Mailing List flyrotary@lancaironline.net Message #12622
From: <kenpowell@comcast.net>
Subject: [FlyRotary] EWP
Date: Sat, 06 Nov 2004 16:24:35 +0000
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Good question Bulent.  This is a show stopper for me.  It takes a minimum of 13 amps to drive the fuel injection and ignition system.  I agree that 1 hour endurance is a reasonable assumption; I am using 45 minutes to allow for greater than expected battery degredation (I wiill replace the battery yearly).  I agree that the EWP will shorten this endurance considerably.  Dual alternators would minimize this risk.  Unfortunately 2 alternators just will not fit under the cowl of my RV-4.  I am considering a snowmobile/motorcycle type PM alternator but I am a LONG ways from addressing this feature.  So I will add to Bulent's question - what will be the current draw at  25 gallons per minute when installed in a functioning cooling system? 
 
Ken Powell
 
-------------- Original message --------------

> Did anybody figure out by how much the engine run time will be shortened
> after an alternator failure. Now we know the engine will run approx. 1 hour
> before it quits. The electric water pump will shorten this time a lot I
> think.
> Bulent
>
>
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