My understanding is that the piston skirt is there to retain and distribute lub. oil, not to remove any excess. (Well, its primary job is to steady the piston at TDC and BDC, and oil distribution is a secondary task).
Here I would normally defer to your previous career and expertise as an engine designer; but for a few other interests of my own, particularly "classic" petrol-driven internal combustion engines in single-, v-twin, and parallel-twin configurations...and the two-wheeled chassis wrapped around them
For decades one of the tuning techniques for four-stroke (four-cycle for American readers) engines was to sharpen the edge of the piston skirt to allow it to "clean" the bore more - less "oil drag" on components in high-revving motors; it was the oil
control ring that retained and distributed oil in that part of the cylinder
ABOVE the gudgeon pin (wrist pin
)...especially if there were oil feed holes IN the piston, just below the control ring's groove; and especially so as the oil control ring would be an inch or two....or three!..."above" the line of the piston skirt. In other words - the piston skirt edge could only scrape the oil off that portion of the bore
that the piston skirt actually travelled up and down - ABOVE that part of the piston's stroke, the oil control ring was responsible for that task, retaining/distributing oil on the
upper cylinder walls...
Therefore, the more spartan oil regime in-cylinder required new piston rings that wore better and distributed oil more effectively themselves.
Exactly! Given that the portion of the upper cylinder where the compression rings...bore...would need lubrication too...and THIS was above the travel of the oil control ring
The oil control ring would control the lubrication THERE
where the compression rings travelled....
not the piston skirt.
Although I do also fully agree with your comments last night regarding the
rocking of the piston due to increased piston skirt clearance probbably causing high wear too - especially if the earlier rings were rectangular-edged...
Hence the
greatly accelerated wear over earlier K5s -
SEVERAL factors simultaneously contributing to accelerated ring wear?
If the new HD30 lub. oil spec. was less viscous, this might have added to the problem of retaining oil in-cylinder.
Yes, this came to me a while back when I first read up on the HD30 issue! Unfortunately I haven't come across any comparisons yet...surely there MUST have been
some done and discussed in and around the period of the Paul Pryon Agreement, the agreement by which the British agreed to take on U.S.-
equivalent oil grades to greatly simplify the logistic chain!
But there must have been some
great difference if Austin's "technical people" could say their engines would run on their old specified oil grade - but
NOT on HD30!
As to the standardisation of the wading spec., I wonder if they looked at where they were going in NWE, and realised there was going to be a lot of water about, i.e. the ports of Calais, Dunkirk, Antwerp, the latter with the operations around the Scheldt and Walcheren, and then there's the Dutch lowlands, which the Germans could flood, then the Rhine that needed crossing, then the north German lowlands, which WERE flooded etc.
That's one for Rich perhaps - to what extent was THIS direction of travel obvious to OVERLORD planners
BEFORE the events of the summer of 1944? My take was more that the first wave of operations would be
to the south and south-east, to secure the Breton Peninsula and allow the USAAF to establish airfields there within a couple of weeks at most - not the couple of
months as per OTL? But that was for the
Americans - where had the
British been
planning on heading?
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