To me, that seems more vertical flex than torsional flex. Not at all discounting your findings, but looking at how small #1 main bearing and all the added leverage from the crank snout with the heavy balancer and tension from the belt is what (in my opinion) is the reason it is breaking behind 1&2.
Here is a quick simulation applying a torque to the end of the crank. Note the stress points. Almost impossible to distinguish bend flex from torque flex failure.
That being said, has anybody broken an internally balanced crank on a duramax?
I really like that people are working on this but the only problem I have with all of it is why bone stock trucks break them and some live over a grand without problems. I honestly hate reading these threads, I am in fear about every time I start my truck now lol
It is interesting to note that a NASCAR style flat ground crank would have a twist variation of only 1.00 when using a firing order of 1-8-3-4-7-2-5-6 and be lighter and internally balanced. Shame they generate second order vibrations that most people would find offensive. Much like a 4 cylinder engine does.
It is hard to tell if it was bending or torsional stresses that cause the cranks to snap without looking at the actual failure point itself. Thanks to somebody whose images I poached (it was a while ago so I forgot whose they are...) we have a perfect example that is even well lit by a flash to highlight the beach marks.
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The cumulative stresses on the crank are not enough to induce fatigue failure in of themselves.
The location of the failure initiation is always off center and always in the same direction. As I illustrated with the last FEA for torque, the stress concentration for an applied torque and from bending are in the same place. You can NOT distinguish between them
Since the cumulative loads are not enough, the question is where is the extra force coming from? The only mechanism I can come up with is harmonics. Even one undampened force in tune with the cranks torsional harmonic will build to the point of failure.
In your FEA you are correct that you cannot distinguish between the two modes of loading. However, you can distinguish between metal fatigue due to torsion versus bending by analyzing the surface of the failure. The pictures people are posting are all indicating a brittle fracture resulting from cyclic bending.
Go back and look at the actual forces on the rod journal. THEN explain to me how it is being twisted.
Without changing the order, I think a properly designed dampener would reap great benefits too.
I highly doubt the water pump had anything to do with the failure. They probably did not re install the dampener with the proper torque. After all they are tighter than two frozen squirrel nuts.Not knowing much about dampener design other than some are counter weighted for proper balance and there are several different dampening materials utilized (fluid, rubber, dynamic shot, etc), what "design" change would you make?
While I don't think the balancer is 100% at fault, there were many threads over the years where guys changed their water pumps (with balancer removal/reinstall), or switched balancers and soon after experienced crank failure. While not a 1 for 1 cause and effect scenario, it was something that always had me wondering (and glad I'm still on original water pump). It leads me to "think" some property of it plays a roll in crank failure (just not smart enough to figure out what it is).
Never once did I say it is being twisted. Bending? Yes. Torsion? No.
Need some experimental work done to capture the crank in flex. Should be able to log the signals from the torque converter sensor and the crank sensor to see if their alignment varies. This would not only show crank twist, but could also help determine if there is a base harmonic within the operating range of the engine if the twist changes with RPM.
OK, EDP, don't keep us hangin, how much for a cam with a stock grind?
This makes me second guess my cam I just bought now... Damnet!!