§1. Solder flow geometries and area bonding [00:35]
This is the old packaging technique, still used in many things — J-leads coming out of an aluminum oxide package. It shows the types of solder flow you can get, many of which are bad because of variations in solder wettability at different locations. You get different contours, and people used to do computer models of the surface tension of how these things would flow. This is a gull wing — those are J-leads and these are called gull wings. You run into problems with how the solder flows.
Area bonding — we talked about that briefly. You can have a PC board with a bunch of packages on each one of these slots. This is a composite that's probably about 13 layers thick. The other one I passed around was 21 or 22. This is one of the layers. They metallize the layers, and they have to register very closely when they bond them together. That's a resin, a plastic that's been metallized with copper, and then tin-plated, and they're going to form a transient liquid phase diffusion joint — tin into copper. They'll get the vias between the layers. They may put it in a plating bath later and plate that to get connections going through the thickness of the board. Then you'll take components that may have solder balls on them, flip it over, and make the solder bond.
§2. Thermal expansion mismatch and chip cooling [03:12]
We've talked about flip chip and the problem of thermal expansion. Coefficient of 2.6 for the integrated circuit; thermal expansion for glass aluminum epoxy, glass polyester resin — which is basically what that sheet of plastic is — of 6 to 27. You've got a real problem. The plastics have large coefficients of thermal expansion. Silicon is a ceramic, fairly low. Sometimes people are bonding from silicon to a copper heat sink. When you get to a powerful chip like a Pentium or one of the Itaniums, or whatever the Intel chips are now, these little chips will put out 30 watts when they're humming along. 30 watts per square centimeter is roughly equivalent to taking a plumber's propane torch and putting it right on the surface of something, just holding it there. That's the heat transfer rate of that flame against the surface. When these chips are operating, you've got to cool them down.
In your laptop you're running at two percent duty cycle or so, but in a high duty cycle application — number-crunching in a supercomputer — we're limited by the heat we generate. We're limited by lots of things, including the frequency, how fast you can operate the computer. But one of the things you're limited by is the amount of heat you can generate and pull out of there. IBM, for their 360 mainframe, had gaseous helium going in among the chips. The whole thing was sealed and they had a heat exchanger with gaseous helium.
Why helium? The lighter the element, the better the heat conductivity in a gas. It goes as the inverse square root of the mass of the gas. The kinetic theory of gases tells you that the thermal conductivity of the gas is proportional to one over the mass. So if I have air — diatomic oxygen at 32, nitrogen at 28 — but helium is at four. One over four, take the square root, is one half. One over thirty is about one fifth. You can get two and a half times the thermal conductivity with helium that you can with air, and about three times the conductivity you get with argon. This actually gets to be important when we do arc welding, where we like to use helium. But they now have to go to water cooling in many computers, because gas just has not enough molecules to carry the heat away fast enough.
§3. Solder balls, self-alignment, and chip repair [06:30]
On the side of solder balls — I told you about the Bond number, that by surface tension, if you melt something properly, it should form a sphere if it's less than about three millimeters in diameter. So one of the ways they make these little solder balls on these flip chips, or C4 connections, is they'll electroplate lead-tin alloy. They remove the resist, the polymer that protects the surface and only lets you plate where you want. You end up with this little pad, and then they just reflow it. They melt the lead-tin and it balls up naturally.
Once you get that ball, fortunately, because of surface tension, it helps you if you mess up. If this is your pad and you misalign the chip so the balls are way over to one side of the pad you're trying to bond to, it will actually create a restoring force. The surface tension wants to bring those misaligned balls into registry, so it's self-aligned. There's a little torque, a little XY translation, and it's self-aligning — one of the advantages of flip chip.
When you start looking at your silicon chip, and through your circuit board, and your balls — you may have several layers of these things, with all kinds of layers in between with wires routed. It's a rat's nest of wiring. Back in the old days, they had a problem: they only put 10 million transistors on a chip and most of them had to be good or you had a bad chip. Nowadays they build redundancy into the chips with 100 million transistors. You can afford to lose 5 or 10 million transistors as redundant, so you can reprogram your circuits and use other areas. If you have a bad area on the chip you can reprogram it in software, and the hardware takes rerouting. Or you may go in there with a little focused ion beam.
Student: What's a focused ion beam?
Gallium atoms, usually. Focused ion beams came around in the 1980s. They've been around since the 1950s — they've been making tungsten tips very small, down to an atomic scale, for atomic probe microscopes, since the 1950s and 1960s. They have different etching techniques to take a thin tungsten wire and make it essentially atomically smooth. You can have a radius at the tip of 50 atoms. Then they put gallium on there, and gallium is second to mercury in terms of low melting point metals. Mercury's liquid at room temperature; gallium melts at around 85 degrees centigrade. So it doesn't take much. You put gallium on there and you get a thin layer of gallium by surface tension. Then you put 20,000 volts across it and you can strip off gallium ions — you get a focused ion beam.
They now have these things in scanning electron microscopes. They first put them in transmission electron microscopes, and you could machine your sample on a 10 or 20 angstrom scale. Pretty neat. You're just hitting it with 20-kilovolt — not electrons — gallium atoms. The gallium atoms have 20,000 times the weight of an electron. So you can be pretty impressive with the holes you can drill on a nanoscale.
Focused ion beams can repair chips. They can machine things down to 10 angstroms, which means they can break circuits, and they can actually deposit gallium as a solder joint to bridge new circuits, so you have extra transistors on your chip.
The largest single use of scanning electron microscopes in the world is quality control for the semiconductor industry. All of your $400, $500 chips — your big expensive computer chips — they all get an inspection in a scanning electron microscope. I haven't seen it, but I'm told there are rooms at Intel with a hundred scanning electron microscopes, because it can take an hour. Hey, it's a $500 chip, right? It can take an hour in the SEM to check it out, program it, find where the good spots are, the bad spots, and everything else. Because one bad joint and the thing's no good. But now they basically have redundancy so they can reprogram it, use focused ion beams to repair them, and so on. So there's a lot of technology that goes into that.
§4. Brazing: advantages, strength, and erosion cases [12:42]
Unless you've got more questions on micro-joining and electronic packaging, I'll now go into brazing and do it fairly quickly. We've already talked a fair amount about brazing. Ordinarily I might be running two or three lectures behind by now. It's because you're not asking me questions, so I can digress. What I need is questions like the focused ion beams, or one over the square root of the mass. I'd much rather digress than go over these ancient lecture notes.
Brazing is just a higher temperature than soldering. Same process. But because of the higher temperature, you have several advantages. One is more flexibility in fluxes, and the fluxes become more reactive because chemical reactions proceed faster at higher temperatures. It's just the Arrhenius equation. So while there were some things that couldn't be soldered — beryllium, titanium, tantalum, niobium — because you don't have the chemical reactivity at the soldering temperatures below 450 to clean off those very stable oxides, at brazing temperatures there is no oxide that can't be destroyed by a good brazing flux or brazing technique.
Essentially everything — where you can get the right wettability of your filler metal with your substrate, meaning your filler metal has to create a lower interfacial energy than whatever your fluxing component has. You want to displace the flux and bring in the filler metal with a lower interfacial energy. We usually use metals on metals, but you might use ceramics on ceramics. You have more flexibility in your choice of fluxes. I have never seen anything that can't be brazed except things like polymers that can't go above 450 C — they just decompose. If it's stable above 450 C as a solid, I have never come across anything that can't be brazed. Carbides — in fact I passed around a carbide drill tip. Diamond. Graphite gets brazed all the time. Carbon gets brazed all the time, works with platinum at very high temperatures. You can join almost anything that's stable at high temperatures.
Room temperature strength is greater. I told you the other day a very rough Tom Eagar rule of thumb — you won't find this in the book — for a solder joint, you should never have more than a thousand psi. That's seven megapascals. In fact you'd like to be around one or two megapascals as the stress level on a solder joint, because otherwise over a thousand or two thousand or ten thousand hours the thing will just pull apart. With braze joints, a typical strength will be 5000 psi, and creep is not usually a problem — you're at higher temperatures. You can go as high as 40,000, but then you really have to get into controlling the coefficients of thermal expansion, because in fact your braze joint should be stronger than even 5000, but you usually have residual stresses in there with this number of metals that lower it.
When I say a thousand psi with solders, that's higher-temperature solders. Lower-temperature solders are going to be around 100 psi. The brazes are stepped up three, four, five hundred degrees in temperature, so they're over the creep regime. If I had to use a good rule of thumb, 5000 psi is a good number. But I know cases where people braze carbide bits or ceramic bits to machine tools — these are machine tools where you're tearing up the road or you're mining, reclaiming asphalt. I had a student develop a braze alloy for Norton where they wanted to put carbide tips on these things that reclaim asphalt. They're tearing up, taking all the asphalt off the road, and they leave these grooves in the highway. Those are carbide tips. They might last one evening of tearing up the road. It's pretty aggressive service.
If you start losing your tips by brazing, you can't lose very many tips before this whole great big expensive machine goes down, and now it's going to take the rest of the evening to re-tip it, and you lose tremendous productivity. So the student developed a braze alloy where he got a better matching coefficient of thermal expansion. He ended up using titanium hydride as a paste powder with copper and tin. He had about six components in there — carbon — and he would actually form titanium carbide in situ. Titanium hydride decomposes around three or four hundred degrees centigrade, just drives the hydrogen off, so you end up with titanium metal. If you're brazing in a vacuum, he ended up with a copper-tin titanium carbide composite. Titanium carbide is a ceramic that melts above the temperature of the brazing alloy. So you're making an in-situ composite brazing alloy. With enough titanium carbide in there, his coefficient of thermal expansion of his brazed alloy was half of what you would get with a copper-base brazed alloy.
With lower coefficients of thermal expansion he got tremendous strengths — well above 5000. I don't know that we measured the strength. His way of measuring the strength was, Norton would go out and tear up roads. It was an engineering approach. He wasn't looking at a shear strength or a simple tensile strength of the braze joint. They just went out and saw how long the things lasted. They lasted three times as long. That's pretty good. Before, they might have to re-tip once a night and lose hours. If you can get the whole evening when the roads are closed and run the whole period, that's a tremendous advantage in productivity. So essentially he made a composite braze alloy. It was reacting while it was brazing to form solids within the braze alloy, and it was still wetting the alloy.
§5. Volatilization, vacuum furnaces, and the cross-field amplifier fix [20:29]
You have to worry about residual stresses to get the very high strengths, but you can get very high strengths. You have to worry about volatilization. Zinc and magnesium are big problems. They both have very high vapor pressure. Zinc boils at 900 C. Magnesium is around 1100 C. You're getting to reasonably high vapor pressures at your brazing temperatures. You stay away from zinc in your vacuum silver brazes, because you'll just contaminate your whole vacuum furnace. That vacuum furnace just sucks the zinc right out of there, and you'll end up depositing it all through your furnace and you'll destroy it.
I had a situation where a guy had a two-million-dollar brazing furnace down in San Diego, and someone put the wrong braze alloy in there, ran the brazing system, and contaminated the whole system with zinc. Rather than think about how to do it, they decided they'd just try to heat the whole thing up even hotter — vaporize it out of the furnace. Except the furnace has hot spots and cooler spots. The outside is water-cooled; you can put your hand on the wall of the vacuum furnace when it's running. So all they did was move the zinc into the cooler regions. By the time they screwed up trying to fix it the quick and dirty way, they ended up destroying the whole furnace.
At higher temperatures you end up with — I told you about the problem when they were trying to braze the molybdenum to the copper for the cross-field amplifier for the radar. They originally had an 82 gold, 18 nickel braze, and they were forming nickel-three-moly intermetallic, and you get like five degrees bend and the whole thing would snap. Then they got to a transient liquid phase — they only had three percent nickel in their braze alloy, a lot less gold, a lot of copper. Formed a TLP bond with no intermetallics; you could bend the thing like a hairpin 180 degrees.
§6. The recuperator: brazing a room-sized heat exchanger [23:14]
On erosion — in soldering you can have it, but it's not usually a problem. In brazing, you can have erosion of 50 or 100 microns or even more. [Tom hands around a section of brazed heat exchanger.] This was a heat exchanger about the size of this room. It's all brazed together all at once. It consists of stainless steel, and there are little tubes and big holes, and they were crossing each other. This was for an internally cooled recuperator for a naval ship.
The destroyers and frigates and cruisers all run on oil, and they get their oil from the aircraft carrier that runs on nuclear energy. The aircraft carrier is big enough that it carries all the oil for all the sister ships protecting it. Because of the problem of a nuclear strike, the destroyers and frigates need to be about 30 miles away from the carrier when they're on duty station. The problem is, 30 miles is a significant fraction of how much fuel they have to burn, and they would spend 10 to 20 percent of their duty time just going back to refuel and going back out to station. They wanted to get to the point where, rather than 10 or 20 percent of duty cycle time going back and forth to refuel, it was only about five percent. They wanted to preheat the incoming air going into the boiler that's burning the oil.
So they built a heat exchanger about the size of this room, and they stuck it on a turbine at Rolls-Royce in England. This whole braze system was supposed to last for a hundred thousand hours. I calculated it lasted for two minutes before it started leaking. It was a $100 million Navy program, about 15 or 20 years ago. They were trying to save money. It was right after 1992 when peace broke out with the former Soviet Union, defense budgets were going down, and they decided they'd only do a 2D finite element model of the heat transfer. No one told the gas it had to go through this thing symmetrically. So this great big three-dimensional object — some of the gas went this way, some went that way. Within two minutes they had tie bars that were six-inch-thick hardened steel holding the whole thing together. Within two minutes — and you can calculate that's how long it takes to start heating up some of this metal to high enough temperatures that the thermal expansion stress just starts snapping these tie bars. The whole thing turned into a pretzel.
I was on a team that had to go in and tell them what happened. It wasn't too hard to figure out. It had nothing to do with the braze joints. It had to do with the fact that you cannot assume that the gas will always go through symmetrically, and that things will heat up uniformly because you want them to. Wishful thinking is not good engineering. But those are some complex objects you can make with braze joints.
§7. Turbine shroud seals and the salt-shaker brazing job [27:10]
Now this is another braze joint where it gets to the problem of erosion. Inside a jet engine, you have the turbines spinning around inside the shroud, the stationary shroud. You've got the turbine spinning, with the disc going around and the turbine blade. You don't want gas to slip past the turbine blade at the top. Originally they just tried to machine things very precisely, but the problem is these things get hot and they creep, so their length increases. In some cases they actually braze on a carbide, and they want the carbide to eat into the shroud as it gets longer with age. So you get a perfect seal.
You can lose 10 or 20 percent of your efficiency. This is the hot section. In the compressor section, you can lose a lot of efficiency if the compressed gases start leaking back toward the front of the engine rather than being pushed to the back. So what they do is they make a honeycomb of high-temperature nickel-based superalloy, and they braze it together. This honeycomb has only got a thickness of about three or four thousandths of an inch of sheet metal. [Tom holds up a used shroud section.] This is a used one. You can see where the turbine blades have been cutting right through this as it spins around at high speed. This is a section of a shroud.
Student: Doesn't that contaminate the engine?
Oh no, it's very fine. This stuff is microchips — they just add more fuel to the engine. They're going to be microns, maybe 10-micron size. It's just grinding swarf, very finely divided, and it'll just oxidize. The engine adds more fuel. When they first assemble the engine, the clearance is probably slightly negative, like one or two thousandths negative, and it cuts in. The first couple of times you spin around — it doesn't take long because that honeycomb is pretty weak. You can't have too much clearance for the thing, you can't get the thing to spin obviously, but that first time you want to spin it, you've got a little inertia from all the friction. Once you get a good spin, a couple of spins just eat it away, and now you've made a good seal.
In the old days, because of the erosion of the base material, they used to use this 82 gold, 18 nickel brazed alloy I told you about. The reason is there's no erosion of nickel and gold against a nickel-based superalloy. But the types of braze alloys they like to use now are nickel-phosphorus, nickel-carbon, nickel-boron. These actually dissolve part of the base material when they first try to use them without any inhibitors. The inhibitors can be things like chromium and palladium, which at one time was cheaper than gold. It's now even more expensive sometimes because of catalytic converters in cars.
In the old days, when I made my wife's wedding ring, I used palladium because I couldn't afford all the gold — palladium was cheaper than gold. I was actually using platinum for her engagement ring. But I ran out of iridium — it's a long story. I had to lie to Engelhard to get the iridium. There's only about 100 ounces a year of iridium mined in the world, and I only wanted half an ounce. They wouldn't sell it to me. I had to go to my thesis advisor — I was working on superconductivity, niobium-three aluminum, but there was a niobium-three iridium alloy. I got him to sign a note to Engelhard saying we were going to use this for scientific research, and so I got my half ounce of iridium. I made the engagement ring. A year later, Engelhard sent two people by Bob Rose's office to find out how the research went. He didn't tell them we already had a son — he just made something up. But I had to get permission to buy half an ounce of iridium, which I thought was kind of silly. So I ended up making the wedding ring out of palladium because we had some lying around the lab.
The gold-nickel does not erode the base material. These other alloys could erode two thousandths, 50 microns deep. Your four-thousandths sheet metal gets eroded from both sides and you've got nothing left. You don't have a honeycomb; you have a blob of melted metal on the surface. So in the mid-70s they were using 82 gold, 18 nickel. By the early 80s they got rid of it because the price of gold went up to $800 an ounce from about $200 an ounce, and there was enough financial incentive to get rid of it.
But let me tell you what happened here. At an aerospace company located here in New England that will remain nameless, they would get this as a powder in 50-ounce jars. They would take a salt shaker — literally a salt shaker — and they would put the honeycomb inside the shroud, and a person would take the salt shaker and shake some of this gold-nickel brazed alloy into the pores. Then they would take some Krylon crystal clear lacquer like you buy at the hardware store, and they'd spray it on to hold the powder in place. Then they'd put it into a brazing furnace and melt the gold-nickel alloy and make the shroud with the seals.
In the mid-70s they were building a lot of this particular military engine, and the guy in charge of the brazing area would go through about one jar of this 50-ounce stuff a week. Then production scaled up, and he'd get two jars a week. To get a jar, all he had to do was go down to the supply area in the plant. He had to have his supervisor's signature, because if you think about it, at $400 an ounce — about what the price of gold was at that time — if you've got 41 ounces of gold in a 50-ounce container, that's sixteen thousand dollars a jar. It's not a very big jar. It's only about three and a half pounds of gold, which doesn't take up much space.
Production ramped up and he was using two jars a week. Then production started ramping down, and he thought, "Ah, what the heck, I'll still get two jars — one for the company and one for me." No one caught him until about 16 months later, when someone turned him in. The whole system didn't have controls. I was hired to come in because the whole operation under government contract was bonded, which meant an insurance company had to pay for any losses of precious metals. The aerospace company didn't really care — they had been paying the insurance and passing the costs on. But the insurance company wanted to know how much to reimburse. Because all they were doing was putting a lot of salt on one part and a little salt on another. So I was hired to do an audit to figure out how much this person stole over the previous 16 months. It was somewhere between 1.6 and 2.5 million dollars worth of gold over 16 months.
By the time I got there, they were still using the salt shaker technique, but they would weigh the salt shaker before they sprinkled the part, and then weigh it afterwards. Before that, they didn't even know how much gold they were using per part. Who cares? The government was paying for it. It's a cost-plus contract. I came up with a range of numbers, and I'm sure the insurance company paid the government back that amount of money. But the rest of the story: the guy in Connecticut who was doing this got a one-year jail sentence for stealing several million dollars. In mid-70s dollars, that'd be like stealing 10 or 15 million today. You have to ask yourself whether one year in jail is worth 10 or 15 million dollars. The guy who was running it to New York City got six months suspended. And the guy who was fencing it in New York City to sell it didn't get anything. He got off. Because it's just an insurance company paying the bill — no one really cared.
But anyway, that all had to do with erosion of the base metal in brazing. If you think that's true. I've got stories.
§8. Braze alloy families: aluminum, silver, and the radiator revolution [37:35]
There are other things about brazing. Just like I showed you families of solder alloys, braze alloys are above 450 C. There really is nothing between 400 and 500 centigrade. You start the braze alloys in these aluminum alloys. Aluminum is difficult to braze. However, we braze a lot of aluminum. Anybody think of what the largest application of aluminum brazing is in the world?
Automobile radiators. Back when I was your age, most radiators were copper in cars. A mechanic could repair a copper radiator — if it sprung a leak, he'd get out his little propane torch, pour braze alloy in until it held air pressure, and loaded up until another leak started. Around 1980, Alcan Aluminum developed a brazing flux for aluminum that was not so fussy that you had to do it in a plant. The mechanic in the auto shop could take some of this flux, paint it on with a little acid brush, and braze it just like he was brazing copper. This was a fluoride-based flux — don't tell him he's strengthening his teeth by breathing this in. Hydrofluoric acid and others. They developed a brazing technique so that radiators didn't have to go back to the factory. In the early 1970s, the only automobiles with all-aluminum radiators were things like the Chevy Corvette, where weight was critical. If you could afford to buy a Corvette and you sprung a radiator leak, you just bought a whole new radiator. You could braze them in the factory in the early 70s, but you couldn't field-braze them until Alcan developed this brazing flux. With that brazing flux, they opened up a whole new industry, got rid of all that copper, and now aluminum is used for brazed radiators.
Silver solders are actually braze alloys, with different amounts of copper and zinc. Again, you have to keep the zinc out if you're going to use it in a vacuum application. Down here we've got cadmium. Cadmium's a problem. Why is cadmium a problem? Cadmium's toxic. Just like mercury or lead, and it's very volatile. It'll come off. If you were doing cadmium torch brazing in a factory, or you're a plumber doing silver brazing for a critical plumbing application, you could get what they call metal fume fever. Metal fume fever is when you breathe in certain types of metal. Zinc is one of these. Zinc is not really that harmful — if you work in a brass foundry without good ventilation and you breathe in a bunch of zinc oxide, zinc oxide is not really that harmful. You go to the health food store, they'll sell you zinc supplements. You just pop a few zinc pills in your mouth. If you don't want to do that, go eat some oysters — about one and a half percent zinc.
So zinc is not harmful in itself, but if you ingest it through your nasal passages and it gets down to your lungs, the zinc oxide forms zinc hydroxide, and you get metal fume fever. I've never had it. A technician I know said he had it once. He says first you get so sick you're afraid you're going to die, then you get so sick you're afraid you're not going to die. It only lasts about 48 hours, you're fine afterwards, and there are no long-term effects. Now, cadmium — that's not true. Cadmium, your liver doesn't get rid of it very well. But there are certain advantages to cadmium silver brazing. First, you use less silver than a lot of other alloys. This is silver content versus temperature. It also operates at the lowest temperatures. For production, cadmium silver brazing is great. But in general, they aren't using it anywhere near as much because of the toxicity problem.
§9. Cadmium in light switches and Swedish house fires [42:27]
But there are other stories about cadmium. Light switches, right here. I just released some cadmium atoms into the room as I turn the light switch on and off. Every light switch below 15 amps will have a little bit of cadmium in it. You need a little bit of cadmium oxide with the silver. You have silver contacts because you'll get an electric arc, and if you don't have cadmium, just plain silver contacts are good for about seven amps. If you put a tenth of a percent cadmium oxide in there, you can get 15 amps. Then you can break a circuit at 15 amps without creating an arc — it will suppress the arc.
In Sweden, back in the 1970s or 80s, they're very environmentally conscious, and they decided to outlaw cadmium in the environment. The Scandinavians also wanted to outlaw chlorine in the environment. I don't know how you do that when you're surrounded by ocean. But they decided to outlaw cadmium, and they took the cadmium oxide out of their electrical switches. Within three years, they decided they would rather have cadmium oxide in their electrical switches than have people's houses burn down. They were burning down houses left and right.
Sometimes the whole system is fairly complex. There are gold brazes, the gold-18 nickel, gold-copper, a gold-silver-copper. There are lots of other brazes — copper brazes, nickel brazes. We've talked about the boron and phosphorus brazes, manganese and palladium. This is one that doesn't erode things, so when they replace some of this stuff to make those seals for the jet engines, they were probably working initially on nickel-manganese-palladium. With palladium alloys, you're getting up to 1200 C. These are brazes that are close to the melting point of steel. So you can get some pretty high-temperature brazes.
§10. Solder versus braze terminology, lead and cadmium today [44:38]
On silver solder versus silver brazing — when you're soldering, it used to be lead-tin solders until 1978, when Massachusetts outlawed lead in plumbing. Now it's typically tin-antimony with maybe a little silver for strengthening — five percent silver or three percent silver, tin-antimony.
Student: Is silver solder a solder or a braze?
Silver solder is actually a braze — that's what I just put up. And that's a misnomer. It really is a silver braze. If Handy & Harman still existed — they were the leaders in silver brazes — they would call them silver brazes, not silver solder. Silver solder is just a generic slang term. They are silver brazes, not solders. Soldering copper pipes is usually done at lower, soldering temperatures. There are cases in copper heat exchangers, or boilers, where you might get higher temperatures and you don't want the creep problems of the lower-temperature solders, so you'll use silver brazes.
Most places have outlawed cadmium in the brazes. There are still some cadmium brazes, just like there's still lead-tin — those little solder bumps on the semiconductor chips, most of them are still lead-tin. I showed you how you don't need much superheat with lead or lead-tin alloys to get them to flow well. There's so little lead in that semiconductor package. And if you want to talk about toxic metals in a semiconductor package, what do you think gallium and arsenic are? The whole thing is toxic. So who cares about a little bit of lead? Because lead-tin has such great soldering characteristics, they still use it in that microscopic amount in those solder bumps. You can still buy cadmium-based brazed alloys, but they'll have all kinds of toxic labels on them. You really should have ventilation or do it in a hood, even if you're torch brazing, because you don't want to be breathing cadmium vapors. Just like lead vapors.
When I was a student and you broke a mercury thermometer in the lab, you'd just go get some sulfur and sprinkle it on the floor to make mercury sulfide to tie it up. Or you just swept it into the corner and let it vaporize into the room for the next six months. I'm not kidding. Nowadays you've got to call out the EPA, and they're going to come in with their hazmat suits, cordon off the whole room, declare it a disaster area for the next six months while they vacuum it out for only half a million dollars. I'm not kidding.
§11. Hot shortness, aluminum filler selection, and class wrap [47:42]
Student: Are those alloys hot short?
They would be hot short if they weren't so thin. If you had a big bulk thing and it was solidifying in a thick joint, they'd be really hot short, because of the big freezing range. Phosphorus with copper, phosphorus with nickel, phosphorus-iron — give you big freezing ranges. Silicon with aluminum gives you a big freezing range. Those things cause hot shortness. Hot shortness comes from the big freezing range. Anything with a big freezing range is going to be hot short. Nickel-copper, that's your prototype hot short range. That phase diagram happens to be isomorphous. That's not hot short, that's not hot short, but everything in between, big freezing range, hot short.
Hot short means as it's solidifying and shrinking, it will just rip itself apart under its own thermal contraction. If delta T is large, lots of strain. If delta T is small, not so much strain, not so much strength.
Student: What about welding aluminum?
When you're arc welding aluminum, depending on your alloy: if it's heavily alloyed, you use a heavily alloyed filler. You don't mix low-alloy and high-alloy to end up with something in the weld metal that's the worst of all worlds. If it's low alloy, like nearly pure aluminum, use a very low-alloy filler metal. You have to worry about that with aluminum. You don't have to worry about it with steel, but with aluminum you do. These are the types of questions you should have been asking.
So, class next Tuesday. Enjoy the snow tomorrow. I would have lectured a little bit tomorrow, but I decided — I don't know what it's going to be like.