Mailing List flyrotary@lancaironline.net Message #47919
From: Mike Wills <rv-4mike@cox.net>
Subject: Re: [FlyRotary] Re: FW: More Charging Circuit Info
Date: Mon, 31 Aug 2009 20:48:23 -0700
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Al,
 
 That wasnt from me, that was from the weblink Kelly sent. I simply quoted it. I dont know if it is true or false, but I do know that at least one of my previous cars opened the alternator field any time the starter was engaged. It is my understanding that this is typical of car ignition switches though I dont know if its necessary or just a holdover.
 
 My approach is to leave the field de-energized during cranking, energize it after the engine starts, and then energize the non-essential equipment bus. My RV is a very simple day VFR airplane so even when everything is turned on the electrical load is pretty low.
 
 I couldnt be much happier with the cooling. 95 is about as hot as it ever gets here. Oil temp did not limit my climb performance - I chose to level at 5000 to avoid conflicts with airliner traffic. At some point I will investigate the cowl flap option but first just want to get in some flight time and figure out how to consistently land this thing well.
 
The DNA muffler arrived today. Looks like its actually going to be a pretty easy swap with my existing muffler so i may get it installed before the next flight.
 
Mike Wills
RV-4 N144MW
----- Original Message -----
From: Al Gietzen
Sent: Monday, August 31, 2009 12:18 PM
Subject: [FlyRotary] Re: FW: More Charging Circuit Info

From Mike   - …..ensure that the field is de-energized while cranking the engine.

 

And I will respectfully disagree with that – at least until somebody can prove me wrong.  The output current is a function of rpm as well as what the voltage regulator is demanding.  From what I can find, I conclude that alternators typically won’t put out their rated current until they get spinning about 1500 – 2000 rpm, or more (which is usually about double engine rpm). So there is no risk of damaging the rectifier diodes at cranking speed.

 

I’m going to guess that it is a worse shock to the electronics if the field is suddenly turned on at higher rpm when the regulator is on full demand – although I don’t think it’s an issue.

 

 Off topic, another 1.2 hours closer to completing my Phase 1. This was the first flight that after I landed I didnt have anything on my list to fix before the next flight. 95 degrees OAT at takeoff today and the oil temp got to 200 at the top of the climb to 5000' but backed off to 192 after I leveled. H2O temp never above 180. Starting to gain some confidence in it.

Contrary to our friend George’s faint praiseJ, I’d say your temps are excellent.  If it does that well at OAT of 95 F; then your next thing will be to think about adjustable cowl flap to reduce cooling drag at cruise on a cooler day.

Al

Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster