Mailing List flyrotary@lancaironline.net Message #29854
From: William <wschertz@ispwest.com>
Subject: Re: [FlyRotary] Re: Suitability of NPG for Rotary Engine use
Date: Wed, 1 Feb 2006 21:31:06 -0600
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
The other thing that occurred to me in reading Dave's account is that he ran it on the ground, getting stable temperatures. It was only after taking off, climbing to altitude, and then leveling off that he had the temperature excursion and the problem.
 
** speculation/theory**
On the ground, the cooling from the prop blast would be relatively low, therefore the glycol could circulate and warm up. During climb -- engine generating a lot of power, air speed higher than taxi, but still not at max flow of air through the radiators. Now you get to altitude, level off, speed up, increase the flow of air (and resultant cooling) through the radiator, and lower the power setting somewhat.  ??Can you?? get into a situation where the radiator is cooling the glycol so much that it gets viscous and starts slowing down/blocking flow passages?? I don't know, but I had the following observation on a cold morning in December:
 
I was driving my wife's PT-cruiser at steady speed on an interstate with the temperature on the outside measuring -15*F. The temperature gauge in the car would rise to the thermostat set point, hold for a short time, and then drop off. This cycle repeated as long as I was maintaining constant power input. When I would go off the Interstate, going through town at ~30mph, the temperature would stabilize at thermostat setting, solid as a rock. My *hypothesis* of what was going on was:
 
1. At low speeds, the radiator/thermostat combination could assume a steady state condition.
 
2. At highway speeds, the high rate of very cold air flowing through the radiator would supercool the coolant, and when the thermostat opened the cold coolant would cause the engine temperature to drop a few degrees, then the thermostat would close and the temperature would slowly climb back to the thermostat setting. I have watched for this behavior at less extreme conditions, and if there it is not noticable.
 
Bill Schertz
KIS Cruiser # 4045
----- Original Message -----
Sent: Wednesday, February 01, 2006 7:49 PM
Subject: [FlyRotary] Re: Suitability of NPG for Rotary Engine use

Thanks, Bill
 
Just thought it might be useful to some who might be considering it why NPG just might not be well suited to the stock rotary coolant system.
 
Yes, I noticed that the chart did not measure the viscosity of the NPG at the same temps as they did the 50/50 mixture.  Might be a legitimate reason for that but escapes me.  I suspect the viscosity goes much higher at lower temps.  No problem with a running engine, but starting a really cold block might offer some problems as you suggest.  Especially given the small diameters of some of the GM cores channels.  Could be that Dave simply was not getting any significant cooling due to minimal flow.  I recall him saying the temps went up all of a sudden and wonder if the coolant "trapped" in the block might not have reached very high temps before managing to "burst" lose and send the temp sensor soaring.
 
 
Ed
----- Original Message -----
From: William
Sent: Wednesday, February 01, 2006 6:40 PM
Subject: [FlyRotary] Re: Suitability of NPG for Rotary Engine use

Excellent write-up Ed, I would be particularly leery of NPG in a severely cold climate with small channels in the heat exchanger. High viscosity and small channels can lead to high pressure drop -- low flow. This then becomes unstable, if the flow becomes low, the fluid in the radiator can become colder, leading to higher viscosity, lower flow, higher pressure drop, all the while the engine portion can be overheating.
 
Note that the viscosity for NPG+ is >10 times that of 50-50 EG/water at 50*F, a really interesting number would be the viscosity at 0*F (Where Dave was flying). It could be that the pump cannot generate enough pressure drop to force the fluid through the radiator if it gets cold. On plain (room temperature) water, the Mazda pump can generate ~20 psi at zero flow at 5500 rpm.
 
Bill Schertz
KIS Cruiser # 4045
----- Original Message -----
Sent: Wednesday, February 01, 2006 9:31 AM
Subject: [FlyRotary] Suitability of NPG for Rotary Engine use

Things have been a little dull on the list, since Dave reported on his "adventure". 
 
 Also, I recently received a phone call from a rotary enthusiast (not on the list) about the use of Evans NPG (Propylene Glycol) in rotary engines.  I did a bit of research and my conclusion was the rotary engine was not well suited to benefit from the properties of NPG in its stock coolant system configuration.  
 
 That the use of 100% glycol would  require increased coolant flow rates by 10-15% and more coolant pump power would be required (hard to quantify this one but it appears in the range of 15-25% more).  Also the hazard of fire due to a leak on hot exhaust would be increased (this would apply to a 100% mixture of either Ethylene or Propylene glycol).  There are benefits to using NPG, however, in my opinion the effort needed to change  the rotary cooling configuration to safely use it makes the cost effectiveness of the conversion questionable.
 
The apparent success of Evans NPG in reciprocating engines is not in conflict with my assessment about its suitability for the rotary engine.
 
Attached is some supporting (I believe) facts to support this opinion (and that is all it is).
 
Ed
 
Ed Anderson
Rv-6A N494BW Rotary Powered
Matthews, NC
eanderson@carolina.rr.com


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