sorry have to play devils advocate there are hudge displacement 4 cylinders out there. there are also big displacement 4 cylinders out there normaly they have slower RPMs and compression ignition engines. refering to cargoships and earthmovers. im in agreance with okland ang nliii
Refer to my previous post:
Nliiitend1 said:
...should I even BEGIN to explain why that is an utterly retarded idea for car engines??
Young Roids said:
I don't agree with your logic at all. Lets look at truck engines, the biggest truck engines use inline 6 cylinders. Not four cylinders but they have single cylinder sizes of above 1.25 litres. They do not rev as high as car engines but that is because of the extra long stroke and higher compression they use due to being diesel.
...AND BECAUSE THEY HAVE A LOT OF MASS IN THE RECIPROCATING AND ROTATING ASSEMBLIES. They also have a "delay-time" (the fixed amount of time that it takes to ignite the incoming fuel when it hits the superheated/supercompressed air) that limits peak power to a lower RPM range, so it'd be less useful to have high engine speeds. This is actually why diesels usually have large pistons and or/are turbocharged. Also, the higher compression ratio is not the reason that a diesel engine does not rev as high. In fact, running a higher compression ratio allows
higher engine speeds because the exhaust valves can be opened earlier (something needed for high engine speed) in the power stroke (since the engine starts making power earlier in the power stroke because of the high compression). Diesel engines would have EVEN SLOWER engine speeds if they had lower compression ratios (which of course wouldn't really work since the compression in a diesel engine is what brings about combustion). Of course, if you actually took the time to read and comprehend my last post, you'd know I'm not talking about diesels, so all of this is really moot:
Nliiitend1 said:
Which brings me to my next point: Detonation becomes a major problem in a spark-ignition engine as cylinder size gets too big, as the "burn" of the fuel takes on less predictable characteristics due to large area that it now must occupy in a short burst of time. This can lead to decreases in fuel economy, acceleration of wear-related engine damage, and overheating.
Obviously, I'm not even bringing diesels into the debate. Are you saying you want a 5 liter 4-cylinder
diesel engine in your car?? Cause they could definitely make that work, though it would be a whole lot less fun to drive than any car with a 5 liter V8 spark-ignition engine...
Young Roids said:
I don't know if the burn area being "unpredictable is a problem on bigger cylinders but I highly doubt it. And if it really is a problem then up the boost pressure and the air will be more atomised for an even burn.
(hand)
You sir, are an idiot. It IS a problem. Efficiency on a SPARK-IGNITION engine goes WAAAAAAY down, and the propensity to detonate before the spark goes way up when you make the cylinders too big. It's fact. You can't just "up the boost pressure" to solve the problem, because that in effect makes the detonation problem WORSE. Diesel engines get away with large cylinder sizes because they don't have to worry about pre-ignition/detonation. They can "up the boost," as you say, because you can run virtually unlimited boost on a diesel engine since you don't have to worry about pre-ignition/detonation...it's the nature of the beast. Also, when you approach piston diameters over 5-6 inches the additional fuel you'd have to inject to make use of the extra room to make more power wouldn't burn fast enough to burn completely (especially at higher engine speeds), further reducing the fuel economy.
Now please, continue to show us all how little you really know about this subject...
(yupnope)
dkswim said:
6.04 lieter oposed 4 cylinder big enough.... runs on gas 5.319 in bore, thats huge.
Lycoming IO-390
wow im taking this farther off topic.
OK. That is an AIRPLANE engine, which is an entirely different animal. It's designed to spend most of its running time at cruise speed (65%-75% of full power), with only short-lived dips into the higher power bands (during take-off and climbing). It also makes peak power at 2700 RPM, and probably only revs to 3-4K rpm...
Also, if you read up on that engine, they've gone to great lengths to minimize the drawbacks of running a large cylinder-size gasoline engine (and at a price of ~$30K, I'd hope so):
The current configuration includes a robust rotating system closely derived from the TIO-360-C1A6D, specifically developed cylinders, tuned induction system, Lycoming's roller tappets, Slick Start ignition and front facing fuel injection.