Oil temps
We are flying as of July 2. The engine is a IO360-A1B6 200hp.
This is what the first configuration looked like
I had 3" scat tubing from #4 cyl to the Niagara 20006A 13 row cooler that Vans sells. Note the exit plenum and ducting. The thought was to direct the flow to the exit and perhaps create a bit of venturi effect.
Note this is a nose dragger with all of the tubes obstructing the cowl exit. I do have a bit of rounding at the corner of the firewall.
First flight. cyl head temps ~350 oil temp 235 and climbing before I started backing off.
The baffling (PITA!) seemed to be well sealed. The first thing I did was remove the exit plenum. Aboslutely no change to either the oil or cyl temps.
I next removed the vernatherm. It appeared to expand as advertised. I measured the standard lycoming body, and it appeared to be about .030 deeper than it was supposed to be. Dan H has a bunch of info on vernatherms elsewhere. I fabricated a .032 crush washer instead of the .063 crushwasher. It made a distinct improvement, but would still climb up around 235 with high power (trying to seat new rings) and keep going up until power was reduced. Oat was in the 25 - 30C range.
airspeed seemed to have little effect.
I replaced the 3" hose from the baffle to the cooler with 4" scat. Again an improvement, but still the temps inched up and up under high power.
I did note that #1 and #3 cht were maybe 30 degrees higher than 2 and 4.
I had installed the baffling with the plates in front of #1 and #2 at full height. I trimmed the #1 plate off about 3/4". Problem solved! oil temp now may get up to 220 on a long max power run, but it is very stable with no inclination to keep climbing. It looks like the path under the inlet ramps really gets squeezed down and not a very smooth flow with that plate at full height.