Return-Path: Received: from fed1rmmtao11.cox.net ([68.230.241.28] verified) by logan.com (CommuniGate Pro SMTP 4.2.8) with ESMTP id 610773 for flyrotary@lancaironline.net; Mon, 17 Jan 2005 18:17:13 -0500 Received-SPF: none receiver=logan.com; client-ip=68.230.241.28; envelope-from=daveleonard@cox.net Received: from davidandanne ([68.111.224.107]) by fed1rmmtao11.cox.net (InterMail vM.6.01.04.00 201-2131-117-20041022) with SMTP id <20050117231641.DVQK28808.fed1rmmtao11.cox.net@davidandanne> for ; Mon, 17 Jan 2005 18:16:41 -0500 From: "DaveLeonard" To: "Rotary motors in aircraft" Subject: RE: [FlyRotary] Re: Switching to Evans NPG+ Date: Mon, 17 Jan 2005 15:18:45 -0800 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" 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) Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 Thanks Marv, that is a good data point. I'm sure it is true that if the coolant is 250, the coolant o-rings in the rotary will be quite a bit hotter than that.... I have more or less committed to giving it a try. At this point I am trying to decide upon a safe redline... Pineapple racing (rotary) uses 250-260. After hearing your story I might start at 240 and see how things go... Dave Leonard > HI dave, > > Just a data point for you to consider.... > > I've been working on this Eagle540 V8 powered Lancair IVP for the > last several > years. When we received the engine we installed it, put coolant > in it (50/50 > anti-freeze/water) and started to run it in order to work the > bugs out of the > instrumentation. During a call to the engineer who designed the > motor he went > apoplectic when he heard that we were running 50/50 coolant/water > in there, as > the engine has a magnesium intake manifold and may well suffer > from corrosion > from the water. We drained it and replaced it with Evans NPG+. This was > about a year or so ago. At that time the folks at Evans also > suggested to Ted > (owner of this Lancair) that since this coolant was so superior and has > hundreds of proponents running it in their race cars and other > vehicles, that > 250*F coolant temps are just fine. > > Fast forward to now..... > > One time during the most recent testing phase, when we were > working our way up > to full power, Ted let the coolant temp (on the hot side, coming > out of the > engine to the thermostat housing and on to the radiator) rise to abou 240 > degrees. I saw a couple puffs of black smoke from one of the > exhausts, Ted > saw a cloud of something fly over the top of the cockpit, and so > shut down. > We had coolant on the outside of the engine, at the front on the > gearbox, > about 4 feet away from the coolant overflow bottle. It looked > like we sprung > a leak between the intake manifold and the head on the right side of the > engine. I pulled the mamifold, found a kinked o-ring, replaced > it, put things > back together and tried again. More coolant outside... bummer. > Tried dealing > with the manifold once again and during the next test discovered > that the leak > was coming from the right head gasket. Replaced it and went back to > testing... new leak from the left head gasket, or more likely > just another one > that we didn't see when the right leak happened. When Ted got it > up to 240 he > managed to blow both head gaskets. That's not the worst of it... > the internal > metal temps of the engine had to be considerably higher than the > 240* we were > seeing on the coolant, as when we pulled the left head we found cylinder > scoring, and perhaps even evidence of a couple broken rings in > there... the > engine is being removed from the aircraft and being sent to the local > pro-stock engine builder for a complete bottom end tear down, > inspection, and > replacement of damaged parts... rebalance, etc, etc...... > > The moral of the story is that the folks at Evans might know > everything there > is to know about the chemistry of their product but they don't > know everything > about the metallurgy of every engine their product might be used > in. While I > understand the argument that there's only a relatively small difference > between 200* and 240*, the heat load that the metal parts are > seeing can be > far greater. Other components may suffer as well. Before you go > merrily on > your way, convinced that 250* is ok for your rotary you might want to ask > yourself this question: If that's the case, how come everybody > sets their > redline at 210 or thereabouts? We already know that water has a higher > specific heat carrying capacity than other checmicals, so why is > it ok to pump > more heat into something that doesn't work as well as water? > > Don't get me wrong, you might be perfectly ok setting your > redline with NPG+ > at 250. Then again, you might not, and wind up going down the > same road we > are with this monster V8. Personally, I'd rather see you make the > water/anti-freeze system work... higher temps could well take certain > components right over the edge, and who needs that aggravation? > > >