I apologize if there is already a thread for this topic, but I didn?t find anything I could use. After a long build (more than 11 years) my RV-6A took to the air in August (flown by my flight adviser). It sat for several weeks until I came back from getting transition training, then I started to fly off my 40 hours. For several reasons, my next few flights were of short duration (half hour to 45 minutes), so I never noticed high oil temps. However, I finally saw the oil temps climb to around 227 degrees, only decreasing as I pulled back the power and lowered the nose.
I am running an overhauled O-320 with a fixed pitch 3-blade Catto prop. Cooling baffles are from Van?s FWF kit. I have several penetrations in them: one 2? SCAT tube to the heat muff, two 1? SCAT tubes for cooling the battery and my one magneto, and a 3? SCAT tube from the back baffle to the oil cooler which is mounted on the firewall (again, using Van?s kit). All that air (plus what was flowing over the cylinders) is being routed to the back of the cowling.
I?m sure oil is being circulated through the cooler, so that leaves airflow as the culprit. It?s my semi-educated theory that all the air being dumped into the back of the cowling is not able to exit the cowl fast enough to allow a negative pressure area and permit proper airflow through the oil cooler. The exhaust pipes fill some of that rectangular opening, and the nose gear structure may block some air.
I have a set of louvers on order from Avery Tools, but have not received them yet. I am hoping they will contribute to a better airflow out of the cowling. Thoughts?
What puzzles me is that my configuration is not much different from those built by others, so why am I having this problem? I know of no way to observe whether sufficient air is flowing, so I really need some ideas here. As it is, I can?t fly the airplane very long until the oil temps reach unacceptably high levels. Lycoming recommends 180-190, with an absolute maximum of 245. My temps might get that high under sustained level flight, and I have no desire to damage my engine.
Thanks in advance for your help. I welcome any and all suggestions.
Jim Bower
RV-6A N143DJ
Flying (sort-of)
St. Louis, MO
I am running an overhauled O-320 with a fixed pitch 3-blade Catto prop. Cooling baffles are from Van?s FWF kit. I have several penetrations in them: one 2? SCAT tube to the heat muff, two 1? SCAT tubes for cooling the battery and my one magneto, and a 3? SCAT tube from the back baffle to the oil cooler which is mounted on the firewall (again, using Van?s kit). All that air (plus what was flowing over the cylinders) is being routed to the back of the cowling.
I?m sure oil is being circulated through the cooler, so that leaves airflow as the culprit. It?s my semi-educated theory that all the air being dumped into the back of the cowling is not able to exit the cowl fast enough to allow a negative pressure area and permit proper airflow through the oil cooler. The exhaust pipes fill some of that rectangular opening, and the nose gear structure may block some air.
I have a set of louvers on order from Avery Tools, but have not received them yet. I am hoping they will contribute to a better airflow out of the cowling. Thoughts?
What puzzles me is that my configuration is not much different from those built by others, so why am I having this problem? I know of no way to observe whether sufficient air is flowing, so I really need some ideas here. As it is, I can?t fly the airplane very long until the oil temps reach unacceptably high levels. Lycoming recommends 180-190, with an absolute maximum of 245. My temps might get that high under sustained level flight, and I have no desire to damage my engine.
Thanks in advance for your help. I welcome any and all suggestions.
Jim Bower
RV-6A N143DJ
Flying (sort-of)
St. Louis, MO