Using stock Mazda coolant “O”
rings and exceeding those temperatures would indeed compromise the “O”
rings and you end up with coolant in your combustion chamber and/or combustion
gases in your coolant galleys – I know - as it happened to me as well as
others when first sorting out my installation back over 10 years ago.
However, once we found and substituted
TES (Teflon Encapsulate Silicon) coolant “O” rings with a
much higher temperature rating, and Viton seals for the oil ring seals, it
became quickly apparent that a lot of the problem with elevated temperatures had
been the “O” rings and somewhat higher temperatures could now
be sustained without any apparent damage or problems. Not to say, higher
temperatures are recommended, but many of us have found brief excursions above
200F do not cause any detectable problems.
My normal cruise coolant and oil temps are
within 5F of each other and normally range from 160F to 185F at cruise
depending on power levels and OAT. So as a percentage of operating time,
my temperature excursions are on the order of 1.6% of my total engine operating
time. On a hot 90+ day, I will exceed 200F during climbout until I hit
120 MPH IAS – usually a brief period of from 2-3 minutes before airflow
catches up with heat being produced.
Numerous rotary installations now fly with
red lines above what would have been prudent if using the older stock
Mazda “O” rings. I have over 8 years on my installation with
TES “O” rings, Tracy Crook over 15 years the vast majority of it
with the TES “O” rings. So until we get some aircraft
with over 2000 hours on an engine (and set of TES O rings), we really won’t
know whether these brief excursions are resulting in accumulated ill effects or
not. If it takes 2000 + hour to manifest itself – then I am not
concerned.
There is no question that the rotary can
not, for the reasons mentioned by several, with stand the temperature ranges of
most piston engines – however, we are not quite as bound by earlier
limits (at least for limited time periods) as we once were. Thanks to
sturdier seals.
We had 8 rotary powered aircraft at the
Texas Rotary Round up and it would be interesting to know how many have
exceeded 200F and any heat associated problems. Although most have less
than 500 hours, so not a true indication of what to expect one way or the other
Time changes, technology advances and
improvements are found.
Ed