>Tightness at T.D.C. is a good thing for ABC & AAC engines.
>The newer engines ABC & AAC are built with a taper in the
>sleeve. The smallest dia being at the top of the stroke.
>This is where it is needed most for a good compression seal.
>The newer motors such as the PA's and the Ro Jetts etc.
>require more break in time and they are built to last. If
>you break in an AAC properly you will find even after a year
>of full use the motor will still be tight when cold. Another
>advantage is should you have a lean run the sleeve will
>expand accordingly to the temperature, thus returning to
>normal when cooled down. The motor is not ruined as in the
>days of the old Mc Coys etc. Motors like the the OS have
>much less taper and probably more clearance between the
>piston and the sleeve, they are easier to break in. They are
>made this way on purpose so they are more user friendly to
>the beginner or the modeling public and he can get in the
>air faster. This does not mean they are bad motors, just a
>different type. Many OS's have been broken in in the air.
>This is not a wise decision when dealing with the AAC or the
>ABC. It is best to break them in on the stand first so when
>you put your first flight in it will be a good one. When
>first breaking in a AAC motor it will run a little erratic
>until the piston and the sleeve develope a good seal. It's
>best to follow the manufactures instructions to the letter.
Ron B.
F4Fguy
Gregg:
Not to nitpick but,well,to nitpick,the real answer is in the piston/sleeve materials,and the fact that they have different thermal expansion coefficients.The taper is chosen so that,at temperature,the bore and piston diameter and resulting fit is a straight line,or nearly so.This usually results in an interference fit at TDC on a cold engine.
The fits and tapers required are different for different sleeve materials(Al,brass,or bronze),and different silicon/aluminum alloy pistons but,the bore plating material has little or no effect on the thermal expansion.The piston always runs hotter than the sleeve.Al/Si alloys have significantly lower thermal expansion coefficients than other alloys.This is why the Al/Si alloy is used for the piston,so the piston can be fitted closer and still not over-expand the bore.The big issue on break-in is to bring the fits to those best suited to the operating condition.
Unlike the older iron/iron engines,AAC,AAN,ABC,or ABN should be broken in at as near as possible to the expected running condition.This,generally,means a lot of short runs at or near the in- air condition,with complete cool-down between runs. Avoid overheating as this will accelerate wear,but also avoid running at too light a load as the wear pattern will be altered by an undesirable thermal profile.Actually short tanking and flying with a size smaller prop is an excellent break-in procedure.
Most high quality iron bore/iron piston engines have some taper so that the bore is straight at operating temp.This extends even to full size aircraft recips,some having as much as .020" of "choke"at the top.