Seeing that it is mil-spec, is made from the right materials (8620/Carpenter 158), is heat treated, shot peened, and MPI tested, I have no issues with. BCGs are going for over $300 on GB, and you don't know if they are new or used, or who the manufacturer is in most cases. I could care less about the coating, it is in stock and is priced right for me. I will lube it as I would any other BCG. BTW - this morning Shade told me he had 500 in stock. Mine ships tomorrow.
Those guys on M4 are A-holes ("I only use Colt or BCM"). If I had only used GM blocks in one of my engines, I would be picking up pieces.
http://www.m4carbine.net/archive/index.php/t-106680.htmlOk, so in English, will QPQ reduce the impact toughness of a bolt and lead to a shorter round count life or not?
Alloys that create nitrides are typically contain aluminum, chromium, molybdenum and titanium. With this in mind, nitriding works better on metals that contain these metals, but not in excessive amounts as these metals can create very hard and very brittle (especially in the case of aluminum) nitrides that break easily and cause cracks to form. So the real question is at which amounts *will* these nitride creating metals create a situation where the surface loses its impact toughness? There were a lot of "mays" and "mights" in the above post, i'm looking for verifiable data please.
Same question for barrels and barrel extensions.
Also, does not the addition of the nitriding process lower the coefficient of friction between the materials, thusly reducing the stresses between parts? And since hydrogen isn't part of the nitriding process, nor is surface etching, how does your final statment factor into the equation?
In English, you are looking at a very complex system and then asking questions about metallurgy and fatigue analysis. The answer is statistical and dependent upon the bolt alloy, geometry, surface treatment conditions and loading cycles amongst many others. If you want a brief answer I would not use this type of treatment on an AR bolt and you should note that none of the competitors in the recent competitions for the military submitted this. The current TDP precludes the use of CN for bolts specifically for a reason.
I will answer this out of order. You are looking for verifiable data, for a very case specific application. This can only be achieved by an extended series of testing and given the fact that the life is governed by first stage fatigue in a low cycle environment it is not a viable proposition to accelerate the tests. The only recourse is to real time testing to collect the data. In English you need to shoot a minimum of 32 rifles to failure using a certified batch of ammunition. Ideally many more. Your verifiable data costs considerable money. Unless the party concerned is conducting an academic exercise or writing a research paper the existence of the data is of no help as you will have no ability to either access it or duplicate the result.
You have half answered you own question in that you have researched and found that the nitrogen free radicals can work adversely with certain elements. As to the percentages of elements present that will be detrimental to a metal this will depend upon the loading and the geometry as well as the chemistry. Potential micro surface cracks in a 25lb retaining piece that is 8" thick are of little consequence, as an illustration, but such initiation points in a bolt would be detrimental. Bolts are typically, what is generally referred to as surface hardening alloys, in that the carbon content is lower and they are usually used in an application where the surface will be hardened. But they are also higher alloys so in this instance they are not clearly classified.
Barrels, good ones, are CMV through hardening alloys, draw your own conclusions! Dropping the alloy specification can allow a barrel to be effectively CN treated. The manufacturer must determine this. Stainless steel is out and the ability of the nitrogen to combine with the chromium will frequently leave the resulting part more susceptible to corrosion that the virgin part.
Barrel extensions are good if run in isolation. They are a very suitable alloy but must be taken in the as machined form. CN over the existing case hardening is a variable proposition.
To address friction between components, again the information that you are using is case specific example. In this case the tribological results from a controlled standard test. The information should be regarded as indicative of properties that can be achieved. If you can definitively quantify that a CN treated bolt/barrel extension will impose less bending stress on the lugs than a classical case hardened combination, when there is substantial contamination from combustion gasses and also lubricant, either as applied or burnt, then you have the perfect answer.
The comments wrt hydrogen and surface etching were general information and correctly are not pertinent to the direct discussion of CN on alloys. They were related to the consideration of surface treatments by other methods and how problems may occur.
I hope that you realize that I am not being evasive in trying to provide answers it is just that a simple yes or no does not exist. I also hope that you do not think that I am being detrimental to the use of CN. Many parts benefit from this finish but like NiB, Chrome, Nickel and Ionbond it is not a universal fix all. The gun industry has the tendency to "find" a process/lube/finish and then finding a single good application, pounce upon it without any further examination and use it for everything they can throw into the vat. This said I am examining CN QPQ for barrels in one instance and I think that bolt carriers may be another great application. I like NiB for through hardened parts and use both chrome and Ionbond in my products.