Return-Path: Received: from bewersdorff.com ([192.220.83.90] verified) by logan.com (CommuniGate Pro SMTP 4.1.5) with SMTP id 2622282 for flyrotary@lancaironline.net; Fri, 03 Oct 2003 01:18:54 -0400 Received: (qmail 80263 invoked by uid 21338); 3 Oct 2003 05:18:54 -0000 Received: from unknown (HELO rapunzel) ([216.101.149.124]) (envelope-sender ) by 192.220.83.90 (qmail-ldap-1.03) with SMTP for ; 3 Oct 2003 05:18:54 -0000 From: "Marko Bewersdorff" To: "Rotary motors in aircraft" Subject: RE: [FlyRotary] Re: Electric Water Pumps and Heat Rejection Date: Thu, 2 Oct 2003 22:18:30 -0700 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-2" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 Importance: Normal I concur - sorta, I tried to run a little vacuum pump with an electric motor and burnt my finger on that wire I hooked up to it. Not scientifically speaking it used a lot of power pumping nothing (3 inch of quicksilver worth of nothing that is) I think I'm going with the electric gyro btw.. I also tried to run that pump with my big drill press - that vacuum sucker sucked a lot of amps! I was surprised. So since water is thicker than air I could see that a properly sized electric motor with a high efficiency pump got to do more than 1 kW. On the other hand someone ought to tell us how many cm^3 of water flow per second it takes to remove the heat from a 160 HP developing 13B. Maybe a balmy trickle through the engine does the trick anyways. Does anyone recall how much of a trickle from the faucet a test stand engine is using? re Marko > -----Original Message----- > From: Rotary motors in aircraft > [mailto:flyrotary@lancaironline.net]On Behalf Of Ed Anderson > Sent: Thursday, October 02, 2003 4:52 PM > To: Rotary motors in aircraft > Subject: [FlyRotary] Re: Electric Water Pumps and Heat Rejection > > > > From: "Rino" > To: "Rotary motors in aircraft" > Sent: Thursday, October 02, 2003 6:53 PM > Subject: [FlyRotary] Re: Electric Water Pumps and Heat Rejection > > > > Ed Anderson wrote: > > > > That analysis was based on the fact that the Mazda water pump > > > supposedly consumed 13-16 HP at 6000 rpm. > > > > > > Ed Anderson > > > > A half inch V belt will NOT transmit 13-16 HP for very long! I do not > > think that is a realistic value. > > > > Rino > > I presume you are correct, Rino. The Mazda water pump is driven > by two "V" > belts on the older engines which would up the capability a bit. But, the > main point is - how much power does it really take to flow enough > coolant to > keep the rotary engine happy at 6000 rpm rather than how much power might > the pump be consuming. > > I don't know the answer, but I agree 16 HP seems a bit on the > high side. My > point was that if you base analysis on erroneous data or assumptions, then > it would seem to follow that the answer you get is liable to be erroneous > {:>) Hopefully, Todd will get his bird back into the air with an > EWP and we > will have real world data/evidence. > > Ed Anderson > > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html