Midget/Fordboy,
Just to satisfy my curiosity I finally assembled some information and comparisons of the through-bolt loadings and stresses. This is on the attached pdf, along with a copy of the ARP stud drawing, in case you don’t already have it.
From the results, it seems there are some conclusions to be drawn.
The 90 x 90 degree make-up rotation spec is most likely bogus.
The Rover upgrade to 10.9 material and 180 x 135 degree rotation makes sense, since that puts it right in the region of the yield strength of the material--not that some yielding is unacceptable. Clearly, the previous 9.8 spec material probably was, as is roundly noted in various places, loaded into its yield range.
The made-up bolt load appears to be plenty to contain the gas pressures--didn’t bother to estimate bottom end loading.
The ARP 50 lb-ft torque puts it right in alignment with the other schemes as far as generated load. Plus, the higher strength of the stud material can probably accommodate the thermal loading while still staying under its yield point. This would be a good thing in that it would retain most of its preload and springiness. Some preload may be lost due to gasket compression, but at least not more from the bolting.
IO - I was over at Mark's last night, and we discussed your numbers.
Above everything else, we were stunned that anybody's curiosity other than our own would have led anybody else down the path of the calculations you went through in order to produce this information, and we're
very grateful for it.
It also led us into the old conversation regarding engineering to a price/cost point, and how often in engines like the K, an overriding idea by a bullheaded engineer can sway a project into unnecessary headaches and disappointments.
An unnamed manufacturer's attempt to build a 90 degree V-6 diesel was recounted to me, but I digress.
If you watch this video from Rover and read between the lines, I can easily see where corporate inertia, combined with commitment to concept and the associated egos involved, coupled with Rover's precarious financial position at the time could easily have led to the problems the initial iteration of the K went through.
3:15 shows the machinery Rover developed to mass produce the design.
https://www.youtube.com/watch?v=Os3b6hVOrFg Here's the first part of this 2 part video -
https://www.youtube.com/watch?v=4tb-ucz_FpgWhile I think the
idea of the expansion of the block with respect to the bolts being utilized producing the final setting of the clamp load and yield is brilliant, it just seems to me that the degree of consistency
of so many components - 10 bolts, the head, head gasket, the cylinder case, the girdle, the oil ladder - would need to be held to a much higher standard than Rover was able to carry out.
So yes, I'll be ordering the ARP kit.
IO, thanks again.
I think we owe you a drink.
