Subject: [FlyRotary] Re: Cooling oil
----- Original Message -----
From: "Joseph Berki"
<joseph.berki@grc.nasa.gov>
To: "Rotary motors in aircraft"
<flyrotary@lancaironline.net>
Sent: Thursday, June 10, 2004 12:39
PM
Subject: [FlyRotary] Re: Cooling oil
> It would be interesting to measure flow in both
engines. I thought that
> both Lycoming and Mazda engines rejected 2/3 heat
load through the
> oil that is why I started going down this
road. If the engines generated
> the same Hp than the heat load should be
similar.
>
> Joe Berki
Joe, both engines may generate the same heat load, but
the proportion
rejected through the coolant in case of the Mazda is
2/3 of its waste heat
while the oil rejects another 1/3 of the waste
heat. Neither engine rejects
anywhere near 2/3 of its waste heat through the
oil.
Most aircraft engines reject on the order of 300-600
BTU/Min through the
oil, the Mazda at 160HP rejects approx 2446 BTU/Min
through the oil.
Ed Anderson
Ed;
That number looked
a bit high to me, so I went in to my file to check. My data shows 28% of
the fuel burn energy in the rotary gets converted to HP, 18% goes to the
coolant, and about 7% to the oil. Most of the rest goes out the exhaust pipe.
For 160 HP output, I think that should be 1725 BTU/Min going to the oil
cooler. So about 3 times the comparable powered Lyc.
Double check me on
this.
Al