Return-Path: Received: from envelope.rose-hulman.edu ([137.112.8.21] verified) by logan.com (CommuniGate Pro SMTP 4.2.8) with ESMTP-TLS id 611218 for flyrotary@lancaironline.net; Tue, 18 Jan 2005 02:06:10 -0500 Received-SPF: none receiver=logan.com; client-ip=137.112.8.21; envelope-from=madsena@rose-hulman.edu Received: from bob (dhcp024-160-204-151.ma.rr.com [24.160.204.151]) (authenticated (0 bits)) by envelope.rose-hulman.edu (8.11.6/8.11.6) with ESMTP id j0I75RX03669 (using TLSv1/SSLv3 with cipher RC4-MD5 (128 bits) verified NO) for ; Tue, 18 Jan 2005 02:05:36 -0500 (EST) Message-Id: <200501180705.j0I75RX03669@envelope.rose-hulman.edu> From: "Alex Madsen" To: "'Rotary motors in aircraft'" Subject: RE: [FlyRotary] Re: Switching to Evans NPG+ Date: Tue, 18 Jan 2005 02:05:18 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Mailer: Microsoft Office Outlook, Build 11.0.5510 Thread-Index: AcT9EZgFLbmnDlaYQvmka9EapiD09AAELiDg In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2180 I have to disagree with you comments about pressure being needed to keep coolant in contact with an engine's surfaces. All that matters is that the ABSOLUTE pressure of the coolant does not exceed the vapor pressure of the coolant. Yes, it is VERY important to consider all operating environments of the fluid (0 to 15,000 feet+) it would be a foolish mistake to do otherwise. However, it is important to remember that any system in our atmosphere has pressure on it (atmospheric pressure). For any coolant system we have the pressure of the atmosphere + the (optional) pressure of the coolant system. This gives us the absolute pressure keeping the coolant in contact with the engine. The only way the coolant will lose contact with the engine is if the vapor pressure of the coolant exceeds the absolute pressure of the cooling system (vapor pressure is temperature dependant variable). When that happens coolant vaporizes (boils) and allows the liquid coolant to separate form the surface being cooled. So yes a coolant system must have some absolute pressure. However it irrelevant if this pressure is above, at, or possibly below atmospheric pressure as long as the vapor pressure of the cooling liquid is exceeded. What someone needs to do is determine the max coolant temp in an engine (remember the local coolant temp inside the engine may exceed the exit coolant temp by several degrees). Now call up Evans and see what the vapor pressure of NPG+ is at that temp. If the vapor pressure exceeds the atmosphere pressure of you max altitude (+ a safety factor) then you do not have to worry about vaporizing coolant. The reverse is also possible find out what you min atmospheric pressure is and see what coolant temperature it corresponds to. Alex Madsen Mechanical Engineering SR Rose-Human Institute of Technology PS I think it would be easy to figure out what changes need to be made to a cooling system in terms of fluid flow and pipe diameter to convert from H20 to NPG+. If someone will provide some data I can dig out my Heat Transfer Text and crunch the numbers. -----Original Message----- From: Rotary motors in aircraft [mailto:flyrotary@lancaironline.net] On Behalf Of Marvin Kaye Sent: Monday, January 17, 2005 10:56 PM To: Rotary motors in aircraft Subject: [FlyRotary] Re: Switching to Evans NPG+ Try and remember that the rules for what happens inside an engine at sea level are different than what goes on at 15,000 feet. While the NPG+ may not boil until 396*F at sea level, I'm certain that it's a different beast at altitude. The guy who engineered the Eagle was livid when we told him that Evans recommended a pressureless system... part of the reason for the pressure is to keep the coolant pressed firmly against the metal surfaces it's trying to cool. Even if you have a high boiling point, when the metal temperatures exceed it the boiling will happen and without the pressure to insure coolant contact, pretty soon everything is surrounded by a cloud of PG steam (well, maybe not a "cloud", but all the hotspots will be working overtime keeping the coolant boiling next to them). Those metal temps quickly build, the areas where the coolant has turned to vapor grow, and the problem feeds on itself until the system goes completely out of control. At this point your pressureless system vents itself, throwing out what's left of the coolant and the engine is toast. The point here is that there are more reasons for having a pressurized system in an airplane than meets the eye. One more thing... with a pressurized system you can alarm it for a low pressure situation. If something goes wrong with the coolant system (like you spring a leak) the pressure will likely go down before you see a rise in temps. If the system is setup to run at 20psi and you alarm it at 15, when you see that master warning you know that pretty soon you're probably going to overheat. Just another chance to get a jump on things that you pass up without pressure. >> Homepage: http://www.flyrotary.com/ >> Archive: http://lancaironline.net/lists/flyrotary/List.html