X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from proton.sasknet.sk.ca ([142.165.20.178] verified) by logan.com (CommuniGate Pro SMTP 5.4c2) with ESMTPS id 4922970 for flyrotary@lancaironline.net; Fri, 25 Mar 2011 22:37:49 -0400 Received-SPF: none receiver=logan.com; client-ip=142.165.20.178; envelope-from=hjjohnson@sasktel.net Received: from pps.filterd (proton [127.0.0.1]) by proton.sasknet.sk.ca (8.14.3/8.14.3) with SMTP id p2Q2SbkC028998 for ; Fri, 25 Mar 2011 20:37:13 -0600 Received: from bgmpomr1.sasknet.sk.ca (bgmpOMR1.sasknet.sk.ca [142.165.72.22]) by proton.sasknet.sk.ca with ESMTP id v95tgu0xr-1 for ; Fri, 25 Mar 2011 20:37:13 -0600 Received: from sasktel.net ([192.168.234.97]) by bgmpomr1.sasknet.sk.ca (SaskTel eMessaging Service) with ESMTP id <0LIN001IZ8M1TPA0@bgmpomr1.sasknet.sk.ca> for flyrotary@lancaironline.net; Fri, 25 Mar 2011 20:37:13 -0600 (CST) Received: from [192.168.234.25] (Forwarded-For: [216.197.211.104]) by cgmail1.sasknet.sk.ca (mshttpd); Fri, 25 Mar 2011 20:37:13 -0600 Date: Fri, 25 Mar 2011 20:37:13 -0600 From: H & J Johnson Subject: Re: [FlyRotary] Re: intersting video To: Rotary motors in aircraft Message-id: <51f300c4d07d.4d8cfcf9@sasktel.net> MIME-version: 1.0 X-Mailer: Sun Java(tm) System Messenger Express 6.1 HotFix 0.20 (built Feb 27 2006) Content-type: multipart/mixed; boundary="Boundary_(ID_/V2oqVv9VTvg+lqNM5zrog)" Content-language: en X-Accept-Language: en Priority: normal X-Proofpoint-Virus-Version: vendor=fsecure engine=2.50.10432:5.2.15,1.0.148,0.0.0000 definitions=2011-03-25_10:2011-03-25,2011-03-25,1970-01-01 signatures=0 X-Proofpoint-Spam-Details: rule=outbound_notspam policy=default score=0 spamscore=0 ipscore=0 suspectscore=0 phishscore=0 bulkscore=0 adultscore=0 classifier=spam adjust=0 reason=mlx engine=5.0.0-1012030000 definitions=main-1103250185 This is a multi-part message in MIME format. --Boundary_(ID_/V2oqVv9VTvg+lqNM5zrog) Content-type: text/plain; charset=us-ascii Content-transfer-encoding: 7BIT Content-disposition: inline Greg, I can't remember if I've asked this in the past, so forgive me if I have. How is the air from the boundry layer divider [diverter?] going to get out around the plumbing conduites [running back from the firewall]? From this last front shot, it looks like the 'conduites' are sorta 'fencing' in the air the would normally get diverted out the sides. I'm sure I'm missing something [just the angle of the shot] but thought I'd ask. She's going to be a speed demon!! Jarrett Johnson > One more shot with gear doors shut. > Greg > > ----- Original Message ----- > From: "Thomas Giddings" > To: "Rotary motors in aircraft" > Sent: Friday, March 25, 2011 4:54 AM > Subject: [FlyRotary] Re: intersting video > > > Greg: I also thought about the P51 style scoop. I do think it is a > great > idea. I have a landing gear that retracts into the fuselage and > there really > is not much room for a belly scoop. Could you post some Pics of > how you did > this. How Big is the Radiator and scoop and where did you place > the oil > cooler. By the way if any of you are at Sun N Fun next week . > Please stop by > and say Hi. I will be in Building A booth 67 all week. I plan on > getting out > and looking at some flying examples if possible. and maybe see > some of you > folks then. > > Tom Giddings > > On Mar 25, 2011, at 12:43 AM, Greg Ward wrote: > > > Hey Tom; > > We looked at this scenario when we were laying out our Legacy, > and > > determined that it was packing too much into a cowling that > already had a > > large intercooler, and a turbo that was guaranteed to be > radiating about > > 1400 to 1900 degrees of heat. So, the question was, where to > put a > > radiator, oil cooler, etc. outside of the cowling? We settled > on a P-51 > > scoop for both, and built it exactly like the original, hoping > for a > > little thrust return. Difference was, we kept the radiator out > of the > > fuselage, because we didn't want a leak in the cockpit at 20+K > feet, with > > all that entails. We are also looking at installing a hot water > heating > > system, with valves both in and out for the very same reasons. > So, what > > we have left is, the engine, intercooler, turbo, and whatever > goes on the > > firewall, with a lot of air going through, to hopefully keep > everything > > happy. The flaps on the scoop should enable us to keep temps > under > > control, a' la P-51, so we'll see. > > > > Greg Ward > > Lancair Legacy N178RG, Still in progress > > > > > > ----- Original Message ----- From: "Thomas Giddings" > > > > To: "Rotary motors in aircraft" > > Sent: Thursday, March 24, 2011 8:59 PM > > Subject: [FlyRotary] intersting video > > > > > > Here is a youtube engine test run of an LS1 V8. Watch it long > enough to > > see how the dual radiators are plumbed. This system for engine > cooling > > includes two radiators which appear to be in series. It seems > to be going > > from the thermostat housing to the top of the first radiator > then is taken > > out the bottom of the first one and crosses over to number two > at the top > > inlet and back out the bottom into the pump and back through the > block > > .They are both dual pass radiators . They feed this air from two > outside > > the cowl scoops. Bud Warren claims this cools very well. In fact > he claims > > it is the only way to cool the 300HP LS1 V8's . I wanted to > original > > install a LS3 into my Questair, but could quite get it stuffed > in there . > > http://www.youtube.com/watch?v=CUSbOAZRRtg. If this link does > not work > > search youtube for Franks Bearhawk Test run. Incidently they > claim they > > need 1256 Sq In of radiator surface to keep the V8 running at > 190 in > > cruise and 200 max in the climb. Also if you to geared drives > yahoo forum > > there is a very interesting read on the subject on cooling > requirements > > for the LS1. > > > > Tom Giddings > > VP Avionics Sales > > MIDWEST AVIONICS > > 200 Hardy Roberts Dr > > PO Box 219 > > West Paducah,KY 42086 > > 877-904 9966 > > Cell; 727 858-1772 > > FAX:270 744 3466 > > tom@midwestaviation.net > > Online Store > > www.midwest-avionics.com > > > > > > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: > http://mail.lancaironline.net:81/lists/flyrotary/List.html > --Boundary_(ID_/V2oqVv9VTvg+lqNM5zrog) Content-type: text/plain; charset=iso-8859-1 Content-transfer-encoding: 7BIT Content-disposition: inline -- Homepage: http://www.flyrotary.com/ Archive and UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html --Boundary_(ID_/V2oqVv9VTvg+lqNM5zrog)--