X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from ms-smtp-01.southeast.rr.com ([24.25.9.100] verified) by logan.com (CommuniGate Pro SMTP 5.0.9) with ESMTP id 1155605 for flyrotary@lancaironline.net; Thu, 15 Jun 2006 12:02:46 -0400 Received-SPF: pass receiver=logan.com; client-ip=24.25.9.100; envelope-from=eanderson@carolina.rr.com Received: from edward2 (cpe-024-074-111-186.carolina.res.rr.com [24.74.111.186]) by ms-smtp-01.southeast.rr.com (8.13.6/8.13.6) with SMTP id k5FG1fNY015475 for ; Thu, 15 Jun 2006 12:01:43 -0400 (EDT) Message-ID: <002c01c69095$1dfbdcd0$2402a8c0@edward2> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Remove Turbo Date: Thu, 15 Jun 2006 12:02:34 -0400 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="UTF-8"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.2869 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2900.2869 X-Virus-Scanned: Symantec AntiVirus Scan Engine Steve's comments are on the money, Thomas. Yes, you can certainly design a cooling duct system optimized for cooling in a climb. However, as Steve indicated you will then pay with additional drag/weight,etc for each of those many hours at cruise airspeeds. Many (most?) of us try to design for optimum cooling at cruise (minimum drag) and accept the fact that for a few minutes during/after takeoff we may incur a cooling deficient. My limits are 200F oil and 220 Coolant, so long as my full power climbout does not cause either of those limits to be exceeded, I feel comfortable. Now, once I have reach 120 MPH IAS I start to get into the sufficient cooling capacity region and all temps start back down. At cruise my cooling temps are normally around 160-170F for both oil and cooling - which could indicate that I still have a bit too much cooling capacity (and therefore cooling drag). Ideally at cruise, I would like to see oil and coolant at 180-185F. However, since I don't wish to exceed my establish limits in climbout, I accept that I probably have more cooling drag at cruise than I need to have. If I were flying a Bush plane in and out of hills and valleys carrying heavy loads and at relative slow speeds, then I would opt to optimize the cooling system for takeoff and climbout. If I were flying a canard type I would opt to optimize the cooling system for cruise. With an Rv I'm someplace in the middle {:>). Like most of areas when discussing aircraft, cooling is another one of those "compromise things" Ed Ed Anderson Rv-6A N494BW Rotary Powered Matthews, NC eanderson@carolina.rr.com ----- Original Message ----- From: "Steve Brooks" To: "Rotary motors in aircraft" Sent: Thursday, June 15, 2006 9:51 AM Subject: [FlyRotary] Re: Remove Turbo > Thomas, > You could design a cooling system for extended climb, but you would be > adding > significant drag to the aircraft. There is only so much you can do with > cowl > flaps. > > I believe that most builders (and also most certified aircraft) design > cooling > for cruise, and tolerate temperatures climbing somewhat in climb. There > do > have to be tolerable limits, however. > > I'm afraid that if I built my cooling system to maintain temps on an > extended > climb, at full power, on a 95 degree day, I would have much cruise speed > when > I leveled off. > > I've seen several discussion on this group, where people leveled off for a > while, or reduce power and go to a cruise climb, in order to let thing > cool > back down. > > On my aircraft, the oil temperatures are fine, but coolant is marginal on > hot > days. On a 95 degree day, I could only get to about 2000 feet AGL before > my > coolant temperature was at redline. Leveling off and reducing power, > cools > it down, and then I can increase power and continue climbing at a cruise > speed. > > I have some more gains that I can make on mine cooling system by making > improvements in air flow. Currently I have some dead space below the > radiators which I'm sure allows some air to roll back out. I also have a > couple of spots that are allowing air to leak through, which I need to fix > as > well. > > Steve > > On Wednesday 14 June 2006 09:30 pm, Thomas y Reina Jakits wrote: >> "" >> >> > While it doesn't make sense to try to have sufficient cooling for >> > climb, >> > I think that I can still make some air flow improvements and get a >> > little >> > better cooling. >> > >> > Steve "" >> >> Steve, what makes you think/believe that!? >> I always assumed that one would design/plan for the worst case scenario: >> Slow/steep/pro-longed max power climb.... >> >> You always can close the flaps/louvers (streamline/reduce drag) when you >> change into a less severe regime. >> But what good is a 250hp engine if you can't use it for more than 2 >> min.... >> I would at least want a 5 min limit for T/O-power. As Rotaries go, they >> will hold up fine with max power for cruise/racing/etc. fine too - but if >> you can't cool it..... >> >> What if you are in line on really hot day? You might not even get 2 min >> of >> max power. >> I would rather err on the wild side of cooling - you always can cut down >> and close off, once you know your ride... >> >> TJ >> >> >> -- >> Homepage: http://www.flyrotary.com/ >> Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ > > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: http://mail.lancaironline.net/lists/flyrotary/ >