AeroElectric-List Digest Archive

Sat 12/04/04


Total Messages Posted: 9



Today's Message Index:
----------------------
 
     1. 05:46 AM - Re: Toggle Switch Knob (Mark Sletten)
     2. 06:58 AM - Re: Alternator Off During Start Up? (Gary Casey)
     3. 07:34 AM - Re: Toggle Switch Knob (D Fritz)
     4. 09:39 AM - Re: Toggle Switch Knob  (Eric M. Jones)
     5. 10:34 AM - koroseal cable lacing (thomas a. sargent)
     6. 01:12 PM - larnin' 'lectrics (Fergus Kyle)
     7. 08:06 PM - E-Bus Usage Procedure / Question (Matthew Brandes)
     8. 08:21 PM - Re: E-Bus Usage Procedure / Question (Dan Checkoway)
     9. 08:37 PM - Re: E-Bus Usage Procedure / Question (plaurence@the-beach.net)
 
 
 


Message 1


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    Time: 05:46:26 AM PST US
    From: "Mark Sletten" <marknlisa@hometel.com>
    Subject: Re: Toggle Switch Knob
    --> AeroElectric-List message posted by: "Mark Sletten" <marknlisa@hometel.com> Why don't you just carve one out of wood? I carved a flap lever out of aluminum using a grinder, but the round shape of the wheel might be easier with wood. Mark & Lisa Sletten Legacy FG N828LM http://web.hometel.com/~legacyfgkit


    Message 2


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    Time: 06:58:03 AM PST US
    From: "Gary Casey" <glcasey@adelphia.net>
    Subject: Re: Alternator Off During Start Up?
    --> AeroElectric-List message posted by: "Gary Casey" <glcasey@adelphia.net> <<Automobiles live with a thing called "load dump" or "load dump transient," where if something shuts off or a wire breaks, the alternator output voltage will jump way up momentarily. I forget if they design to 40 or 70 volts, and somewhere in the car or an accessory is a huge zener to limit overvoltage beyond that.>> I think when push comes to shove I believe the average car will have a slightly "quieter" electrical system than a plane. Since weight is not an issue they have a much larger battery and larger-gage ground wires, both of which tend to keep voltage transients down. Although, since we supply electronic components to the auto industry we are constantly being surprised with weird glitches that - of course - are all our fault. The "load dump" phenomena is caused by the inductance of the field in the alternator - imagine the alternator cranking out full current to supply a load and then that load is suddenly removed. The voltage regulator senses the increasing system voltage and shuts off the field. However, the field, being created by a large coil of wire surrounding an iron core, can't be instantly changed, so the alternator continues to produce now-excess current until the field current decays, which takes 10's of milliseconds. The effect is usually very slight as the battery serves to hold the voltage at a near-constant level, absorbing the momentary excess current. The load dump that causes big problems is when there is an open circuit at the battery and in this case there is nothing that will absorb the current that was being taken by the battery, whereupon the system voltage can rise to over 100 volts. Automotive systems are designed to survive this type of voltage transient even though it is quite rare. No, there is nothing in an automotive system specifically designed to ABSORB that transient - everything is designed to TOLERATE it. No "huge zener." <<I have a high compression 540 and long starter leads. Several times I've had difficulty starting the engine with the alt. field on. When I turn the field off it seems to crank faster and starts easily. Is the alt putting a lot of drag on the engine when the voltage drops on cranking?>> The alternator is putting negligible torque on the engine during cranking, but it does draw a few amps (less than 5 as I recall). Would this make the difference? I've found that the usual "observation" is that the starter has trouble torquing the engine over the first compression stroke so the driver tries a couple of times (then shuts off the alternator?). By that time the compression pressure has leaked down sufficiently so that it will go past the first compression and the rest are easy as there is some momentum built up by then. And by the way, in passenger cars the alternator is "on" during cranking. Most of the accessories are turned off during cranking to reduce battery load, NOT to protect them against any mythical voltage transients. Incidentally, according to the wiring diagram my Cessna was originally equipped with a relay in the avionics bus that shut it off during cranking - long since removed. Gary Casey


    Message 3


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    Time: 07:34:51 AM PST US
    DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; b=gCIEa2h9GAe6HZudWzy8xT/u0J83z9Q6unllZkJiOTjKadhlcCI9V/BDGtXhoGLO77znPBDxl7fFdiSCTyPxxc3enXIMOxIyS01omd7ORqFBAcPVNumwQ2oWL0+mwXLzrxin1pbikyzK4OeWIKdRTS44jv8WOr7342MqHPFcUWA= ;
    From: D Fritz <dfritzj@yahoo.com>
    Subject: Re: Toggle Switch Knob
    --> AeroElectric-List message posted by: D Fritz <dfritzj@yahoo.com> I'd be interested in getting one of these as well. Also, while we're discussing switch ergonomics, does anyone know of a source of T-shaped landing light switches? All the commercial and military aircraft I've flown have these shaped so you can tell it's for the landing lights without looking. Dan Fritz ---------------------------------


    Message 4


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    Time: 09:39:06 AM PST US
    From: "Eric M. Jones" <emjones@charter.net>
    Subject: Re: Toggle Switch Knob
    --> AeroElectric-List message posted by: "Eric M. Jones" <emjones@charter.net> Eaton makes a ton of the stuff. If Marine Air Supply 800-678-6085 doesn't have the switch tips I would be surprised. http://www.marineairsupply.com/ Regards, Eric M. Jones www.PerihelionDesign.com 113 Brentwood Drive Southbridge MA 01550-2705 Phone (508) 764-2072 Email: emjones@charter.net "Life may have no meaning. Or even worse, it may have a meaning of which I disapprove." -- Ashleigh Brilliant


    Message 5


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    Time: 10:34:55 AM PST US
    From: "thomas a. sargent" <sarg314@comcast.net>
    Subject: koroseal cable lacing
    --> AeroElectric-List message posted by: "thomas a. sargent" <sarg314@comcast.net> I just got some koroseal. I'm familiar with ordinary nylon cable lacing. Koroseal is a lot thicker and stiffer. Is it used in exactly the same way as the thin lacing (which looks to be difficult), or is there some better practice to follow? -- Tom Sargent RV-6A, firewall.


    Message 6


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    Time: 01:12:21 PM PST US
    From: "Fergus Kyle" <VE3LVO@rac.ca>
    Subject: larnin' 'lectrics
    --> AeroElectric-List message posted by: "Fergus Kyle" <VE3LVO@rac.ca> Matthew, I saw your email on AeroElectric list and note that you are new to this form of the art............ May I recommend the AeroElectrics Connection book produced by Bob Nuckolls, who frequents and replies to this list? Far from shooting you, he and several others, including Brian Lloyd and many others have extensive experience in this and radio fields. However, I suggest that as a minimum step, you buy Bob's book above and become familiar with the particular chapters of interest. It is excellent, and in spite of 40 years of Amateur Radio (and 55 years in flying), have learned much from Bob and others. Your familiarity with the details will qualify you for serious answers we all need to complete our favourite projects. Good hunting! Ferg Europa A064


    Message 7


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    Time: 08:06:36 PM PST US
    From: "Matthew Brandes" <matthew@n523rv.com>
    Subject: E-Bus Usage Procedure / Question
    --> AeroElectric-List message posted by: "Matthew Brandes" <matthew@n523rv.com> I think I'm getting closer to understanding all this electrical stuff.. but I have a question about the E-bus procedure. (Ref. Dwg 11) So your toodling along and your alternator craps out. No big deal... you've planned for it. The alternator is taken offline and you are ready to switch over to your E-Bus. So you flip the e-bus switch, so the e-bus is now drawing current from the battery side of the contactor. The diode is keeping current from flowing back to the Main bus, HOWEVER, if the battery contactor circuit is still closed (BAT switch On), the main bus would still be drawing current through the contactor, yes? So with this design, if the alternator craps out and you want to switch over to the e-bus, you need to put the master switch in the off position, opening the battery contactor cicuit, keeping the main bus from drawing current. Did that make sense? Am I missing something? Procedure: Turn on the E-Bus then turn off the Master Switch. Matthew RV-9A Finish Kit 'lectric newbie


    Message 8


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    Time: 08:21:15 PM PST US
    From: "Dan Checkoway" <dan@rvproject.com>
    Subject: Re: E-Bus Usage Procedure / Question
    --> AeroElectric-List message posted by: "Dan Checkoway" <dan@rvproject.com> Matthew, Yes, you got it...but...I always fly with my E-Bus switch ON. Constantly. That way it's just one switch flip if and when the alternator dies, and voltage to my "essentials" (some of which need initialization time, such as the GPS) is NOT interrupted. If you fly with the E-Bus switch ON all the time, when the alternator dies, flip the master switch all the way off and keep flying. Plus, this way, the devices on the E-Bus theoretically don't see the voltage drop they otherwise would if the E-Bus was being fed through the diode. The E-Bus is being fed from the battery bus (I think!). Hope this makes sense, and please correct me if I'm wrong. )_( Dan RV-7 N714D http://www.rvproject.com ----- Original Message ----- From: "Matthew Brandes" <matthew@n523rv.com> Subject: AeroElectric-List: E-Bus Usage Procedure / Question > --> AeroElectric-List message posted by: "Matthew Brandes" <matthew@n523rv.com> > > I think I'm getting closer to understanding all this electrical stuff.. but I have a question about the E-bus procedure. > > (Ref. Dwg 11) So your toodling along and your alternator craps out. No big deal... you've planned for it. The alternator is taken offline and you are ready to switch over to your E-Bus. So you flip the e-bus switch, so the e-bus is now drawing current from the battery side of the contactor. The diode is keeping current from flowing back to the Main bus, HOWEVER, if the battery contactor circuit is still closed (BAT switch On), the main bus would still be drawing current through the contactor, yes? So with this design, if the alternator craps out and you want to switch over to the e-bus, you need to put the master switch in the off position, opening the battery contactor cicuit, keeping the main bus from drawing current. > > Did that make sense? Am I missing something? Procedure: Turn on the E-Bus then turn off the Master Switch. > > Matthew > RV-9A Finish Kit > 'lectric newbie > >


    Message 9


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    Time: 08:37:00 PM PST US
    From: plaurence@the-beach.net
    Subject: Re: E-Bus Usage Procedure / Question
    --> AeroElectric-List message posted by: plaurence@the-beach.net On 4 Dec 2004 at 21:18, Matthew Brandes wrote: > --> AeroElectric-List message posted by: "Matthew Brandes" > <matthew@n523rv.com> > > I think I'm getting closer to understanding all this electrical > stuff.. but I have a question about the E-bus procedure. > > (Ref. Dwg 11) So your toodling along and your alternator craps out. > No big deal... you've planned for it. The alternator is taken offline > and you are ready to switch over to your E-Bus. So you flip the e-bus > switch, so the e-bus is now drawing current from the battery side of > the contactor. The diode is keeping current from flowing back to the > Main bus, HOWEVER, if the battery contactor circuit is still closed > (BAT switch On), the main bus would still be drawing current through > the contactor, yes? Yes So with this design, if the alternator craps out > and you want to switch over to the e-bus, you need to put the master > switch in the off position, opening the battery contactor cicuit, > keeping the main bus from drawing current. Correct > > Did that make sense? Yes Am I missing something? No Procedure: Turn on the > E-Bus then turn off the Master Switch. Correct Peter RV9A wings > > Matthew > RV-9A Finish Kit > 'lectric newbie > > > _




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