Mailing List flyrotary@lancaironline.net Message #11197
From: Mark Steitle <msteitle@mail.utexas.edu>
Subject: Re: [FlyRotary] Photos of Core tanks internals
Date: Tue, 07 Sep 2004 12:06:19 -0500
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Ed,
What is amazing to me is that there are only three small holes in each cross-tube.  Its hard to believe that these small holes will pass enough coolant to cool a 13B @ WOT. 

Mark S.


At 12:38 PM 9/7/2004 -0400, you wrote:
Well, David,  I just went down to the shop through the pouring remnants of
Frances and cut open each side tank of a core I had taken from the junkyard
years ago.

The photos are attached and speak for themselves - no dividers or other
impediments to coolant flow in the tanks - pretty clean channel from top to
bottom.  Each "row" has 5 approx 1/8" (perhaps slightly larger) dia holes
that conduct the water through the core to the opposite side tank.  So 14
rows * 5 * area of 1/8-3/16" dia hole would give a cross flow channel area
of around 0.86 sq inches to 1.93 sq inches - probably toward the larger
figure.

So as Bill suggested they may have redesigned the heat exchangers to take a
different approach to recondensing the refrigerant calling for the divider
plate.  Given the relatively small cross channels, it is my opinion that a
serpentine cooler is probably offering considerably more resistance to flow.
Some of the radiator shop webpages give an estimate of the increase in flow
resistance of a Serpentine core over the straight through - as best I recall
it was something like 4 times as best I recall.

So, its clear that not all GM evaporator cores are created the same way.
This one was from the an late 80s early 90s Cadillac.  I looked all over for
some identifying model number but could not find anything.  I do recall it
had a yellow sticker with a black C on it when I yanked it.

In any case, it looks like we can not simply order just any GM cooler core.
I suspect that when they switched over to the more environmental friendly
refrigerant then  there could have been some redesign of the core, but just
speculation on my part.

Here's the photos

Ed.


Ed Anderson
RV-6A N494BW Rotary Powered
Matthews, NC
----- Original Message -----
From: "David Carter" <dcarter@datarecall.net>
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Sent: Tuesday, September 07, 2004 11:55 AM
Subject: [FlyRotary] Re: Water pump problem


> Thanks, Ed.
>
> I wonder Steve Brooks's core with a "plate" is different from the
> GM/Harrison cores that I have (Chev'y Caprice).
>     - When I probed my core last night and found no plates in the end cap
> with the larger of the two welded tubes, I DIDN'T check the other side -
> those smaller 1/2" OD tubes turn 90 degrees and run about a foot, so I
never
> probed that side.  That is the side that has the little "filter" and/or
> "expansion jet" thing sitting about an inch down inside.  Perhaps there's
a
> plate on that side that matches what has been discussed recently.
>
> If Steve's core is a typical GM/Harrison core, then I'd like to understand
> more about which end "the plate" is in and tell us more about "the tube
that
> was removed".  I've not yet cut into any of my cores to mod the fittings,
so
> am ignorant of the insides.
>
> David
>
> ----- Original Message -----
> From: "Ed Anderson" <eanderson@carolina.rr.com>
> To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
> Sent: Tuesday, September 07, 2004 6:54 AM
> Subject: [FlyRotary] Re: Water pump problem
>
>
> > Hey, David, not to worry.  We have all hit the "Send" button on an e
mail
> or
> > two and later wondered why we did. {:>)
> >
> > Ed
> >
> > Ed Anderson
> > RV-6A N494BW Rotary Powered
> > Matthews, NC
>
>
>
> >>  Homepage:  http://www.flyrotary.com/
> >>  Archive:   http://lancaironline.net/lists/flyrotary/List.html
>



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