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Alternator failure. Info provided
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lhelming(at)sigecom.net
Guest

Posted: Wed Jul 05, 2006 3:50 am Post subject: Alternator failure. Info provided

Bob, if you want a beta tester when you get the system developed, let me 

know.  I could be a good candidate.  I have new IR 60amp  alternator that is 

waiting to be installed if the ER alt. from Vans fails which is controlled 

by a B&C LR3; but I could make the switch sooner.  Larry in Indiana with 

flying RV7



 	  Quote: 	
		   

 <nuckollsr(at)cox.net>

    Don't worry about it. There's a system under development

    that's easy to add on to any existing system that provides

    the any-time/any-conditions absolute control over a

    stock automotive alternator. The risks for not having it

    right now are low. If you want OV protection now, you can

    install the original Z-24 configuration knowing that the

    ultimate solution will use the b-lead contactor and alternator

    control switch. The straight transorb approach hypothesized

    on the last figure of page 4 will not work. We've got

    a plan-E . . . or is it "F" . . . anyhow, the solution

    will not be difficult or expensive.



    See:

 http://www.aeroelectric.com/articles/Alternator_Failures.pdf



    Bob . . .

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nuckollsr(at)cox.net
Guest

Posted: Wed Jul 05, 2006 4:56 pm Post subject: Alternator failure. Info provided

At 06:47 AM 7/5/2006 -0500, you wrote:



 	  Quote: 	
		  

<lhelming(at)sigecom.net>



Bob, if you want a beta tester when you get the system developed, let me 

know.  I could be a good candidate.  I have new IR 60amp  alternator that 

is waiting to be installed if the ER alt. from Vans fails which is 

controlled by a B&C LR3; but I could make the switch sooner.  Larry in 

Indiana with flying RV7


	




   I'll keep it in mind. There will be some beta-systems shipped

   to builders who are willing and able to provide best-practical

   turn-around for proofing installation instructions and product

   performance.



   Thanks for the offer!



   Bob . . .

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