Return-Path: Received: from [65.33.166.167] (account ) by logan.com (CommuniGate Pro WebUser 4.0b9) with HTTP id 1803528 for ; Fri, 11 Oct 2002 18:44:06 -0400 From: "Marvin Kaye" Subject: Re: [FlyRotary] EWP water pump To: flyrotary X-Mailer: CommuniGate Pro Web Mailer v.4.0b9 Date: Fri, 11 Oct 2002 18:44:06 -0400 Message-ID: In-Reply-To: <00a901c27130$ab7781a0$1702a8c0@WorkGroup> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Ed Anderson" : > Well I've now got an EWP from Davies, Craig in Oz. Hi Todd, Great to hear you have taken that on. Leon and I exhanged a few views on the suitability of the electric water pump for aircraft use and I certainly respect Leon's experience and smarts - but, the bottom line is no one (that we know of ) has yet tried one in an aircraft. I will most interested in what you find out. If it works, then it would be nice to get max coolant flow when you need it most (High power takeoff with low air flow through radiators) and then save HP at lean cruise by lowering the flow rate and associated losses. They certainly have been made to work in auto and marine applications. While I must admit to some skepticism as to their suitability for aircraft use, I am always ready to revise my opinion based on some real world data. So good luck and let us know what you find. Best Regards Ed Anderson