cessna170bdriver wrote:….
Also, higher octane fuel IS NOT higher energy than lower octane fuel. Higher octane fuel simply allows a higher compression ratio without causing pre-ignition or detonation, and the resulting engine damage. A given engine produces no more power with higher octane fuel than it does with the octane for which it is rated.
I knew immediately when I posted …that particular choice of words was wrong and almost edited it right-away. Yes, I’m completely in agreement as to what octane numbers mean and why. That was just a quick-and-dirty comment which was intended to refer to the higher efficiency of higher compression.
daedaluscan wrote:GAHorn wrote:daedaluscan wrote:Displacement is the volume moved by the piston. Either the volume sucked in through the intake valve (assuming perfect conditions of course), the volume displaced by the piston on the compression stroke, or the volume pushed out through the exhaust valve. Simply bore cross sectional area x stroke (x number of cylinders).
If an original piston sitting at the bottom of an original cylinder…times six…equals 300 cu. inches…. then how can a taller piston which takes up more space inside the cylinder…. also equal 300 cu. Inches.
You are confusing displacement - the volume "displaced" by the piston with the total volume of the cylinder. The volume of the cylinder is displacement plus combustion chamber volume (the volume above the piston at top dead centre). The taller piston will reduce combustion chamber volume but not change the displacement (bore cross section x stroke).
Think of the 0-300 as having six pistons which each displace (move) about 50cu in. on each stroke. It doesnt matter at all what the remaining volume in the cylinders is.
Taller pistons will increase compression ratio (The ratio of (displacement + combustion chamber volume) / (combustion chamber volume)) as the combustion chamber volume is smaller. Higher compression ratio gives more power, as well as more risk of detonation and more load on the bottom end.
….. It’s the definition of displacement which (was) not making sense to me. As I suggested earlier, this confusion was a matter of terminology. Thanks for clarifying it daedaluscan and Miles.
Soo….the better way to have said my first post would have been not to use the word “displacement”…but instead to comment that cylinder VOLUME is reduced if taller pistons are installed.
Yes, I can see that any increase in HP would also increase the load on the lower-end of the engine. But the important parts of that lower end were sufficiently robust to accommodate their identical brothers in the 175 HP GO-300 engine, and the same crankshaft is used in the IO-360 which can be rated up to 210, soooo… it will be interesting if they can boost the HP of the O300. It still brings up the issue of a fixed-pitch prop vs constant speed.
It seems to me that this engine is limited more by it’s prop RPM than by it’s compression ratio, and increasing its’ compression ratio will likely prevent it’s use of mogas for those who like to use it….. while any performance increase of the aircraft which utilize the O300 will likely be poorly documented (like many other mods) and any actual change (personal prediction) will be almost negligible.
When I take out all the junk I carry in my baggage compartment it’s amazing how much better the airplane performs.