- Joined
- Dec 3, 1999
- Messages
- 9,437
Thanks Rick, that is my theoretical understanding of it.... but in application it just seems like a blade that has gone through the brutality of forging, and then goes directly to a hardening cycle (and from a very high austenizing heat) is going to crack all over the place. I know FOR SURE it will when you let it cool to ambient room temp, and then drive a diamond penetrating point into it on a Rockwell tester.
nb11b- You are absolutely correct about the geometry affecting things. My reason for starting off with test "coupons" or "tiles" is that there's less work involved in developing the initial sample pieces, and they are easy to surface grind and then Rockwell test across the entire piece.
For steels like 52100, 5160, O1, etc. a piece will typically harden pretty darn evenly thoughout, but with steels like W1, W2, and 1095, you can get a test piece that's 66/67C on the edges, and 45C in the center (which is of course why we like those for creating blades with hamon
).
I have done quite a bit of tests already, but it's going to take me some time to lay it out here.
My very initial tests were done with a bar of 1084 that I cycled through the forge (1800-1950F) 5 times but did zero forging on, along with some test pieces cut from the parent bar in the as milled condition. I did different normalizing cycles in the Paragon, in the salt, different temps, different rates of cooling, and then austenized in the kiln and in the salt.
A quick note on the results, at this point I'm not seeing much of a difference between the two heat sources other than the kiln causing scale to form and giving just a bit of variation in the Rc tests.
I am very pleasantly surprised to see with 52100, the descending thermal cycles with a quench have given me steel with working conditions that seem very comparable to 52100 that has gone through an overnight spheroidal annealing cycle.
nb11b- You are absolutely correct about the geometry affecting things. My reason for starting off with test "coupons" or "tiles" is that there's less work involved in developing the initial sample pieces, and they are easy to surface grind and then Rockwell test across the entire piece.
For steels like 52100, 5160, O1, etc. a piece will typically harden pretty darn evenly thoughout, but with steels like W1, W2, and 1095, you can get a test piece that's 66/67C on the edges, and 45C in the center (which is of course why we like those for creating blades with hamon
I have done quite a bit of tests already, but it's going to take me some time to lay it out here.
My very initial tests were done with a bar of 1084 that I cycled through the forge (1800-1950F) 5 times but did zero forging on, along with some test pieces cut from the parent bar in the as milled condition. I did different normalizing cycles in the Paragon, in the salt, different temps, different rates of cooling, and then austenized in the kiln and in the salt.
A quick note on the results, at this point I'm not seeing much of a difference between the two heat sources other than the kiln causing scale to form and giving just a bit of variation in the Rc tests.
I am very pleasantly surprised to see with 52100, the descending thermal cycles with a quench have given me steel with working conditions that seem very comparable to 52100 that has gone through an overnight spheroidal annealing cycle.