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piston seals |
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| Jan7-13, 12:32 PM | #18 |
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piston seals
intent was not to talk down as this is not productive to anyone..least of all me...but blanket statements about no active piston coolling can not stand without comment. You are correct about the fact that all rings are pressuriezed and I was not clear not 100% correct in my previous statements.
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| Jan8-13, 02:40 PM | #19 |
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then again, if piston heats up more and expands more, wouldn't it create enough contact stress? you might argue that it would need precise clearances, but wouldn't you need that for seals as well? that is what my doubt keeps coming back to. whatever function the seals are serving, could be performed by the piston. no? also, someone please tell me at what stage of ic engine development did seals come into the picture. how did engines operate before seals? |
| Jan8-13, 03:13 PM | #20 |
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| Jan9-13, 02:27 AM | #21 |
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Thanks Q, lets see now..if I remember correctly Mr. Otto and I used technology that was currently available ...we borrows the piston ring technology used on steam engines. The pressure of an internal combustion engine is significantly greater and we had to modify the rings to use the combustion pressure to properly seal the combination.. see Stanley steamer 735 engine piston rings attached..( hey..I'm old but not that old..people!)
one more point.. Sprint cars must be push started as the builders eliminate the starter and clutch assembly to get the lightest combination. Consequently the engine spews fuel and oil for the first couple of laps until the engine heats to operating temperature..every race night these cars are out on the track means a super slick asphalt track..I hate it..can you imagine what would happen if we made a piston with no rings and relied on the heat to expand the piston to close the clearances..What a mess..EPA sure would be all over us like Ugly on an Ape! |
| Feb25-13, 07:27 PM | #22 |
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In aircraft engines, the cylinder walls are either chrome plated, nitrided, or plain steel. Because of this the piston rings are different materials as well. As for the end gap, they're staggered in even portions (i.e. 4 rings at 90 degrees each, 3 at 120, etc.) This is done so that you don't have leakage from the combustion chamber into the crankcase, which creates a loss of power, and mucks up your oil faster. The rings on the piston are a little bit spring-like, so they press against the cylinder wall. The top rings seal the combustion chamber and the ring at the very bottom ring it the oil control/scraper ring which keeps and excessive amount of oil from entering the combustion chamber (keeps just enough on the walls for lubrication) so you don't get fouled plugs.
The majority of this has been said, but I just wanted to throw in from an aircraft engine point of view, even though the basics of the Otto-cycle engine are the same. |
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