Mailing List flyrotary@lancaironline.net Message #18942
From: Bartrim, Todd <Steve.Bartrim@canfor.com>
Subject: RE: [FlyRotary] Re: Electric water pump
Date: Thu, 17 Mar 2005 10:22:12 -0800
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Message
    Yeah, I thought Tracy and yourself were using the smaller hoses with the pretty AN fittings, and there is no doubt that Tracy at least has been successful (and I'm sure you'll be right behind him :-), but I still stand by my theory that if the automakers use no less than 1.25" hoses, then why would should we when we have a higher heat rejection requirement.
    Now maybe we can get away with less, but then the argument that the EWP can't possibly have enough flow because of our higher heat output is invalid. Maybe we can get away with smaller hoses, or maybe we can get away with an EWP, but can we get away with smaller hoses AND an EWP???
    Because I knew that many were watching closely as mine was the first known aircraft use of an EWP (some hoping for success and many expecting failure), I decided that 1.25" hoses were mandatory. I'd originally started my installation with 1" hose, but changed my mind on this before I was even completed that part of the installation.
 
Todd

 
If I'm not mistaken, Tracy is using 3/4" hoses???  I've been using AN12 hoses, with two evap cores in series, and there has never been a question of cooling the water on the RV-3, even in severe climb tests.  The antique mechanical pump does have a lot of muscle, and might be making up for it though, and I still haven't found a way to test the EWP by itself in flight.
 
  
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