§1. Post-weld heat treatment: what it does and why [00:09]
Preheat we did yesterday. Post-weld heat treatment: if you go back to this Venn diagram, you have to have material, stress, and an environment for hydrogen cracking. A post-weld heat treatment for steels is typically putting it in a furnace at 1100 to 1200 degrees Fahrenheit, or building a furnace around it, one hour per inch of thickness. So if you're talking about a four-inch-thick pressure vessel, once you get it up to temperature as measured on the outside, you hold it there for four hours. That's the typical stress relief time. There are more sophisticated tables, but if you go through the thermal conductivity of the steel in order to get it heated all the way through, that's typically what you do. The rule of thumb is one hour per inch of thickness at temperature — not starting in the cold furnace, but once you get to temperature, then you start your time.
You do three things. You temper the steel to lower the hardness. You have this heat-affected zone that cooled quickly with high hardenability, so you have a wide hard zone. Above 300 degrees you start to temper, but above a thousand degrees you really temper and you get a nice soft heat-affected zone. Even if it had been Rockwell C55, right after a post-weld heat treatment you'll probably be down to Rockwell C30 or so. That lowers your hardness to a level that is not likely to give you hydrogen cracking. You also relieve the residual stresses — sometimes this is called a stress relief heat treatment. And you also remove hydrogen.
Now you shouldn't wait too long to do your stress relief if you're going to get rid of the hydrogen. You can wait as long as you want for stress relief itself, but for hydrogen removal you can't wait too long. If you've got to build a furnace around the whole thing, it takes a while to build the furnace, and so it might be days. Which is why you need preheat, to try to get rid of some of the hydrogen up front.
If you have a very high hardness steel like a 4340, take Bell Helicopter in Fort Worth, Texas — they build the military helicopters there. Can't build military helicopters in another country, at least not for the U.S. Department of Defense, so they still build the military helicopters in Fort Worth. The civilian helicopters are in Mirabel, Quebec. It's not always welding that introduces the hydrogen — I mentioned that the electroplating process can introduce hydrogen. They actually go from the electroplating bath directly into the furnace that's going to bake the hydrogen out at 375 degrees for 23 hours. It's less than five minutes between bath and furnace — they don't wait a full hour — because now we're talking about a mast made out of 4340 steel at a strength level of 240 KSI. And they are worried enough, because if you lose your mast — you've only got one mast on a helicopter, and it's not a good day if you lose the rotor. You drop like a rock. Can't auto-rotate to ground.
So post-weld heat treatment is a high-temperature, very expensive process, but necessary if you have very thick steels because of the residual stresses, and also if you have high hardenability steels.
§2. Over-matching and under-matching filler metal [04:30]
I wanted to say something about joint efficiency and over-matching and under-matching filler metal. In general we over-match the weld metal to the base metal by about — it's supposed to be zero to twenty percent, but it's typically ten to twenty percent over-matched, where the weld metal is stronger. So if this is HY80, we'd be using a stick electrode that would be an E11018. That's years ago; we use gas metal arc now, but we'd be using an E110S. The 110 means 110 KSI; HY80 is 80 KSI, so you're a little bit more. They might have used a 118 in some cases. If you're doing an HY100, you'd use a 12018 or an E120S electrode, so you'd be nominally twenty percent higher strength in the weld metal. If you pull on it, it's going to neck down and fail in the base material.
The problem could be relieved if you could use an under-matching filler metal. If you could use a 7018 electrode, you can't build up residual stress greater than the strength of the weld metal — the weld metal is going to yield, and your maximal residual stresses won't be 110 KSI, they'd be 70 KSI, the strength of the under-matching filler. That's what they did in the early days of fabricating some of the foundations for the Nautilus. They had to go to an austenitic filler metal which had half the strength of the HY80 and would absorb a lot of the hydrogen. They were able to do it until they developed procedures that wouldn't crack with the hydrogen and the higher residual stresses they were encountering.
So under-matching has been a holy grail, and people have tried. The Navy has spent on several different occasions millions of dollars making great big foundations and testing near full-scale things. When I say near full scale, something the size of a small car, and doing mechanical tests to see how it fractures. Because remember, in the submarine business you've got to set off an explosion next to it — that's what's going to happen if someone hits you with a depth charge. They've tried it and they've always found that it doesn't work. The reason has nothing to do with welding; it has to do with fracture mechanics. Think about it: if I have two very strong things held together by something very soft, and I now deform this in an underwater explosion or anything else, in the laboratory I'm going to concentrate all my strain in the weld metal. These other two things are like grips and they don't deform at all. If you're severely under-matching — by more than five percent — you'll concentrate all your strain in the weld metal, and if you've got fifty times as much base metal as weld metal, you now have fifty times as much strain concentrated in the weld, and you're just going to break it.
The fracture properties when you start plastically deforming in an explosion are lousy. People have tried this in civilian business because they can save money on stress relief, and they've proved that they don't like the impact properties. When you concentrate all your strain, all of a sudden your impact properties fall apart. They did a study and spent millions of dollars in the '60s, and then twenty-five years later they did millions of dollars again, and they concluded the same thing again. About every twenty-five years you get a new generation of engineers and someone has a bright idea — oh, we can use under-matching filler metal. You can't. Forget it. Don't go spend millions of dollars trying to use under-matching filler metal. It's been tried, doesn't work.
§3. The Helms Project: nine-month delayed hydrogen crack [09:13]
I'm going to start giving you some examples of classical failures. We've talked about the Seawolf. On the Seawolf they ended up with a very high material strength in the weld metal — too high. It was over-matching by about thirty or forty percent. You ended up not necessarily with an inherent problem in the weld metal, but with higher stresses and higher hardenability, and they didn't have enough preheat for that higher hardenability to get the hydrogen down to a low enough level.
There are some other cases to show that this still occurs on a fairly regular basis. One of the stories I was involved in, in the early 1990s, is Pacific Gas and Electric decided to build a pumped water storage project, because the nuclear reactors like to run flat out. They don't like to cycle up and down. They like to run continuously twenty-four hours a day, nice and steady. But that's not the way people use their electricity. The peak electricity time is between five and seven PM, when people get home from work, it's still hot, they want their air conditioner running during the summer.
So they went to the High Sierras — actually, it's not Sierras, it's the Sierra Nevada. I was corrected many times for making it plural. Anyway: they had a lake at about 8,000 feet and another at about 6,000 feet. All they had to do was build a pipe between the two. During the night the nuclear reactor could pump the water up to the upper lake, and during the day they could let it run down through turbines — a hydroelectric plant. They've built a number of these around the world, but this was one of the larger ones. A 22-foot-diameter pipe, miles long. Not very round pipe — maybe that's why it failed. 188 PSI water at the failure location, which was up near the upper lake. That's just the static head at that location.
They had a failure. Almost everybody had left the construction site; some guys were left to clean up. They had some little porta-potties, and one of them had gone into the porta-potty — it was nearly five o'clock — and as he's exiting the door he hears this crack. He looks about fifty yards away and sees water spraying out of a man-way, just a little flange with a cap bolted on. The man-way was so someone could get in if they had to. You'd empty the whole pipe and someone could crawl in. The pipe crossed 180 feet across a canyon — everything else was buried in the rock, they bored a tunnel and grouted it with cement, supported everywhere else. This was an open 180-foot section, in 40-foot pieces, with a little man-way down about the five-thirty position.
The guy saw the spray of 188 PSI water and headed for high ground. He made it. Nobody got hurt. He and one other guy got in a pickup truck to go up to the upper lake to shut the 22-foot-diameter valve. Turns out 22-foot-diameter valves are not the easiest thing in the world to move, and this one hadn't really been exercised even though it had been put in place a year before during construction. It took them half an hour to close it. In the meantime, when this thing completely broke apart in a brittle fracture, you had 4 million horsepower heading up against the canyon wall. That 4 million horsepower of water ate away a hundred feet of the canyon wall. It was no longer a 180-foot-wide canyon, it was a 280-foot-wide canyon when this was done. The upper lake dropped by about two-thirds in volume down to the lower lake. Some came down the ravine beside the mountain, carrying everything — bears and rabbits and raccoons running for their lives, some drowned. Built about a 300-foot-long sand bar at the lower lake, wiping out the ravine.
It also did about 180 million dollars worth of damage. As a public utility will typically do, they went to the rate commission in California: we had an accident, we'd like to put it on the rate base, spread it like peanut butter over all the rate payers in California. The Public Utilities Commission said: you can't do that unless you sue American Bridge of U.S. Steel, because your expert said this was a manufacturing defect. American Bridge had manufactured this. It turns out one of the founders of one of the world's largest engineering consulting firms in California was out there three days later. He gave a press release saying it was American Bridge's fault. So now they have to go to trial — if they don't, the Public Utilities won't let them put the money in the rate base. The actual rebuilding was 180 million; the total loss was 800 million in terms of lost power and production. They wanted all of that in the rate base, so it had to go to trial.
They already had two metallurgists, and they hired me as a third. I said, what's going on here? They said: the judge has said he can't have more than two, we're just going to let you talk about the welding. We want you to talk about how this crack occurred. If you looked at the fillet weld that held the man-way to the pipe, there was what looked to me like a hydrogen-induced crack. It was oxidized — the crack was hydrogen-induced but oxidized. According to the boiler and pressure vessel code, this was inch-and-a-quarter material, and inch-and-a-quarter material with a fillet weld does not have to be stress relieved. If it had been an inch and a half thick, the code says you have to stress relieve it. Under certain exceptions in a certain paragraph of the code at inch and a quarter, you don't. Well, it costs a lot of money when you're 6,000 feet in the Sierras to take something 22 feet in diameter and stress relieve it, so they decided not to.
So I had to look and figure out why this thing failed. There's my stress — they didn't stress relieve it. I had a material that was susceptible but not terribly susceptible, and they had welding procedures that should have prevented hydrogen getting in there. But in fact, when they're building this in the High Sierras — you can't truck up 22-foot-diameter pipes, they don't fit on the trucks or the roads — they had to fabricate on site. They had a big camp, bunkhouses where these people would work. It was getting close to Thanksgiving and they were going to shut down after Thanksgiving, because the snows had started in early October. These people were working in the snow at 6,000 feet in the Sierra Nevada.
They were welding on this thing, and they had supervisors and quality-control people, except all those people decided they wanted to go home early for Thanksgiving. As far as we can tell, this was welded on the Tuesday or Wednesday before Thanksgiving. We have a progress picture showing six inches of snow on the inside of the pipe on the day they were supposedly welding. They had to preheat, and they probably did preheat the outside, but how well do you think that lasted if you had six inches of snow an inch and a quarter away? They probably got their torch out and used their little template stick: oh, we got the outside to 150 degrees, which was their preheat temperature. That probably lasted all of four or five minutes once you took the torch away. So they were basically welding without preheat, even though they thought they were doing it. No supervisor to say: hey, go shovel the snow off the inside of the pipe. The pipe was lying horizontal — you can see in the picture, snow on the inside.
The interesting thing was, they had just pressurized the pipe up nine months later in the spring. The snows had melted, they were about to start the project up. The crack didn't occur for 18 hours after pressurization. Delayed cracking. The guy who three days after the failure had said it was not hydrogen cracking — he said so because he knew hydrogen cracking always occurs in the first couple of weeks. That's true if you don't refrigerate it. You can trap the hydrogen in there, and if it's frozen for eight and a half months of the year you can still get a hydrogen crack. It had been pressurized 18 hours before at 188 PSI. They had all the pressure logs — there was no wave of stress going through. It just let go 18 hours later. I said it was a hydrogen crack, but I wasn't allowed to say it was a hydrogen crack because this other guy, whose wife drove around in a Rolls-Royce — a big Rolls-Royce, not a small one — had said three days afterwards it wasn't.
So we go to trial. I'm the last expert at trial, and I talked about the lousy welding procedures and the lack of process controls and supervision. We end up losing the case. American Bridge's defense was that the foundation wasn't steady enough and it had cracked 18 hours later because the foundation had slipped. I thought that was a stupid thing, but nonetheless the jury found in their favor. We'd done what the Public Utilities Commission said — taken them to trial. The interesting thing was, because this guy from the big consulting firm had blamed American Bridge in the press three days after the event, not only did we not collect the 100 million dollars we were asking for, they had to pay 17 million in punitive damages for defaming American Bridge. So we lost 17 million on top of not getting 100 million. But they had done what the Public Utilities Commission required, so the California rate payers got to pay for all of it.
One more interesting thing — I might as well put this on YouTube. My bill at the time, early '90s, for the previous two months and several trips out to California, everything, was $55,000. Largest bill I had ever sent anybody, by a factor of two and a half. I thought I'd take forever to get paid. I got paid in less than three weeks. That's because the big consulting firm's bill for the same period was three million dollars. The utility litigated against them because they had so many people working on this. They were having the younger, lower-priced people bill at the rate of the higher-priced person, and those higher-priced people were putting in for 120 hours a week. Some accountant noticed and said, this doesn't make sense. That was one of the reasons I got paid quickly.
So we've talked about Seawolf, we've talked about the Helms Project. This is one of the few cases I know where hydrogen did remain for nine months — but it's a special case. You don't usually freeze your weld for nine months.
§4. Boston Navy Yard destroyer boiler weld [23:03]
Another case — this must have been about 1978. I joined the faculty in '76 and couldn't really quite feed my family. I got a call one afternoon from what used to be a Navy shipyard we had in Boston, since closed. They had a destroyer that had been dry-docked for a number of weeks. It was coming up on time to get out in another week or two, and it wasn't going to make it, because they were trying to weld chrome-moly steel pipes from the boiler.
The chrome-moly was about one or one-and-a-quarter-inch-diameter pipe, fairly thick wall. It was stainless steel in the boiler because of the higher temperatures, and then they had to make a transition weld to two-and-a-quarter chrome, one moly steel, which has very high hardenability and very good high-temperature strength. The very high temperatures in the heating system required stainless steel, but stainless steel is expensive, so they had to make a transition weld. They had to repair some of these pipes in the boiler. They had a procedure from Philadelphia Naval Shipyard developed for this weld. It was a gas tungsten arc weld, just a little pipe like this. They'd been trying for six weeks to make this weld. They had area experts from Philadelphia Shipyard come up to show them how. The NAVSEA procedure said use Inconel filler metal, a nickel-chrome alloy. I might have this backwards — it's been almost forty years.
Every time they welded it, they'd do a post-weld heat treatment for an hour, that was part of the procedure. They'd take it off, do a dye penetrant check because it's stainless steel rather than magnetic particle, and there'd be a crack. So they kept getting cracks. If they couldn't weld these things, the ship couldn't go out of dry dock. They called me in and said: we've been able to weld it if we use stainless steel filler metal — we want you to write a letter to the Navy and tell them it's okay to use stainless steel filler metal. Well, I was 28 years old. I didn't have a clue. I was supposedly a welding engineer, just left Bethlehem Steel a couple years before. I went home late — didn't catch the bus in Central Square — went to the library and looked it up in the welding journal. Found out from ten years before that if you weld it with stainless steel it'll be fine for the first ten years, then it'll crack, because you'll get carbides going into the stainless steel. That's why NAVSEA had the procedure of welding with Inconel filler metal — carbon couldn't diffuse through in some of those regions.
So I thought, well, I can't tell them that. I went down to the shipyard. I thought I was just going to talk to one or two people — I was still naive about consulting. They put me in a conference room right off the shop, and about ten engineers came in, some from the contractor and some from the Navy. The contractor, who hired me, said: we want you to tell them it's okay to use stainless steel. I said, well, I can't, and here's the paper that says why you can't. But tell me a little more about your problem. They were making welds — the weld prep looked like this, a pipe welded from one side. They were putting the root pass in with gas tungsten arc and then trying to put in fill passes, but the root pass would always crack. They said: with stainless steel we get no cracks, with Inconel we always get a crack, and we want to do it with stainless steel.
I said, well, you can't. And they said, well, what can we do? All I knew was this Venn diagram. I couldn't change the material, that's what they made the ship out of. I couldn't change the environment — they were using gas tungsten arc, and I asked, was everything clean, do they have any sources of hydrogen? No, they were paying attention to all that. The only thing I had left was stress. If I could relieve the stress on the weld, I might be able to make this joint. People had been making this joint in other shipyards for years. So I said, why don't you just machine the joint prep a little differently — make a U-joint or a J-joint, whatever you want to call it, with a big long land. This might be 3/16 of an inch; you'd have 3/8 of an inch, put your root pass in there, because now it's like a flexible diving board — I can get rid of some of the stress. As it was, this was fairly highly restrained, nowhere for it to go. The reason other people had probably been successful, I don't really know, is that these guys were probably butting things up tight, and other people may not have had things quite so tight, or they were putting in a bigger weld.
That was the only thing I could think of. Remember, I'm a 28-year-old among all these forty-, fifty-, and sixty-year-old people. I was about ready to leave, realizing I had gotten in over my head. And they said, oh no wait, we'll do it — we'll make the weld right here. They got a couple of stubs and the guy machined it on the lathe. The whole time the foreman is saying, this will not work. This is the 60-year-old foreman of welding: this is not going to work, this is not going to work. They machined it and asked me, is this how you want it, and I said, yeah, that's about right. They welded it, then wrapped it in a fire blanket to slow the cooling rate, simulating slow cooling of the post-weld heat treatment. That took 45 minutes. Then they had to do the dye penetrant inspection. Anybody who knows dye penetrant: you first spray it with a red penetrant out of a spray can. So the foreman is spraying it, still saying it's not going to work. You wait five minutes for penetrant, then clean it off, then put the developer on. He's still saying this is not going to work. And it worked. No cracks.
So what can you say when you don't know anything about it? You can go back to the fundamentals. I couldn't change material, they already had a very good low-hydrogen environment, the only thing I could do was relieve the stress. And I thought of a way to relieve the stress, and I walked out of there a hero. I should look up what I charged — I have records, I think I probably charged 180 bucks for that, and I'd been there a couple of hours. I walked out the hero and thought, I'll get some more work from these people. Then they closed down the shipyard. But they did get the ship out. So that's a hydrogen cracking problem, and it illustrates: you go back to the fundamentals and figure out what you can change.
§5. The 7,000-ton forging press repair [31:33]
Another hydrogen case — I showed you the 17-inch-thick weld from the forging press. This press had gone into service around 1948 or so. It's a 7,000-ton press that had been making forgings for over 50 years, close to 60 years. One day it just cracked in the top head of this forging press. The piece is about eight feet tall — it had some hydraulic ports, and a great big hydraulic chamber, with posts coming down from there, and the whole thing stands six or seven stories tall. But it was this top casting. When I was standing next to it to get up to the top, you had to get on a ladder, because the casting was about eight feet tall.
They had to weld something about 17 inches up near a hydraulic port for the press where the crack had occurred. They hired a company from down in Georgia, very accomplished, very sophisticated welders. These guys had probably graduated from high school and may have had some welding training, but they weren't engineers — they were very good welders. [Tom holds up a weld sample.] That's an excellent weld. This is the piece I passed around. I could pass it around again. Technically it was excellent welding. And they knew it should be preheated if it's that thick. We had pictures: they preheated it for about an hour. Except it was 17 inches thick, and it's supposed to be one hour per inch of thickness.
Now if I had a roast beef that was 17 inches thick — a great big steamship round on a cruise ship — and they put it in the oven for one hour, do you think you'd want a slice through the middle of that? Probably be a little rare, don't you think? Well, steel has a little better thermal conductivity, but they never got anywhere close to a real preheat through the section. For them, that's all they'd ever had to do — they'd never welded 17-inch-thick material before. They did know how to make a good weld. They put down somewhere between 400 and 600 passes, and they did it in a day and a half. They were working 24 hours a day. When they finished, that evening someone heard a big bang. That was the crack running. It was just from residual stresses. Hadn't been stress relieved, had been under-preheated. They didn't think they were going to have to do a post-weld heat treatment 17 inches thick, or peening in between as we used to do on armor steels that were 17 inches thick, to relieve the residual stresses.
So they decided, well, we need more preheat. They came in with heating blankets and heated up just locally. This thing is big — 15 feet across and eight feet tall. They heated locally, and this time they successfully made the weld, put it back on its post, and on the first shot to forge something — big bang, cracked again. At that point they decided it was scrap. But they had a spare from 60 years before, some other press piece, and were able to fix the machine and get working again. In the meantime, this cost about five million dollars. The owner wasn't happy with their welding. There wasn't sufficient engineering oversight for what would be a little beyond the normal welding these excellent welders knew how to do. So it's not just a certified welder who can put down a good bead. Sometimes you need real engineering expertise. Increasingly I see that we don't have the real engineering expertise. I think yesterday's presentation on what happened at Newport News — they just didn't have the engineering oversight there. Hey, by the way guys, there are different types of materials out there.
§6. The pea shooter: a more disconcerting story [36:14]
That's one story. Another, a little more disconcerting, was a pea shooter. A pea shooter is the drive shaft coupling on a helicopter between the engine and the transmission. In a helicopter they flex, so you need to have something that can articulate a little bit between the engine and the transmission. They have a hardened steel tube with internal splines that fit in at each end. They call it a pea shooter because it's just a tube, but it's high hardness, it's nitrided. It's kind of a big pea shooter — like three-quarter-inch black iron pipe, except it's probably a five-thousand-dollar pipe, machined very precisely. They had a procedure, and there was another metallurgist — actually from Vancouver, Canada — working on this. And all —