§1. Volume constancy and tolerances [00:02]
One thing that was important from before: Poisson's ratio is 0.5 and Delta V is zero as long as you have a solid material. If it's a porous material, Delta V doesn't have to be zero because you can forge out the pores. But generally for deformation processing, solids and liquids are not very compressible, and so Delta V is essentially zero at the types of strains we're talking about — strains that can be 100% or 200% elongation. If we're rolling something or extruding it, we can have huge elongations, and so any change in volume is in fractions of a tenth or a hundredth of a percent. For all intents and purposes Delta V is zero. There may be some voids in the material from the casting and I might close those up, but compared to the types of strains I'm doing in stretching the material, the volume's constant. I'm not worried about the fourth decimal place. That's for the physicist, let them worry about the fourth decimal place. It's not significant.
Do other people have questions? I'd much rather answer questions than give my lecture. I've heard the lectures before, they're boring anyway. Actually they're not that boring the first time, hopefully. But I did want to talk about tolerances. I'd put up this thing on tolerances and now I've handed out a copy. Does anybody know what controls the tolerance down here? If I was talking about a one-inch-long thing and I can get a tolerance of one one-thousandth of an inch, that's one part in 10 to the 4th, right? What controls that? Why can't I get one part in 10 to the 5th as a tolerance in manufacturing? Here's 10 to the minus 3, this is 10 to the minus 4, and polishing, lapping, and honing is getting me down to something like two parts in ten thousand. No one knows what the fundamental limitation is.
Student: [suggests grain size]
Just a guess, grain size. Well, it could be grain size, it's a good guess. And later on we'll talk about orange peel and how large grains don't deform uniformly at the surface and you will get a surface roughness that can be a lot more than that. It's called orange peel because it has the texture of an orange and it's actually about the same depth. Very clever the way the people talk about these things.
§2. Gauge blocks and the temperature limit on precision [02:48]
Anybody know what these are? [Tom produces a set of gauge blocks.] These are Johansson blocks or Weber blocks — gauge blocks that a machinist uses. They're very precise in their dimensions. In fact it comes with a certificate of standards. This is traceable to the National Bureau of Standards, and this one is 3 inches, made out of chromium carbide. You can buy them out of steel, hardened steel, but they tend to rust, and if they rust they no longer have their precision. Typically these are precise to about 50 millionths of an inch. If you're a machinist and you don't use a micrometer — if you're trying to get down to a tenth of a thousandth, you can get down to a thousandth or maybe half a thousandth with micrometers. You actually ring these together. They have polished surfaces, and if you ring them together — this is the experiment for the adhesion class — you can actually get them to support weight. A little bit of oil on the surface, and the oil becomes an adhesive and they will hold together. And if you take my welding course you get to calculate the force of adhesion, depending on the thickness of that joint.
They come with their certificate that tells you they're accurate to, at the worst, a gauge plus or minus three microns. What's three microns? A human hair is 75 microns, so this is one twenty-fifth of a human hair. That's the coarsest one. You can get them plus or minus 1 micron, plus or minus 0.8 microns. That's the laboratory master standard. When you read it, it says 1.0 inch equals exactly 25.4 millimeters. That's actually the definition of how we define the inch based on the metric standard. Calibrated at 68 degrees Fahrenheit, 20 degrees centigrade, and 45% relative humidity. So what's important there? Temperature. It also tells me on the back side of this sheet the coefficient of thermal expansion. For chromium carbide it's 4.7 micro-inch per inch per degree Fahrenheit, 8.5 micro-inch per inch per degree C. For most of the materials you might make gauge blocks out of — steel, stainless steel, tungsten carbide, chromium carbide, or zirconium oxide — the coefficient of thermal expansion is about 10 to the minus 5 per degree C. Steel is 10.3 times 10 to the minus 6, so it's 1.03 times 10 to the minus 5 per degree C. Well, 10 to the minus 5, if I had a 10 degree temperature change, it's no longer that size anymore, that precision. So temperature limits you here. You have to start defining length in terms of at what temperature when you're getting down to making something precise.
These gauge blocks were polished and lapped to be very flat and very smooth, even more so than you see in that graph. But to be down at 50 millionths of an inch you actually have to start talking about temperature. In the ball bearing industry, they will actually measure the balls to 50 millionths of an inch, and you have to go into a room that's air-conditioned, temperature and humidity controlled. They have the super-duper micrometer. You've seen little hand micrometers — the micrometers to measure the balls for very precision ball bearings are the size of a small lathe. They are in a room that is temperature controlled and humidity controlled, because a 2 degree Fahrenheit change in temperature will screw up your measurement. So when we talk about precision in these tolerances — when you get to these types of precision, you're getting down to where other things have an effect. I've seen people make measurements where they say "oh we measure this" and they're getting all this precision in what they're doing, and I say "and at what temperature?" and they say "what do you mean?" Unless they define the temperature of the measurement, when you get to some types of precision some people claim — well, there's a difference between precision and accuracy, but that's another lecture.
§3. The aluminum can and limiting drawing ratio [07:46]
I also mentioned beer cans and Coke cans, and I found this in some of my junk this morning. [Tom produces an aluminum can.] The aluminum can by Alcoa. Inside here I just happen to have Will PET Do to Aluminum Cans What Aluminum Did to Steel, presented by Ferro Catrakis [?] — Dr. Ferro Catrakis. He doesn't put it on his card, but he was Joel Clark's first doctoral student about 1976 or '77, and he works for Charles River Associates, an economics consulting firm. He's a vice president over there. Anyway this is one of Backofen's — Coors cans — actually fairly thick, it's kind of banged up over the years. Typical soda can or beer can. Anybody know how thick the wall is? It's probably around five thousandths of an inch, about one and a half human hairs. They've been using supercomputers to design these, because they have to hold a certain amount of pressure. Coke cans are a little more tricky than beer cans because the pressure in the carbonation in a soda is higher than the carbonation in beer.
Here's a little description of aluminum cans for the lay person. It points out that in order to make the can — and we're going to talk about this later, today's a little bit of a descriptive lecture — if I wanted to make something in the shape of a beer can — [Tom passes a set of Backofen's drawn cups.] this happens to be copper, and these are Backofen's as well, I haven't polished them in the last 30 years, they're actually probably brass — you have to go through a series of steps, because there's something called the limiting drawing ratio. You start out with a sheet and you punch out a cylinder, and then you draw the cylinder into a cup, it's called cupping, and then you redraw, second draw of that cup into this shape, and then you redraw again. Eventually with this they did four draws to get this. What would have happened if I took that great big sheet and tried to draw it in one draw? I would have punched the bottom out, because I have to deform all that surrounding material without having so much force on the end that I shear the end right off. When we get to sheet metal forming, which is sort of the end of my lectures, we'll talk about that.
In that little Alcoa thing when they're making the cans, for the body — the top is very complex because it's got the pull tab and stuff, but the body is a little simpler — they're doing 200 strokes a minute. So that's a little more than three times a second. The stroke is probably about four or five feet. The tooling is probably going at 60 or 70 miles an hour, up and down. They do 200 strokes a minute, three strokes a second, and 14 cups per stroke in this press, because they have a great big wide sheet of aluminum and they're not just punching out one can at a time, they're punching out 14 cups at a time. At three strokes a second, that's 42 cans a second coming off one can line, which is almost two cases — about one and three-quarters cases a second.
My first big consulting job was at a brewery in New York, and they were filling bottles and cans at 20 a second. One of the problems with this industry is you have to build that can line, or the bottle line if you're making glass bottles, right next to the facility that's putting the beer in or the Coca-Cola in. Because you can't transport all that air very far. Typically you can transport it about a couple hundred yards. So typically the can companies will build right next to the bottling companies. You might spend $10 million on can line presses and tooling. It's pretty impressive to see. I saw a full-size can line at Alcan Research once — not an operational can line, but they had a full-size thing, and it was a two-story-high bay about half the size of a football field. Not all of you probably could have fit it into one-fifth the size of a football field, they had other stuff around it, but it's a big piece of equipment. And another interesting thing is the paint line to put the label on. You have to also be painting these things at a couple of cases a second, and that's another trick, but we won't get into that.
So that's more of a review than I should have done. But I prefer to tell stories than most of these other things. [Tom passes a set of progressive draw samples.] I'll pass this around. This is also one of Backofen's things, a whole series of cups. There's the original cup, and this is the final product before they trim the end. It's sort of rectangular with big corners.
I don't think any of you are old enough to know what this is. Carl, have you ever seen one of these? Like a case for a relay? It's actually a case for a tube in a tube TV — before we had lots of transistors, back when I was a child. You look in the back of a TV and you had a bunch of little glowing vacuum tubes, and you'd put them in a little aluminum case to protect them from breakage. Here is a set of draws. They don't make this anymore — actually they probably do, but it's not a big industry like it used to be. Kind of buggy whips, but nonetheless.
§4. Cold heading: from sheared rod to threaded insert [15:00]
Another thing I'll pass around, since we're going to talk about extrusion today — this was one of my first things. I've been collecting these things. I stole Backofen's — when he left them, I appropriated them, no one else wanted them, and I took them. Some people have learned that it's worth collecting these things over the years. It may not be something that you can use right away, but if you collect for 30 years — it's sort of like writing a diary every day. Each daily increment may not be significant, but when you put the whole thing together after 35 years you actually have something of significance.
This was one of the first things I ever collected. I went to Pittsburgh to a firm — I can't even remember the name because it was over 30 years ago — and they were doing what's called cold heading. In this course we'd call it extrusion. Cold heading was developed after World War 2 when they discovered that if you took a piece of steel and phosphated the surface — and I cover this when I do adhesive bonding, because phosphated surfaces are how you prepare surfaces for adhesive bonding — you can take a steel rod and you can shear it. [Tom holds up the cold-heading sample sequence.] This is the sheared piece of a three-eighths inch steel rod. It used to feel soapy. Most of us have fingered this a lot for the last 30 years. This is the first sizing operation where they take that and squeeze it to size it precisely, put a little indent on one end. This is the next operation, where they actually start an internal, a backward extrusion, and they start making a deeper indentation. This is the next one where they go deeper and the thing is now getting taller. This is the next operation where they put a flange on it, a head on it. Then they have another operation — and this is the one I don't want you to lose, I've lost it a couple times over the years, I'm about to lose it again — this is the only piece of waste from this process. This is the hole they punch out of the middle of that flange. So this is what you end up with. These two go together, got a hole in it because they punched out that little ring. Then they knurl the outside, then they thread the inside, and then they plate it. And what is it? It's a machine screw insert with a knurl. If I'm a woodworker and I want to put my thing together with machine screws, I can use this insert and drill a hole in the wood, slam this in, the flange keeps it from pulling through, and now I can put my machine screw in and I have a good strong joint in a piece of wood furniture.
But to make this simple little part, which you might buy for 20 cents at a hardware store, you have to go through quite a few forming operations. Right after World War II they developed the phosphating technology to hold the stearate lubricant. Anybody know the other name for stearate? Soap. That's why it feels soapy. If we do a lecture here on lubrication, we'll go through that. If you just try to do oil all those extrusion operations, you have so much sliding against the workpiece, the oil would be gone. You have to have some peanut butter that has sticking power through long stretching of that. They're popping those things out at about 10 a second, maybe 20 a second. You walk through this plant — they don't give you earplugs, they give you the things that cover your ears, because the decibel level in that plant is probably above the threshold of pain, with the machinery pounding away at that speed.
They don't just make little parts like that. I've been through a plant in Detroit where they make most of the steering components for the car. If you look down where the wheel is and you see the steering knuckles — they can weigh 10 pounds on a truck, but on a car they might weigh a pound or two — they're made by cold forming. The ones on a truck at 10 pounds might be done by warm forming, all this deformation and forging at 500 or 600 degrees Fahrenheit, not 1,000 degrees. Usually they can do it at 500 degrees. It's called cold heading because it's the same process that people used for centuries to put heads on nails. But we can now make more complex things than heads on nails, and we can make them very fast. The tooling is kind of pricey, but it's very efficient. You can get very precise tolerances. But you better know how to make your dies. You're going to use the steel initially in a soft condition, but by the time it's finished it's gone way out on that stress-strain curve. You might have annealed it so it's soft; by the time you finished hopefully you haven't gone out to get fracture. You've done multiple operations to get more and more stretch. One operation might bring you to here, the next operation you're on a new stress-strain curve that takes you out to here, the next one a new stress-strain curve out to here, and you do this five or six times, and your total strain is a couple hundred percent rather than the limitation of 30 or 40% that you have in a simple uniaxial test. So that's the principle of multiple forming operations, and it applies to sheet metal too.
§5. Radiator tubes, Attleboro gold, and surface roughness [21:01]
Unfortunately these are getting a little rusty. [Tom produces a progressive die sample.] This is something I probably consulted on 25 years ago in Detroit. I think the guy was an MIT alum. The parts they were making were radiators. In order to make the tubes, they made everything from sheet metal, and they would stamp out — what we see here is a progressive die. A piece of sheet that goes through a progressive die.
Most of the stuff I've seen in progressive dies — if you go down to Attleboro, the jewelry capital of the world — I used to consult for a company that went through seven tons of gold a year. They had three or four continuous casting machines for gold, and they make the gold sheet stock, which I think is 22 karat, that they send to the US Mint. They don't own the gold, the US Mint owns the gold. They receive it, they alloy it from 24 karat down to 22 karat, they roll it out into sheets, send it back to the Mint, and the Mint stamps it out into little circles and then coins it. That's where you get these collectors — $20 gold pieces, which actually have about $800 worth of gold in them. They're 22 karat gold. But the Mint is trying to make money. We can't have gold coinage anymore since 1933 or so — right after the Depression we went off the gold standard. Ron Paul will tell you about that, and why we shouldn't have done that. I don't know what Ron thinks about the gold standard, but a lot of people with Ron's type of monetary policy — I'm not knocking that policy. I think we overspend. I think it's going to come back to kill our grandchildren or maybe even us.
To make these radiator parts, they would make big sheets. [Tom passes radiator-die progressive samples.] It's the same type of drawing operation as the cups. They start out with sheet and then they slit it. You have to slit it because if you look carefully, you're actually making a number of these that are later going to be split into rows of two or three rather than even longer rows. When you start making these little domes it sucks in. If you didn't do this you would have fractured the material. They first make a little dome, then a deeper dome, and eventually they punch out the hole and then stack the holes together. This one actually has turbulators in it, and they braze the whole thing and make very inexpensive heat exchangers out of carbon steel.
Another thing I said I was going to pass around — we talked about surface roughness. [Tom produces a surface roughness gauge.] Here's a surface roughness gauge, so you can feel internal surface relative roughness. This is what a machinist does. He goes and feels the piece's turning on the lathe and the milling machine. He compares it, looks at it. You can also do it a little more scientifically, but frankly this is something he can carry in his back pocket. Doesn't cost $10,000 to make the measurement. They have lasers that will measure this too, but you don't add a $10,000 laser to every milling machine in the shop. So he can measure surface roughness that way.
§6. Friction and the limits of frictionless analysis [25:01]
So we talked about the general deformation zone geometry and the Delta versus yield strength plot, and that's the most important plot in Backofen. The next chapter in Backofen is about friction. I told you last time — today's Wednesday, so Monday — that in a hardness test you didn't have to worry about friction. But in fact this plot that I just handed you, which is chapter seven from Backofen, is for frictionless processing. We don't have frictionless processing. What would happen if I had a rolling mill with frictionless processing? The same thing as if you had frictionless shoes. You couldn't walk down the hall if you had frictionless shoes. You need some friction. In order to roll, you have to have some friction to pull the material into the roll. If it's frictionless, those wheels will be spinning all day long and the plate would go nowhere. So you have to have some friction.
What we want to talk about is the effect of friction. This is figure 8.1 of Backofen. Some of the science is: I've got some compressive pressure P that might be the yield strength, the local yield strength, I have some contact area K. From this I might be able to estimate some deformation zone geometry. The plastic deformation — this is a Delta equal to 10 type operation, high Delta operation, like a hardness test. But you will have a lubricant film which might get pushed aside under these very high pressures. I'm talking about pressures that can be three times the yield strength of the material. So the lubricant films don't always stay in place. That's where they had to learn about phosphating of those cold heading pieces. You may have a shear stress on this at the same time, causing sliding. It gets to be a little bit messy.
This is out of Hosford, your textbook — figure 6.1. By the way, I'm not giving you reading assignments out of the textbook. I want you to learn some of the principles, and then one night you can curl up with Hosford and flip through it in an hour and a half and say "yeah, that's what he talked about." And then someday when you need to know it, you can hire a consultant. So if I take an extrusion — they've shown this as axisymmetric, but it could be plain strain strip, where you don't have any strain in the deep dimension going into the board. Backofen often likes to talk about plain strain strip. But this one he's drawn with this little thing, so we're trying to extrude a rod. Initially I've got some little volume element of the rod, just like a toothpaste tube, and I'm going to change it from this width and height — Delta L initial — to Delta L1, the final. As I've done this, everything stays nice and rectangular, because this assumes a frictionless extrusion.
§7. Inhomogeneous deformation and the Maine molybdenum mill [29:00]
The next figure on Hosford says, well, it's not always homogeneous deformation. If I start out with a bunch of rectangles like this, I can make them flat rectangles and they're still perfect rectangles. But in fact I can get what we call redundant deformation. Redundant deformation is what takes you up to the higher pressures on that deformation zone geometry. Everything's nice and flat, Delta's less than one, frictionless, uniform deformation, rectangles go to flatter rectangles. But in the real world when I'm at a higher Delta operation like two or three or four, like extrusion, I'm going to get nonhomogeneous deformation. Why? Because there's friction at the interface. The stuff at the surface where there's friction is not going to flow as fast as the stuff coming down the middle. That causes redundant deformation. And that redundant deformation increases the extrusion pressure from two times the shear stress — which is equal to the yield stress — to 1.6 times, or whatever that deformation zone geometry curve tells me, depending on the Delta value. In the worst case, in a hardness test, it goes up to 2.57 times.
So today's key point is inhomogeneous deformation. Most of the materials processing deformation operations do not deform the material homogeneously. As a result, my grain structure, my properties, my surface finish, my extrusion pressures or forging pressures — everything's going to be controlled by the amount of inhomogeneous deformation. I'm going to end up with residual stresses.
This is out of Making, Shaping and Treating of Steel, which US Steel used to publish. It's in its 11th edition now. First 10 editions US Steel published it, then they ran out of money, and American Iron and Steel Institute has published the first volume of the 11th edition. If I'm trying to make one of these little draws on a cup, out here in the outer flanges I'll get wrinkling. If you actually look at some of those little aluminum cans going around, you might see some wrinkling. You also can get necking, because everything here is in tension, everything around here is in compression, circular compression, everything in here is in tension. Just gives you an idea of some of the types of defects you might get.
But what I really copied this page for is, US Steel 30 years ago had someone do a computer calculation that if I had lubricant with some friction, I could design a die that's not just a bevel — a cone with straight sides. I could design a contour that would take a square and turn it into a perfect rectangle even if I had friction. You could do it. But the tooling is not that easy to produce. A lot of my dies for wire drawing are out of diamond, and it's hard to shape diamond to nice circular contours. And if your friction coefficient changes, you get a different shape that the die needs to be. So we don't try to control friction, we just try to live with it.
This comes out of Backofen, his attempt to illustrate the differences in inhomogeneity. IF is the inhomogeneity factor, which he's got defined by an equation. This is lubricated strip — strip drawing on the very bottom. I don't know if they took copper strip or brass strip or a steel, he doesn't tell me — it was probably one of his students, he doesn't reference it. They take something and they draw it partway through. They don't draw the whole thing. The thing started out at a knoop hardness of 85. Of course you get work hardening on your stress-strain curve, so as you deform it and get some permanent plastic strain, the hardness increases. Some poor graduate student sat there on the microhardness tester for days mapping the entire plot of the iso-hardness lines. For that very shallow angle — it's a 16% reduction, so this height should be 84% of this height — very uniform hardness across there. A square over here becomes a nice square-cornered rectangle over here. No inhomogeneous deformation, inhomogeneity factor is zero.
If I increase the angle, I'll go from 85 not to 105 but to 120, and I will have very inhomogeneous deformation, an inhomogeneity factor of 19% — that was lubricated. Everything else being the same, but now it's not lubricated, I will have an even bigger factor — but only about a 10 or 15% increase in inhomogeneity with no lubrication versus some lubrication. If I go to half the reduction, from 16 to 0.08, I actually can get more inhomogeneous deformation. This is a higher Delta operation. Why? Why is this lower one higher Delta? More inhomogeneity, over a shorter distance. The height is the same, but look at the width of the deformation zone. Just that little angle here, compared to that angle there. So you've learned — of course you don't have to come next time. Higher inhomogeneity because I've changed the amount of deformation.
Here I've gone to wire, and the wire is axisymmetric deformation. In the strip I didn't have any strain into the board, so that's called plain strain — one of my strain tensor values is zero. If I have axisymmetric deformation, I'm pulling in one direction, actually I'm compressing in two — none of my strains are zero. So in wire drawing with axisymmetric deformation there is no plain strain. I actually have a situation similar to this one, but the deformation is twice as great. It's got the exact same die angle, and it goes from this diameter to that diameter. These two diameters are the same, but the wire compared to the strip has twice the deformation. One's compressing in two directions, the other one's only compressing in one direction. The area goes as the square of a circle and the first power of a rectangle. So if I get 8% reduction here, I have to get twice as much reduction here, because it's axisymmetric. But that means in this case the inhomogeneity factor goes down.
Well, why is that? Because I'm forcing the material to squeeze. The stuff in the center is hardly deforming at all. There's a big plug of material that doesn't get work-hardened very much. That plug of material that's not deforming — the redundant deformation is not as big. So I can go through these types of things and analyze them. You don't have to analyze them; some doctoral student had to once, lucky him. But it creates defects.
Backofen has a picture of this type of defect — cracks formed in molybdenum bar rolled under high Delta conditions. He's passed away and I can't ask him, but he probably went up to Maine to get this. He was probably hired by a little firm up in Maine called Elmet — E-L-M-E-T — Corporation. It was later bought by Philips, the big Philips that makes the DVD players and stuff in the Netherlands. It was called Philips Elmet when I went there. I went there because one of my former undergraduate students was from Maine. Charlie wanted to go back to Maine. He's still a Mainiac. Speaks Maine, almost Canadian. Philips Elmet makes tungsten and molybdenum alloys. When I went there, IBM was buying most of their molybdenum sheet to make the interconnects for the fancy computer chips. This was in the 1980s. They weren't the biggest computers, which were 16K rather than 64K type stuff. You were down in 20 megabytes of storage in your computer or something. Sounds ridiculous to you now, but that's what it was back in the '80s.
If you actually try to roll this — Backofen on the next page has a picture of the molybdenum bar that they're rolling — and it alligators. They're rolling this between two rolls that have semicircular cross-section, and the thing's got tremendous residual stresses. It just alligators out, and it's even got teeth like a crocodile. [Tom holds up the bisected molybdenum sample, held together with a thesis binder clip.] This is one of Backofen's samples that until about a year ago was in one piece. He got a piece of molybdenum from some rolling mill. I now have to hold it together with a thesis binder clip. They were rolling this thing, and it just split right down the middle. It's the same type of alligatoring. There are residual stresses in this material, otherwise it wouldn't split in two directions. That's a result of inhomogeneous deformation. That's a result of the wrong Delta for the forming operation.
In some of these cracks you have white stuff — anybody know what that white stuff is? Anybody know what the melting temperature of molybdenum is? It's about 2500 degrees centigrade. The forging temperature of molybdenum typically is going to be like 1800 degrees centigrade. Over 3000 degrees Fahrenheit — above the melting temperature of steel — to form molybdenum. The interesting thing is, at about 1,000 degrees centigrade the oxygen in the air will react with the molybdenum to form molybdenum trioxide.
So when Charlie takes me into the rolling mill to watch them roll the big molybdenum plates or ingots that were probably four or five inches thick, going to roll it into sheet that's like a sixteenth of an inch thick — not all in this one hot mill — we go up in this pulpit with big glass windows at an angle, looking out like a control tower at an airport. You see the door open to the furnace, and you see this white-hot, almost 2,000 degrees centigrade chunk of molybdenum slab pushed out. As it gets pushed out into the air, you start seeing white smoke come off — it's molybdenum trioxide. Molybdenum trioxide is volatile. They're rolling this in the air. Within 15 or 30 seconds, all you could see was a glow of this white thing through this white smoke cloud. I don't know why he took me up to show me the rolling operation, you couldn't see the rolling operation, you were looking at white smoke with this big white light behind it. Actually that's probably why he took me to show me, it was really impressive. I wish I had a video I could show you. And then I understood why the walls and everything in this room were all white — they were covered with half an inch of molybdenum trioxide. So what you're seeing there in the white, in the cracks, is molybdenum trioxide.
§8. Centerline cracks and the Blackhawk washer [43:39]
Here's a Backofen picture of a wire drawing operation, and someone formed some little cracks right down the center. This is a fairly high Delta operation — internal fracture in a round wire induced by high Delta drawing, 2011 free-machining aluminum alloy. You can see the deformation. There's your width of deformation zone, and a Delta of three or four would only take you down to here. That means you're getting lots of inhomogeneous deformation. This central plug — it's just a tensile test. It's hardly deforming at all, but I've got enough tension I actually split it. So you have to be careful in picking the right Delta for your operation. You can induce defects.
I like to show this one — centerline cracks in extruded steel rods from Don Bliclet [?]. Who's Don Bliclet? He's a graduate of this department. He was my first boss — vice president of research at Bethlehem Steel when I was a young engineer in the research department. Later when I came back here as a member of the faculty he was on the department visiting committee.
Here's another one out of Backofen. I didn't know if I wanted to show you this, but I looked at it some more and I noticed this for the first time this morning. Taught out of this book for three years — learned out of it for one year and taught out of it for two more. This is a mild steel wire undergoing axisymmetric deformation. This is from 1958. This is the type of high-nitrogen steel I mentioned before. You just pull it through the die a little bit and you can see where it deforms. So this is a fairly low Delta operation. There's the width, there's the height of the deformation zone. If I call this the axisymmetric line going down the center — this is a Delta operation of like 1.5. Not very high Delta. But look at that little arrow point right there. That's in tension. It actually started to slip and shear. All this stuff is in heavy compression, but as I get towards the center I actually get to tension. Because of the inhomogeneous deformation, the compressive forces don't reach all the way to the center. So there's more evidence of inhomogeneous deformation.
Here's Backofen just showing you a rolling operation, and they call this alligatoring — splitting down the center. He's pointing out you get very bad residual stresses in your sheet. I tell the story in some of my other lectures — I've got a washer from a Navy helicopter. This is an aluminum washer that 15 or 20 years ago cost $350 for this little washer. It's about this thick, about this big around. It's the washer that holds the tail rotor for the Blackhawk helicopter. One of them failed on an Army helicopter. If it's a Navy helicopter it's called a Seahawk, if it's the Army it's a Blackhawk, the Coast Guard it's the Jayhawk, and the Air Force, Carl — you call them Blackhawks too. That's why I couldn't think of a different name for the Air Force. Jeremy knows all about these things, he did his thesis down in that plant, or he is doing his thesis down in that plant — he spent the last six months there.
The problem was they used a particular aluminum alloy in that helicopter. By the way, the same Blackhawk design — there's also a separate line that is the presidential helicopters. I couldn't even walk over there, because those helicopters have technology in them that I'm not supposed to know about, or believe even. So an Army helicopter in Arkansas was doing a night vision goggles training exercise, and it crashed and killed six Army soldiers and two pilots. It was because this aluminum washer was supposed to have been stress-relieved and was not. It had residual stresses in it, and it got stress corrosion cracking. If you take the welding videos I'll talk about it there. I always like to tell the Navy guys when I'm teaching them during the summer that it was the Navy that found the first cracks, because the Navy is the corrosion leader in the service. They're surrounded by salt and moisture. So if anything's going to corrode, ask the Navy, they'll see it first. In fact the first cracks did show up on Navy Seahawks. But the first fatality was on an Army Blackhawk. Fortunately it wasn't one of the presidential helicopters, but it could have been.
So let's talk about a simple type of forging operation where I might take something like this, which has got a Delta operation of — actually this could be less than one the way they've drawn this. And if I — oops, we've run out of time. I guess this is for Wednesday or Friday. Sorry, I didn't watch the clock.