Mailing List flyrotary@lancaironline.net Message #12635
From: Russell Duffy <13brv3@bellsouth.net>
Subject: RE: [FlyRotary] Re: EWP
Date: Sat, 6 Nov 2004 18:30:56 -0600
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>
Message

Based on Todd’s correction of the earlier unbelievable numbers on current drawer, you can expect somewhere in the neighborhood of 35-40 amps continuous for 25 gpm of flow (which is believable) – if the pump will produce that much flow in a real cooling system.  That’s based on the pump power going roughly as the square of the flow rate.

Hi Al,

In the data, Todd gave the GPM flow rate for several conditions.  It appears there's no way to get close to 25 gpm of flow with the DC EWP.  The good news is that it must not really be necessary, because Todd has flown quite successfully with only one of these pumps, and the Ford evap cores.  

Cheers,
Rusty (hopefully not misquoting Todd anymore)



 I've reposted the flow measurements along with this post with the incorrect current draw deleted. I hope this clears up any confusion about EWP current requirements. I

        I ran the first test with the Ford evap cores in the system, plumbed in parallel.
·        Max flow 9.3 usg/m  35 l/m
·        12.07 volt battery supply voltage
·        

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