§1. FAA certification and who takes the heat [00:02]
That long discussion still applies to additive manufacturing parts. Unless Boeing is certifying them — which in this case with Digital Alloys, Boeing is going to certify the parts under the STC, the supplemental type certificate that they hold. If Boeing certifies to the FAA that these titanium additive manufacturing parts are good, the FAA is going to say fine, you're responsible, you're taking the risk. If the plane comes down because of it, you're going to take the heat. And guess what's happening on the 737 Max? The FAA is not taking the heat — well, they've taken a little heat, but mostly it's Boeing, right, because they approved it.
But you can get around the manufacturer through the PMA process. You can either design a brand new aircraft component yourself and have the FAA approve it, or you can prove equivalency to the design standards. But the FAA cannot release what the design standards are to you. They have them, but it's proprietary information. Boeing gave them that information; they can't release it. If you supply information — a sack of documents like this — they can say yes, this meets the same criteria Boeing gave us, or no it doesn't. But it's not as if you can go through and ask what doesn't it meet. They don't have to tell you; they can't tell you that because they'd be violating the confidentiality. So it's a sort of cat-and-mouse game.
Student: [question about FAA equivalency processes]
In the FAA, most of the equivalencies work very closely with the FAA. The European Union of course has Airbus, and their lab will give Airbus a little benefit of the doubt, like we'll give Boeing a little bit of benefit of the doubt. But if you go to South America, they have their aviation authorities, and when they have a problem, it's not that they're not independent, but they're going to go ask the FAA what they think. And the FAA will send people in to do part of the accident investigation, because they want to know what happened. They're charged with promoting safety. When the 737 Max went down in Indonesia, and the other one in Ethiopia, there are FAA Americans on site. They were probably the ones who came back and merged the data from the Indonesian or Ethiopian investigation. We probably have more expertise in our FAA than Ethiopia or Indonesia. So they actually work very closely. They have to, because none of them have enough staff to do it all.
And they rely a great deal on the manufacturers. When there's a failure, you'll hear that the National Transportation Safety Board went in there the next day. Pipeline explosion, NTSB is there. A ferry sinks, NTSB is there. A railroad derailment, anything where there's transportation involved, we have a National Transportation Safety Board. They're charged with going in and doing the investigation. They don't have all the expertise to do that. They will invite in people from the railroads or the manufacturer of the railroad equipment, and they'll ask them questions, and they have subpoena power. If you don't answer the questions, they'll get it. They'll go to the judge and they'll force you to give it. So there's sort of a cooperative mode here. Is it completely cooperative? No. The companies aren't going to say oh well we screwed up. But these guys, the US engineers at NTSB, are not all stupid.
And now we have a Chemical Safety Board, modeled after the NTSB. NTSB's been around for fifty years. There's a big explosion in a chemical plant in Texas, CSB's in there. Big hundred-page reports on why it happened. It's sort of like ocean investigations of an industrial accident. Sometimes they're pretty good and sometimes they're pretty bad. It just depends on the quality of the government investigator writing the report.
I actually think learning about these investigations and how it really works is interesting. It's not as scientific and technical, it's more political. But it's real.
§2. Digital Alloys: buy-to-fly and the time savings argument [05:04]
I passed the sign-in sheets. Most of you have attended enough classes that's not going to be an issue. This is from the Digital Alloys blog site. They've actually taken a Boeing part, and Boeing has done this analysis. If this is to make a five kilogram titanium part — remember buy-to-fly ratio — five kilograms is probably going to fit within the size of a soccer ball. And making a hundred parts, not just one part. You're not making one-of-a-kind unless you're a spacecraft.
For additive versus machining: yeah, you can set up your CNC machine to do this, and this is just to do rough machining — forty days. Remember you're going to machine away probably ninety or ninety-five percent of the five kilogram, so you're going to make 500 kilograms of parts, but you multiply that by twenty, you've got 10,000 kilograms. You've got a lot of titanium chips at the end, and it takes many days to do that. This is for Joule printing, but if you could do it by binder burnout or something else, you would also get something similar — seventeen days. Forty days versus seventeen days. When you start doing the math on all that on the cost, you're going to find that the heat, the energy in CNC machining for a single part, is not very much energy. I don't think the energy thing is all that interesting.
The real thing here is the time savings. You're going to find that additive manufacturing of these parts is a lot cheaper than manufacturing the old-fashioned way, where they just hog out of a big hunk of titanium and make a little bitty part. Remember the Aladdin movie — great tremendous power, little bitty house to live in for Aladdin. You have to have brackets, maybe.
§3. Process taxonomy: powder bed, directed energy, and part size [07:56]
Part eight is about powder bed fusion, which is something like laying down a layer of powder and coming along with a laser, electron beam or an arc. Now we get part size. Their process will do things as big as the soccer ball, which is your five kilogram part. Some of these things like binder jetting, where you actually squirt powders and fuse them together and build something up, you can make a golf ball or a tennis ball. If you want to make something substantial in size, a meter, you're going to have to be into directed-energy deposition.
Here's an example from the General Electric area, an aerospace fuel nozzle, very complex part. It's a structural material but it's a functional material. Remember I told you the other day, when you're doing pixel-by-pixel, you've got to have a functional advantage. Just tensile strength, yield strength and elongation are not going to cut it. You can usually make those things other ways. But when you need all these little holes and bosses and things, previously made from twenty different parts, there's a tremendous cost savings.
If you go to directed-energy deposition, there's powder and wire deposition. My technical community where I got my tenure was welding. This is the types of stuff that I would do research on and look at heat transfer and whatnot. You basically have a wire, you're feeding in like a welding wire, you've got an arc — this is a gas tungsten arc — and you put down a little drop, some metal about the size of a weld pool. So you can make something a meter in diameter if you keep going. This is laser, on their blog. You've got a laser, you're feeding powders in, and you're making a cylinder out of powders. The wire EDM was slowed down, but for real speed, this is probably about real speed.
Now what do you get if you look at deposition width in millimeters versus print speed in kilograms per hour? If you have nice small pixels less than a millimeter in size, you're not going to put down a lot of kilograms an hour — in fact you're going to be talking ounces per hour. If you have some big weld pool and you're going to be making something the size of a meter, yeah, you've got ten kilograms an hour. And you know what, that's about the fastest any welder can weld. If you go through and figure out the economics of a welder, you look at how many pounds per hour or kilograms per hour a welder can put down. It's a few for gas tungsten arc, around seven pounds an hour is a max. Look at other processes, you might get fifteen or twenty pounds an hour. It's not any faster than just laying it up as weld beads, and we've been doing that — additive manufacturing — for years.
§4. Turbine blade tip repair: fifty years of additive manufacturing [11:44]
In fact that's why I brought this, and that's why I drew this picture. [Tom indicates a turbine engine diagram and a shroud piece.] It's a turbine engine. You've got a center shaft, you've got some compressor blades, and you've got some combustors where you add the fuel and the compressed air. Then those go past the turbine blades. Those turbine blades spin this whole thing. As they spin this whole thing, the compressor blades compress the air by about a factor of thirty in volume, but it's going up in temperature, so you get to like thousand psi pressures. But you've got a problem. You don't want any blowback. When you've got high pressure here and atmospheric pressure out here, if you don't have a good seal between the shroud and the blade, you're going to be losing efficiency as the air goes the other way.
So what do they do? The first thing we do is we make a honeycomb. [Tom holds up a piece of shroud.] This is a shroud, actually a piece of a real shroud that had been in service. This is not the blade with it, but the blade's going to be spinning at twelve thousand, twenty thousand rpm — pretty fast. And it's going to be going past this thing. We make it a nice soft compliant honeycomb structure that will wear away as the blade creeps. It's working at higher temperatures and it gets longer over time — over thirty thousand hours of operation it gets longer. As it gets longer it just cuts into the shroud and it keeps a good seal.
These tips wear out and we want to recondition these blades. Not this one, but some of the fancier blades could cost two or three thousand dollars apiece. So we go along with these little directed energy deposition processes. We never called it that before — the advanced additive manufacturing — they actually called it laser welding. The Air Force went to Tulsa, Oklahoma, maybe Oklahoma City — they have a big repair facility for their engines — and they would put on little carbide composite coatings on the tip so that it intentionally cuts into the surface as it's spinning at high speed. We've been doing that for fifty years. That's additive manufacturing, folks. It's done on the original parts, it's done on the repair parts. We do all kinds of additive manufacturing because we're saving a two thousand dollar blade and letting it go for another thirty thousand hours. There's a lot of value in that. So that's another place of additive manufacturing — repair and maintenance.
§5. Binder jetting shrinkage and surface roughness [14:43]
Then they go through binder jetting. This came up the other day — how big are these parts and do they shrink. If you start out with a powder compact that's fifty percent voids, when you just glue powders together, once you heat it and sinter it, something this diameter shrinks down to this. These are not huge parts, but this is a compressor blade or vane. It really doesn't have great geometry control. I mean it looks good, but balancing this — because it's going to spin at 30,000 rpm — for something that diameter it's got to be balanced, folks, it's not going to be easy. Typically we cast these things; we don't do it by additive manufacturing. This I think is a demo. I'd be surprised if that's in production.
The last thing Alex put together is surface roughness. All kinds of different surface roughnesses. This is wire directed energy deposition — just a bunch of overlapping weld beads. This is the Joule printing, which is pretty rough — you've seen that, pass it around. Binder jetting can be pretty fine. Powder bed, which is sort of like the Desktop Metals, is a lot better than Joule printing. He's got another graph that I haven't really studied, but basically it shows that the surface roughness in microns goes from a hundred microns for that weld bead down to five microns or less for the different processes. So different attributes for different processes. Here's an example he had in there — I think it's probably titanium, it could be stainless steel — a part done by a directed energy deposition process on a plate. The plate actually becomes part of the final machined part. There's lots of machining, but it cuts down your machining.
§6. Sintering shrinkage as an aerospace dealbreaker [17:20]
Student: [question about shrinkage from sintering]
Yep, from the sintering process. It's one of my problems with the sintering process. If I come to the conclusion that aerospace manufacturing is a sweet spot and I need ultra precision for the aerospace market, I don't think the powder shrink as a sintering process is any good for that. They think they're heading towards the automotive market — I think they're kidding themselves. But maybe they're going to have an IPO and they're going to be faculty members of this department walking away with five or ten million dollars in their pocket. I don't have that, so maybe they're not smarter than I am. But your grandmothers are going to end up with a lot less in their pension fund ten years from now. Because someone's going to take and buy some of that IPO, put it in the pension, and over time you're going to see it just drop down, in my opinion. That's my opinion, just an opinion.
But you can make your own choice right now. You now know enough. We spent six hours talking about additive manufacturing — actually not even that, because of tangents. Whether it's additive manufacturing of metals, or whether it's high-temperature superconductors, you're MIT students, you should be able to study the technology on your own for two hours and know more about it than the person who wrote the article in the Wall Street Journal that says it's a wonderful thing, new technology. I guarantee you, two hours of intense study. I would have loved to have given you papers to write where you could take a topic, but I found it's easier just to let you pick a topic that you like and you'll study it. You become an expert with two hours on a topic you're interested in.
If your grandfather left you $100,000 to invest in some new startup at MIT, hopefully you wouldn't just go to the first one walking down the infinite corridor, right? You're going to do some study, and hopefully you'll spend two hours studying the technology, maybe rejecting it. Then you've got to go study another one — two hours. In the end maybe you'll spend ten hours to select one out of five. But you ought to be able in two hours to learn quite a bit and do critical thinking, if you know some of the principles.
§7. The cost of a pound saved: aerospace, Mars, and potato chips [20:07]
One of the principles I taught you in the beginning: the value of a pound saved in an automobile is $2 over the life of the vehicle. In aerospace it's $200. As I always say, they have vice presidents at American Airlines figuring out how many magazines they're going to put on that aircraft, because magazines are heavy. At $200 a pound just to carry around something people aren't going to read, that's a lot of money. And our space technology — Elon Musk, he wants to die on Mars. "Do I want to do it on landing," that's one of his quotes. I think we should send him to Mars. I won't say any more.
First of all, it's a one-year trip one way. And the $20,000 — the people who are going to colonize the moon, let's not go to Mars, they're going to colonize the moon at twenty thousand dollars a pound. The original Space Shuttle was supposed to reduce the price of a pound in orbit — that was in 1970 dollars — from $10,000 a pound to $1,000 a pound. Let's say we can do it for a thousand dollars a pound. SpaceX or whatever is going to get payload in orbit for a thousand dollars a pound. You know what it's going to cost for me to buy a ticket? I would be incentivized to lose some weight. A thousand a pound.
Once you get to the moon, you might need some other things there to live off of, right? Which is why NASA is looking at, well, can we dig up moon rocks and process them to make ore, in order to make metals. And where are we going to get the energy out there? We've got solar energy, yeah, okay fine. You start looking at all the things you have to do. You were at NASA Langley, and they've got hundreds of people looking at how they're going to do this. How they're going to weld things in space, how they're going to process things in space, how they're going to repair things.
I was at an alumni thing in Philadelphia once, about twenty-five years ago. We had a young faculty member — she's not so young anymore, she's close to tenure now, very distinguished career. She was talking about the mission to Mars. She was saying, we can afford this — we spend as much money on potato chips each year as we do on a program of about two to three billion dollars a year, she was claiming, to go to Mars over the next twenty years. Forty billion dollars. First of all I don't think it'll be two billion a year, I think it would be twenty billion a year — four hundred billion. But let's take her two billion. I leaned over to the person next to me, I said, if you did a poll of all the people in America, would they be willing to give up their potato chips for a trip to Mars? I think I know how that vote would come out. I think it comes out every day in the grocery store.
There's a lot of other things we need in this country that we could spend 400 billion dollars on, in my opinion, for a social good, than to send Elon Musk to Mars. I'm sure he's enjoying it and he could pay for it. I have my opinions about some of these things — I just gored an ox. They probably could defend themselves and talk about why it's useful. You can look back at putting a man on the moon — that brought us gallium arsenide, which is one of the great materials advances, I admit that, in LEDs and all those other things, GPS, and a lot of things come out of that. But you could also spend that money in other ways and develop sustainable, environmentally friendly technologies. Maybe we would have had solar power thirty years ago if we had invested some money in solar power thirty years ago. There are lots of choices and they're often made for political reasons.
§8. Strategy assignment: schedule and the startup question [25:05]
Any questions? The next lecture, with Alex, next Thursday will be the sixth lecture. We're supposed to meet on Wednesday but I have to go to a trial in Houston, and I never know when I'll get off the stand. So let's cancel class next Wednesday, let's do Alex Hück step next Thursday. We have Jerry — put this on Stellar. If we need another class after that, we'll schedule a class in October. I'd rather do that than be sitting there on Tuesday evening trying to get the word to you that we do or don't have class on Wednesday. It's just easier. If I am here on Wednesday morning, well, I'll find something to do and you can find something to do on Wednesday morning.
What I'd like to do on Thursday with Alex is let you ask whatever questions, because he's live. He put these blogs together — I think they're excellent and balanced presentations of what the advantages are on different types of additive manufacturing. He is of course in the business and so he is promoting his, but a lot of his stuff came from real data. In this case you can see all the Boeing interest and you're getting Boeing's data on the parts.
I'd like you to think about: if you had an additive manufacturing idea and you were doing a startup, what would your strategy be? What industry would you go after? What material would you go after? Why did we not talk about aluminum? Because aluminum has an oxide and it's hard enough to weld. Try to take little particles of it and join them together is going to be extremely difficult. Titanium doesn't have a surface active oxide that's hard to get rid of, so titanium is nice. Stainless steel is not bad from that point of view. Why haven't we talked about copper alloys? You could do copper alloys or brasses, but what's the volume there? The volume is in steel. Or if you're going to aerospace, you're looking at aluminum or titanium. Or you might get out of metals and into composites. So you might talk about plastics additive manufacturing, which probably has a number of applications in the aerospace industry to make excellent composite structures. Or maybe you've got an even better idea, if you can figure out how to repair those composite structures, because that's one of the big Achilles heels for composites in aerospace. We can make them, but we sure don't know how to repair them very well, and they do get dinged up every now and then. Look at the Space Shuttle.
So I'd like you to think about — do some critical thinking, as if you were going to invest, or you have a startup: what types of materials, processes, industries would you go after? If you don't know where you're going, any road will take you there, and it probably won't be profitable. Any questions? So there's my soapbox.