuff up in some
         suitable enclosure.
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Re: Dual Power Inputs, Dual Buss Electrical System
From: 
Bill Watson <Mauledriver(at)nc.rr.com>
Date: 
Oct 12, 2017
      
      On 10/11/2017 11:09 AM, Robert L. Nuckolls, III wrote:
      > At 08:37 AM 10/11/2017, you wrote:
      >> Im redoing my panel in my aircraft which I built 15 years ago with a 
      >> Z-14 electrical system. Im installing a Garmin G3X panel and all the 
      >> associated boxes. Most of them have the capability to wire for 2 
      >> separate power sources. With dual buss with crossfeed, Im wondering 
      >> if there is any significant benefit to having two CBs and two power 
      >> feeds. I can think of a couple failure modes, but they seem remote. 
      >> There is also a configuration using a backup battery on the second 
      >> power feed, maybe thats a better choice. Thanks in advance for the 
      >> feedback.
      >
      >  With two batteries, two alternators and crossfeed,
      >  there is no value in exploiting the redundancy
      >  features you cited. Z14 has all that stuff built
      >  in.
      >
      >  Bob . . .
      >
      I have a Z-14 and agree. There are even some potential disadvantages.
      
      I originally connected my (3) GRT EFISs to one bus and not incidentally, 
      the engine starter circuit to the other bus. That configuration 
      combined with an inadequate light weight starter originally supplied 
      with the 6 cylinder IO-540 on the RV-10, meant that cross fed starts 
      would sometimes reboot the GRTs. And starting with just 1 battery was 
      marginal in cold weather. Given that I had no on/off switch for the 
      GRTs, this was inconvenient given the boot time required. And it turned 
      out that early versions of the GRT code did not like to have their boot 
      sequence interrupted though that problem was fixed in later releases of 
      the code.
      
      Ideally as Bob has explained, one wants to start with the batteries 
      cross-fed to keep stress on the batteries to a minimum. Then to do 
      normal flight operations with 2 separate buses which makes any failure 
      identification easier and would keep any damaging component isolated.
      
      The other capability I wanted from my Z-14 was to be able to run my 
      panel for an extended period of time on occasion without concern for 
      having enough juice for a subsequent engine start. this is where the 
      main disadvantage might lie. The GRTs are capable of connecting to up 
      to 3 power supplies. At one point I used 2 of those inputs to connect 
      them to both buses. That was a mistake because I found that my ability 
      to run the panel for an extended period was diminished. That created 
      several problematic scenarios that I just shouldn't have had to deal with.
      
      In other words, the Z-14 gave me a lot of flexibility as long as I 
      connect individual components to one bus or the other. It allows one to 
      identify and isolate problem components and flexibly manage one's 
      batteries if desired. If you crossfeed individual components at the 
      component, you give some of that capability away with little if anything 
      gained.
      
      Post Script: Replacing the starter eliminated all problems with cross 
      fed and single battery starts. Returning to a single power supply on a 
      single bus for each GRT gave me back the battery management flexibility.
      
      Bill "I love my Z-14" Watson
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 12, 2017
      
      
      Bob,
      
      Thanks a ton! I'll email you my address.
      
      Soldering skills are not horrible.  Have done very little on circuit boards, but
      I have managed small stuff with pretty good results.
      
      I tested out the camera hooked up to my TV using a 12V battery and the picture
      was really good for such a small camera.  That's when I decided to press forward
      with these mini cameras.
      
      Regards,
      Wade
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473496#473496
      
      
________________________________________________________________________________
From: 
<jim(at)PoogieBearRanch.com>
Subject: 
Re: Constructing an automatic RCA video camera
      feed  splitter
Date: 
Oct 12, 2017
      
      
      Pretty cool idea to use the mini-camera with the GRT EFIS. I'm building
      a taildragger (Bearhawk Patrol) and am considering using a camera like
      this for "taxi assistance" since the engine/cowl somewhat obscures
      what's in front of you. Not that this is a replacement for S-turns, but
      just another tool in the toolbox. At a price of $8-10, why not use it to
      add to the situational awareness?
      
      Jim Parker
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 12, 2017
      
      
      Hey Jim,
      
      Definitely! It really is a neat little feature.  
      
      Be advised that the optional module & software to link into your EFIS runs $150
      from GRT.
      
      Cheers,
      Wade
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473498#473498
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera
      feed splitter
From: 
Charlie England <ceengland7(at)gmail.com>
Date: 
Oct 12, 2017
      
      
      On 10/12/2017 11:30 AM, Airdog77 wrote:
      >
      > Hey Jim,
      >
      > Definitely! It really is a neat little feature.
      >
      > Be advised that the optional module & software to link into your EFIS runs $150
      from GRT.
      >
      > Cheers,
      > Wade
      >
      Or, there's plan B: a $10 USB camera & a $15 android cell phone.
      
      :-)
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
      
________________________________________________________________________________
Date: 
Oct 12, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Dual Power Inputs, Dual Buss Electrical   System
      
      
      I have a Z-14 and agree.  There are even some potential disadvantages.
      
      I originally connected my (3) GRT EFISs to one bus and not 
      incidentally, the engine starter circuit to the other bus.  That 
      configuration combined with an inadequate light weight starter 
      originally supplied with the 6 cylinder IO-540 on the RV-10, meant 
      that cross fed starts would sometimes reboot the GRTs.  And starting 
      with just 1 battery was marginal  in cold weather.  Given that I had 
      no on/off switch for the GRTs, this was inconvenient given the boot 
      time required.  And it turned out that early versions of the GRT code 
      did not like to have their boot sequence interrupted though that 
      problem was fixed in later releases of the code.
      
      Ideally as Bob has explained, one wants to start with the batteries 
      cross-fed to keep stress on the batteries to a minimum.  Then to do 
      normal flight operations with 2 separate buses which makes any 
      failure identification easier and would keep any damaging component isolated.
      
      The other capability I wanted from my Z-14 was to be able to run my 
      panel for an extended period of time on occasion without concern for 
      having enough juice for a subsequent engine start.  this is where the 
      main disadvantage might lie.  The GRTs are capable of connecting to 
      up to 3 power supplies.  At one point I used 2 of those inputs to 
      connect them to both buses.  That was a mistake because I found that 
      my ability to run the panel for an extended period was 
      diminished.  That created several problematic scenarios that I just 
      shouldn't have had to deal with.
      
      In other words, the Z-14 gave me a lot of flexibility as long as I 
      connect individual components to one bus or the other.  It allows one 
      to identify and isolate problem components and  flexibly manage one's 
      batteries if desired.  If you crossfeed individual components at the 
      component, you give some of that capability away with little if 
      anything gained.
      
      Post Script: Replacing the starter eliminated all problems with cross 
      fed and single battery starts.  Returning to a single power supply on 
      a single bus for each GRT gave me back the battery management flexibility.
      
      Bill "I love my Z-14" Watson
      
      
         Bill mentions a starter replacement . . . what
         kind of starter was removed and what was
         the replacement?
      
         This trace I captured of my 87 GMC pickup
         was no doubt produced by inrush from a wound-
         field starter. Here we see that the bus
         falls to 8v for a few hundred microseconds.
      
      
      []
      
      
         Figure 1.
      
         I suspect that my younger cars may have PM starter
         motors. I'll look into that.
      
         We had some discussions at B&C many years ago about
         the market shift of permanent magnet starter motors.
         We elected not to join the parade . . . primarily
         because the wound field motor had lower inrush
         currents and offered better cold weather cranking
         efficiency when the battery was being degraded
         by the cold weather.
      
      
      Emacs!
      
      Figure 8.
      
         At the risk of being redundant, I'm repeating an assertion
         that was offered some years ago when engine cranking inrush
         reboots first raised their heads . . . I think it was back
         in the days of Blue Mountain market roll out.
      
         At that time, I posted the image above excerpted from
         Mil-STD-704/DO-160 assertions suggesting that suppliers to
         the industry should expect power perturbations over the
         constellation of conditions illustrated.
      
         Since that time, a number of processor based products have been
         introduced to the market that re-boot when the bus falls
         into normal/expected regions during engine start. While
         the condition doesn't damage the appliance, it does
         interrupt normal operations until the thing stands back
         up. Intuitively, I believe it's possible to design this
         characteristic out of most such products  . . . but until
         and unless the marketplace makes their desires known to
         suppliers, nothing will change.
      
         In the mean time, consumers of such products are obliged
         to make fundamental changes to power system architectures
         to accommodate an appliance that might well have been
         designed for airplane friendly operations in the first
         place.  It wouldn't be out of line for Listers who
         own such products to put the manufacturers on notice
         that they've stubbed their toe.
      
         Fee free to reference my writings. I'm also willing
         to talk with any party interested in upgrading their
         product. Give 'em my phone number too if you like.
      
         Bob . . .  
      
________________________________________________________________________________
Date: 
Oct 12, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera
      feed  splitter
      
      At 11:22 AM 10/12/2017, you wrote:
      >
      >Pretty cool idea to use the mini-camera with the GRT EFIS. I'm building
      >a taildragger (Bearhawk Patrol) and am considering using a camera like
      >this for "taxi assistance" since the engine/cowl somewhat obscures
      >what's in front of you. Not that this is a replacement for S-turns, but
      >just another tool in the toolbox. At a price of $8-10, why not use it to
      >add to the situational awareness?
      
         I've rented some cars with back-up cameras . . . pretty
         handy. Why not a taxi forward camera?
      
      
         Bob . . . 
      
________________________________________________________________________________
From: 
<mike(at)vision499.com>
Subject: 
Slickstart - Magneto booster
Date: 
Oct 13, 2017
      
      Hello all,
      
      
      I recently bought a used Slickstart magneto booster on e-bay and am not sure
      to how to test it?
      
      
      Any ideas?
      
      
      Thanks
      
      
      Mike
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
________________________________________________________________________________
Date: 
Oct 13, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Slickstart - Magneto booster
      
      At 10:00 AM 10/13/2017, you wrote:
      >Hello all,
      >
      >I recently bought a used Slickstart magneto booster on e-bay and am 
      >not sure to how to test it?
      >
      >Any ideas?
      >
      >Thanks
      >
      >Mike
      
      
        See http://tinyurl.com/ycbhqael
      
      
         Bob . . . 
      
________________________________________________________________________________
From: 
<mike(at)vision499.com>
Subject: 
Slickstart - Magneto booster
Date: 
Oct 13, 2017
      
      Thanks Bob,
      
      
      Much appreciated
      
      
      Mike
      
      
      From: owner-aeroelectric-list-server(at)matronics.com
      [mailto:owner-aeroelectric-list-server(at)matronics.com] On Behalf Of Robert L.
      Nuckolls, III
      Sent: October 13, 2017 9:46 AM
      Subject: Re: AeroElectric-List: Slickstart - Magneto booster
      
      
      At 10:00 AM 10/13/2017, you wrote:
      
      
      Hello all,
      
      I recently bought a used Slickstart magneto booster on e-bay and am not sure
      to how to test it?
      
      Any ideas?
      
      Thanks
      
      Mike
      
      
       See http://tinyurl.com/ycbhqael
      
      
        Bob . . . 
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
________________________________________________________________________________
Subject: 
Re: Dual Power Inputs, Dual Buss Electrical System
From: 
Bill Watson <Mauledriver(at)nc.rr.com>
Date: 
Oct 13, 2017
      
      On 10/12/2017 2:46 PM, Robert L. Nuckolls, III wrote:
      >
      > Post Script: Replacing the starter eliminated all problems with cross 
      > fed and single battery starts. Returning to a single power supply on 
      > a single bus for each GRT gave me back the battery management 
      > flexibility.
      >
      > Bill "I love my Z-14" Watson
      >
      >
      >  Bill mentions a starter replacement . . . what
      >  kind of starter was removed and what was
      >  the replacement?
      >
      The starter that was removed was the Sky-Tec 149-12LS Flyweight Starter.
      I replaced it with the Sky-Tec 149NL.
      
      The LS came as the standard configuration of the Lycoming IO-540 for 
      the RV10 one could order through Vans back around 2009. People in the 
      RV10 community quickly determined this was not a good combination. Even 
      with 2 fully charged 680s, the starter would not consistently turn 
      through the first compression stroke when cold - one had to learn to 
      'bounce it' through the first compression stroke. This was SOP on cold 
      days but it never actually failed to start the engine. And it routinely 
      caused my (3) unswitched EFISs to reboot if I had both buses crossfed, 
      even if it did pull through the first compression stroke.
      
      Lycoming and Sky-Tech came to the same conclusion at the time and 
      specifically recommended that the LS is not a good starter for this 
      application. For a period of time both companies were taking exchanges 
      of the the LS for the NL at no charge. (Sky Tec now offers an XLT model 
      as an updated replacement for the LS. Some RV10 builders used the HT 
      model but reported similar problems.)
      
      When I replaced it with the NL, it was immediately apparent that the NL 
      turned slower but with much greater 'authority'. Even starting on one 
      battery, switched so that it ran on the same bus as the (3) EFISs, the 
      EFISs didn't reboot. Starts are now a no-brainer.
      
      
      ---
      This email has been checked for viruses by Avast antivirus software.
      https://www.avast.com/antivirus
      
________________________________________________________________________________
Date: 
Oct 13, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Dual Power Inputs, Dual Buss Electrical   System
      
      At 12:36 PM 10/13/2017, you wrote:
      >On 10/12/2017 2:46 PM, Robert L. Nuckolls, III wrote:
      >>
      >>Post Script: Replacing the starter eliminated all problems with 
      >>cross fed and single battery starts.  Returning to a single power 
      >>supply on a single bus for each GRT gave me back the battery 
      >>management flexibility.
      >>
      >>Bill "I love my Z-14" Watson
      >>
      >>
      >>   Bill mentions a starter replacement . . . what
      >>   kind of starter was removed and what was
      >>   the replacement?
      >>
      >The starter that was removed was the Sky-Tec 149-12LS Flyweight Starter.
      >I replaced it with the Sky-Tec 149NL.
      >
      >The LS came as the standard configuration of the  Lycoming IO-540 
      >for the RV10 one could order through Vans back around 2009.  People 
      >in the RV10 community quickly determined this was not a good 
      >combination.  Even with 2 fully charged 680s, the starter would not 
      >consistently turn through the first compression stroke when cold - 
      >one had to learn to 'bounce it' through the first compression 
      >stroke.  This was SOP on cold days but it never actually failed to 
      >start the engine.  And it routinely caused my (3) unswitched EFISs 
      >to reboot if I had both buses crossfed, even if it did pull through 
      >the first compression stroke.
      >
      >Lycoming and Sky-Tech came to the same conclusion at the time and 
      >specifically recommended that the LS is not a good starter for this 
      >application.  For a period of time both companies were taking 
      >exchanges of the the LS for the NL at no charge.  (Sky Tec now 
      >offers an XLT model as an updated replacement for the LS.  Some RV10 
      >builders used the HT model but reported similar problems.)
      >
      >When I replaced it with the NL, it was immediately apparent that the 
      >NL turned slower but with much greater 'authority'.  Even starting 
      >on one battery, switched so that it ran on the same bus as the (3) 
      >EFISs, the EFISs didn't reboot.  Starts are now a no-brainer.
      
         thanks for the data dump!
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Eric Page" <edpav8r(at)yahoo.com>
Date: 
Oct 13, 2017
      
      
      I know Wade's specific request for camera switching has been solved, but it sounded
      like the sort of thing that might come up again so I thought I'd take a stab
      at it.
      
      So... here's an alternative for switching cameras to a monitor or EFIS input using
      a couple of voltage regulators and three ICs.  All components are through-hole.
      Everything on a single PCB, and no relays.
      
      Reference the attached schematic:
      
      An LM2931 5V linear regulator and a TC7660 charge pump provide +/-5V rails to power
      the circuit.  A 555 timer is configured in astable mode to provide an output
      with adjustable period of about 3 to 10 seconds.  This output is fed to the
      clock input of a CD4022B octal counter.  The clock signal can be interrupted
      by a SP3T ON-ON-(ON) switch to stop rotation of the cameras or advance them manually.
      Outputs 1-3 of the counter are connected to the logic inputs of an AD8184
      4:1 video multiplexer such that they cause the multiplexer to cycle through
      its four video inputs, connecting each in turn to the output.  RCA connectors
      provide four camera inputs and one video output.
      
      LM2931AZ 5V Linear Regulator: http://preview.tinyurl.com/yakjxubl
      TC7660CPA Inverting Charge Pump: http://preview.tinyurl.com/y7n7g6um
      ICM7555IPAZ CMOS Timer: http://preview.tinyurl.com/ybrvnnq2
      CD4022BE Octal Counter: http://preview.tinyurl.com/ycjsa46w
      AD8184ANZ 4:1 Video Multiplexer: http://preview.tinyurl.com/ybozz2nf
      SP3T Toggle Switch: http://preview.tinyurl.com/ybpazcu5
      
      Critiques?  Suggestions?
      
      If there's any interest, I can gin up a PCB.
      
      Eric
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473514#473514
      
      
      Attachments: 
      
      http://forums.matronics.com//files/4_ch_vid_cam_mux_rev_a_459.pdf
      
      
________________________________________________________________________________
Date: 
Oct 14, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera
      feed splitter
      
      At 11:28 PM 10/13/2017, you wrote:
      >
      >I know Wade's specific request for camera switching has been solved, 
      >but it sounded like the sort of thing that might come up again so I 
      >thought I'd take a stab at it.
      >
      >So... here's an alternative for switching cameras to a monitor or 
      >EFIS input using a couple of voltage regulators and three ICs.  All 
      >components are through-hole.  Everything on a single PCB, and no relays.
      >
      >Reference the attached schematic:
      >
      >An LM2931 5V linear regulator and a TC7660 charge pump provide +/-5V 
      >rails to power the circuit.  A 555 timer is configured in astable 
      >mode to provide an output with adjustable period of about 3 to 10 
      >seconds.  This output is fed to the clock input of a CD4022B octal 
      >counter.  The clock signal can be interrupted by a SP3T ON-ON-(ON) 
      >switch to stop rotation of the cameras or advance them 
      >manually.  Outputs 1-3 of the counter are connected to the logic 
      >inputs of an AD8184 4:1 video multiplexer such that they cause the 
      >multiplexer to cycle through its four video inputs, connecting each 
      >in turn to the output.  RCA connectors provide four camera inputs 
      >and one video output.
      >
      >LM2931AZ 5V Linear Regulator: http://preview.tinyurl.com/yakjxubl
      >TC7660CPA Inverting Charge Pump: http://preview.tinyurl.com/y7n7g6um
      >ICM7555IPAZ CMOS Timer: http://preview.tinyurl.com/ybrvnnq2
      >CD4022BE Octal Counter: http://preview.tinyurl.com/ycjsa46w
      >AD8184ANZ 4:1 Video Multiplexer: http://preview.tinyurl.com/ybozz2nf
      >SP3T Toggle Switch: http://preview.tinyurl.com/ybpazcu5
      >
      >Critiques?  Suggestions?
      
         How about replacing the 555 and counter with
         a single uC. Paul Fisher can probably craft
         the software to emulate these two components
         to include the scan, step, rate and hold functions
         in one, 8-pin dip device and about 1/20th the
         hardware.
      
         Do you want to terminate unused outputs with
         dead shorts or 75 ohm resistors? RCA jacks
         are more robust than most miniature headphone
         jacks. Further, they're available to solder directly
         to an ECB. If termination of an unused output is
         necessary, a 75 ohm resistor can be installed
         in an RCA plug.
      
      
         Bob . . . 
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Eric Page" <edpav8r(at)yahoo.com>
Date: 
Oct 14, 2017
      
      
      Eliminating the 16-DIP-packaged counter and most of the passives sounds fine to
      me.  It will certainly shrink the PCB.  If you can give me a pin-out for the
      uC you propose using, Ill amend the schematic.  Ill need to know pin numbers for
      Vcc, Gnd, two outputs to the mux, how well read user input for run/hold and
      rate, and if an ICSP header is needed.  Im guessing you propose the same (PIC12F683?)
      used for the recent prop current limiter...
      
      The AD8184 multiplexer has just one output, so I didnt figure a termination resistor
      was necessary.  The connectors shown actually are RCA jacks, despite the
      CAD symbol looking like a headphone...
      
      http://preview.tinyurl.com/ycpmbhj5
      
      They connect the AD8184 inputs to ground with an internal switch contact if no
      RCA is plugged in.
      
      Eric
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473527#473527
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera feed
      splitter
From: 
"Airdog77" <Airdog77(at)gmail.com>
Date: 
Oct 14, 2017
      
      
      Eric,
      
      As an end user --I'll emphasize that aspect since you & Bob are speaking on a cosmic
      ethereal plane that this mortal struggles to follow [Wink] -- having another
      option is never bad.
      
      I really like the ON-ON-(ON) switch form factor for control.  Simple and small,
      which is exactly what I need in a Long-EZ.  Probably could be incorporated for
      most designs, but I'm glad you made note of it.
      
      Regards,
      Wade
      
      --------
      Airdog
      Wade Parton
      Building Long-EZ 916WP
      www.longezpush.com
      
      
      Read this topic online here:
      
      http://forums.matronics.com/viewtopic.php?p=473536#473536
      
      
________________________________________________________________________________
Subject: 
Re: Constructing an automatic RCA video camera
      feed splitter
From: 
"Paul A. Fisher" <paulf(at)hughes.net>
Date: 
Oct 14, 2017
      
      
      Since my name was mentioned, I'll weigh in. I'll be happy to modify the 
      program Bob mentioned for this function, or more likely, just write a 
      new one using elements of the one Bob mentioned.
      
      If I understand the AD8184 data sheet, we need to feed A0 and A1 one of 
      four states - 00, 01, 10, and 11. That's pretty easy to do with just 
      two pins. If we used the PIC12F683 (mostly because I'm familiar with 
      it!!), we could do this:
      Pin 1 - Vdd
      Pin 2 - High order bit to AD8184 (connect to A1)
      Pin 3 - Low order bit to AD8184 (connect to A0)
      Pin 4 - not used
      Pin 5 - Run/Hold switch (pull low to hold)
      Pin 6 - Step switch (pull low to immediately switch to the next input)
      Pin 7 - Analog voltage (0-5V) to control the speed of switching in Run mode
      Pin 8 - Vss
      
      I think you could use the same switch (on-on-(on)) to ground pin 4 in 
      position 2, and ground pin 6 in the momentary position. Analog voltage 
      on pin 7 is similar to what you have on the proposed schematic.
      
      Is this what we are looking for? I'll let you and Bob decide on the 
      hardware components necessary to make it all work, but the PIC software 
      sounds pretty straight forward.
      
      Paul Fisher
      
      
      On 10/14/2017 8:00 AM, Eric Page wrote:
      >
      > Eliminating the 16-DIP-packaged counter and most of the passives sounds fine
      to me.  It will certainly shrink the PCB.  If you can give me a pin-out for the
      uC you propose using, Ill amend the schematic.  Ill need to know pin numbers
      for Vcc, Gnd, two outputs to the mux, how well read user input for run/hold and
      rate, and if an ICSP header is needed.  Im guessing you propose the same (PIC12F683?)
      used for the recent prop current limiter...
      >
      > The AD8184 multiplexer has just one output, so I didnt figure a termination resistor
      was necessary.  The connectors shown actually are RCA jacks, despite the
      CAD symbol looking like a headphone...
      >
      > http://preview.tinyurl.com/ycpmbhj5
      >
      > They connect the AD8184 inputs to ground with an internal switch contact if no
      RCA is plugged in.
      >
      > Eric
      >
      >
      > Read this topic online here:
      >
      > http://forums.matronics.com/viewtopic.php?p=473527#473527
      >
      >
      
      
________________________________________________________________________________
Date: 
Oct 14, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera
      feed splitter
      
      At 08:00 AM 10/14/2017, you wrote:
      >
      >Eliminating the 16-DIP-packaged counter and most 
      >of the passives sounds fine to me.  It will 
      >certainly shrink the PCB.  If you can give me a 
      >pin-out for the uC you propose using, I=99ll amend the schematic.
      
         See attached
      
      >   I=99ll need to know pin numbers for Vcc, Gnd, 
      > two outputs to the mux, how we=99ll read user 
      > input for run/hold and rate, and if an ICSP 
      > header is needed.  I=99m guessing you propose 
      > the same (PIC12F683?) used for the recent prop current limiter...
      
         Yeah . . . only 'case they're cheap and we got lots
         of them!
      
         Probably wouldn't fuss with ICSP, just put the chip
         in a socket. This lets a user drop a new chip
         into a fielded assembly should any future feature be
         desired/necessary.
      
         The sequencing software could be set up to default to
         either SCAN or STEP at power up. Your choice. If the default
         is STEP, then Channel A input is the first up.
      
         Momentary depression of the switch to STEP would advance
         to next channel in sequence. Momentary depression to SCAN
         would initiate steps through the four inputs at a rate
         commanded by the potentiometer. Setting a rate of
         say 3 to 10 seconds for zero to 5 volts seems a
         good starting point.
      
         I didn't suggest any DO-160 like protections for
         inputs to the command pins. If the switch is
         on the board it's not needed. If off the board,
         extending the lines in a shielded-twisted pair
         would offer plenty good prophylactics for our
         environment.
      
      
      >The AD8184 multiplexer has just one output, so I 
      >didn=99t figure a termination resistor was 
      >necessary.  The connectors shown actually are 
      >RCA jacks, despite the CAD symbol looking like a headphone...
      
         Aha! Been there . . . fiddled with several
         canned libraries for about an hour each
         before I dumped them all and crafted my
         own.
      
      
      >http://preview.tinyurl.com/ycpmbhj5
      >
      >They connect the AD8184 inputs to ground with an 
      >internal switch contact if no RCA is plugged in.
      
         Understand.
      
         I propose we make this another open source program like
         the wig-wag was . . . I'll be pleased to set up a folder
         to host all the work product.
      
      
         Bob . . . 
      
________________________________________________________________________________
Date: 
Oct 14, 2017
From: 
"Robert L. Nuckolls, III" <nuckolls.bob(at)aeroelectric.com>
Subject: 
Re: Constructing an automatic RCA video   camera
      feed splitter
      
      At 01:50 PM 10/14/2017, you wrote:
       
      >
      >Since my name was mentioned, I'll weigh 
      >in.=C2  I'll be happy to modify the program Bob 
      >mentioned for this function, or more likely, 
      >just write a new one using elements of the one Bob mentioned.
      >
      >If I understand the AD8184 data sheet, we need 
      >to feed A0 and A1 one of four states - 00, 01, 
      >10, and 11.=C2  That's pretty easy to do with just 
      >two pins.=C2  If we used the PIC12F683 (mostly 
      >because I'm familiar with it!!), we could do this:
      >Pin 1 - Vdd
      >Pin 2 - High order bit to AD8184 (connect to A1)
      >Pin 3 - Low order bit to AD8184 (connect to A0)
      >Pin 4 - not used
      >Pin 5 - Run/Hold switch (pull low to hold)
      >Pin 6 - Step switch (pull low to immediately switch to the next input)
      >Pin 7 - Analog voltage (0-5V) to control the speed of switching in Run mode
      >Pin 8 - Vss
      >
      >I think you could use the same switch 
      >(on-on-(on)) to ground pin 4 in position 2, and 
      >ground pin 6 in the momentary position.=C2  Analog 
      >voltage on pin 7 is similar to what you have on the proposed schematic.
      >
      >Is this what we are looking for?=C2  I'll let you 
      >and Bob decide on the hardware components 
      >necessary to make it all work, but the PIC 
      >software sounds pretty straight forward.
      >
      >Paul Fisher
      
         Our 'ships' passed in the night. I was going
         to suggest that you take the sketch I posted
         and adjust to what makes sense both from
         a software and layout perspective.
      
      
         Bob . . . 
      
________________________________________________________________________________
From: 
Alec Myers <alec(at)alecmyers.com>
Subject: 
Re: Constructing an automatic RCA video    camera
      feed splitter
Date: 
Oct 14, 2017
      
      Bob
      
      Do you know how much extra work it takes to make a PIC meet DO-160? 
      
      
      > On Oct 14, 2017, at 6:24 PM, Robert L. Nuckolls, III 
       wrote:
      > 
      > At 08:00 AM 10/14/2017, you wrote:
      
      >> 
      >> Eliminating the 16-DIP-packaged counter and most of the passives 
      sounds fine to me.  It will certainly shrink the PCB.  If you can give 
      me a pin-out for the uC you propose using, I=C3=A2=C2=C2=99ll amend 
      the schematic.
      > 
      >   See attached
      > 
      >>   I=C3=A2=C2=C2=99ll need to know pin numbers for Vcc, Gnd, two 
      outputs to the mux, how we=C3=A2=C2=C2=99ll read user input for 
      run/hold and rate, and if an ICSP header is needed.  I=C3=A2=C2=C2=99m 
      guessing you propose the same (PIC12F683?) used for the recent prop 
      current limiter...
      > 
      >   Yeah . . . only 'case they're cheap and we got lots
      >   of them!
      >  
      >   Probably wouldn't fuss with ICSP, just put the chip
      >   in a socket. This lets a user drop a new chip
      >   into a fielded assembly should any future feature be
      >   desired/necessary.
      > 
      >   The sequencing software could be set up to default to
      >   either SCAN or STEP at power up. Your choice. If the default
      >   is STEP, then Channel A input is the first up.
      > 
      >   Momentary depression of the switch to STEP would advance
      >   to next channel in sequence. Momentary depression to SCAN
      >   would initiate steps through the four inputs at a rate
      >   commanded by the potentiometer. Setting a rate of
      >   say 3 to 10 seconds for zero to 5 volts seems a
      >   good starting point.
      > 
      >   I didn't suggest any DO-160 like protections for
      >   inputs to the command pins. If the switch is
      >   on the board it's not needed. If off the board,
      >   extending the lines in a shielded-twisted pair
      >   would offer plenty good prophylactics for our
      >   environment.
      > 
      > 
      >> The AD8184 multiplexer has just one output, so I didn=C3=A2=C2=C2=99
      t figure a termination resistor was necessary.  The connectors shown 
      actually are RCA jacks, despite the CAD symbol looking like a 
      headphone...
      > 
      >   Aha! Been there . . . fiddled with several
      >   canned libraries for about an hour each
      >   before I dumped them all and crafted my
      >   own.
      > 
      > 
      >> http://preview.tinyurl.com/ycpmbhj5 
      <http://preview.tinyurl.com/ycpmbhj5>
      >> 
      >> They connect the AD8184 inputs to ground with an internal switch 
      contact if no RCA is plugged in.
      > 
      >   Understand.
      >   
      >   I propose we make this another open source program like
      >   the wig-wag was . . . I'll be pleased to set up a folder
      >   to host all the work product.
      > 
      >   Bob . . .
      > 
      > 

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October 05, 2017 - October 25, 2017

AeroElectric-Archive.digest.vol-oc

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