Two Laminate Samples, One “Core” Lesson

Part of the idea with the Laminate Samples is to show how materials and processes work – but there’s another part: showing how to mess stuff up! I have been building in (mostly intentionally but sometimes not) mistakes and demonstrations of common problems that are easy to have. From vacuum bags that are too small, race-tracked infusions and pinholey surfaces, there are plenty of mistakes to make even on a flat panel. Most are pretty obvious once you see them so I’m making sure to show as many as I can without making the samples themselves totally useless.

The Core Concept – Bleed Holes!

This post is about two samples: #18 and #24. They share the same core (1/8″ / 3mm Divinycell H80) and both use 200g / 6oz skins laminated with epoxy and vacuum bagged. One is e-glass so you can see through it. The other is spread-tow carbon, and you can’t see through it but you can see the big mistake!

The main idea here is that when you’re vacuum bagging foam (or balsa) cored parts, you need a way for the air and excess resin on the mold side of the panel (the first skin) to get out. This is why core needs to have either holes or slices with a scrim. Both ways allow air and resin to escape. In #18, I drilled a bunch of holes on 50mm / 2″ centers to let that happen and it came out great. On #24 I didn’t – and the bottom skin was full of too much resin, trapped air, nasty surface defects and at least one fairly large non-bond / void area. Ouch! And I had to go and do it with that pretty expensive spread tow… but it makes for a better lesson that way.

Look at that mess – the excess resin and trapped air forces too much thickness in the bottom skin. When I tap this area it sounds hollow like there’s a huge air bubble between the carbon and the foam – because there is!

The Videos

The good one…

…and the bad one:

Pre-drilled Holes

Most foam core manufacturers sell foam with pre-drilled holes. This is great because it saves a ton of time – drilling thousands of little holes is no fun. Usually the holes are the right size for infusion, where the holes allow resin to get to the bottom skin. They’re also fine for bagged wet layup, where they let air and excess resin out. For pre-preg, you may be able to get away with smaller holes.

Hole Spacing and Layout

The ideal size is about 1mm / 0.04″ for bagged wet layup. If you have good control of your resin wet-out ratio this will be fine. If you just pile the resin on there like I did in #24 – you’ll need bigger (or more) holes. Thicker core or core bedded down with thicker filled resin will need larger holes too. The weight penalty for larger holes decreases if you are using a core bedding mix that has a low density filler.

Hole spacing depends on the core thickness, bedding material and how much you expect to bleed off the bottom skin. I’d suggest keeping it closer then 100mm / 4″ so that there is never more than 50mm-ish of distance for air to travel. For filled core bonding resin, go closer. Really, unless you have tested it – 50mm / 2″ spacing is ideal. If you are building big stuff you should totally test it!

I also suggest sticking to a regular pattern. It is appealing to just blast them all random and assume that averages will work out in your favor. The big problem is making sure you don’t leave “islands.” Draw a grid and be systematic. If you have many sheets to do, stacking them and using a pattern and a long bit can speed the work.

Vacuum Level

And about vacuum level and pressure – you can bleed off too much resin if you really hammer on the vacuum. For stuff like this, 15inHg / 500mbar or so is fine. I have seen people use much less for bagging wet laminates and things come out fine! Check out what happens when you really crank up the vacuum in Laminate Sample #5: Vacuum Bagged Wet-layup Carbon/E-Glass with Foam Core. That carbon really shows how resin starved the e-glass is. Its easy to think things are great with carbon but fiberglass telly you what you’re really getting in there!

Note: If you are thermoforming your core, you should get un-perforated core and then drill the holes after you form and slump the core. They close up when you bend the panels and redrilling thousands of holes is bad news.

I hope that helps explain the importance of perforating core with bagged wet layup. Nothing like seeing it on video!

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Foil With Shear Web: A Very Old Test!

I was cleaning out a toolbox and found this off-cut from an old test – from maybe 2008 or so. This was when I first had a CNC router and was working on making small daggerboards for a sailboat. This was a test of a one-cook section of foil – maybe 250mm front to back and 25mm thick. The test was only 300mm long and I have no idea where the rest went – but this small section survives.

short section of a prepreg carbon foil test with a foam shear web

After some consideration I ended up doing the parts a different way, but I went back and searched through my photos and found that I had carefully (for me) documented the layup and bagging process. The bagging is a neat example of using internal and external vacuum bags – in this case tube-bag. You can see the wavy fiber in the close-ups of the part which would have been prevented by pre-curing the skins of each half – but this was an attempt to mold and cure the whole thing at once.

Certainly not an ideal outcome, but pretty interesting to see the way the fiber behaved – and a good way to illustrate the inside/outside bagging method and tying two halves of a part together with +/-45 degree strips of pre-preg. This was before I had an autoclave – but it would be neat to test this concept again with more pressure!

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Bag stack resin absorption – a data point!

So I was working on a video about really basic pre-preg – and making Laminates Sample #2 and #4 at the same time. Because my basement is not a fussy place, I used dry peel ply (crinkly nasty old dry peel ply actually) as the first layer of my consumable stack of sample #2. I removed the peel ply from the already-trimmed (1’x1′) panel and weighed it because I was curious. Then I carefully cut a one square foot dry sample of the same plain nylon peel ply – with the red stripes. I think this is Airtech, but I’m not 100% sure.

The dry sample weighed 10g and the sample that absorbed resin weighed 13g. So: 3g or resin per square foot, about 11 square feet (10.764 you nerds) per square meter. 3 x 11 =33. Now I don’t know if that three on the scale is 2.51g or 3.49g… but it’s a range. (I went back and weighed it again later – see below – and the absorbed resin weighed 5g – probably need to look into that scale!) This means that this peel ply absorbs 30-50g of (this) resin per square meter.

dry peel ply resin absorption rate prepreg

This makes sense if the peel ply is 100-120g per square meter, a 35% resin ratio would be 35-40 extra grams. My mental go-to estimate is 50g per square meter (don’t remember where it came from!) – so it’s nice I’m in a reasonable place given these observations and my questionable measurements. Maybe I’ll try some larger samples and other resins to see if we can science this up a bit!

So if your pre-preg laminate can afford 35g-50g of resin per square meter – go ahead and forget that pre-preg peel ply. And the resin you bleed off – well that’s up to you. But if you use perforated release film (and out of an autoclave, you should) it’ll be something!

Now on to breather. In Laminate Sample #4 – a 3mm QI prepreg panel, I had 4oz breather that was nearly fully saturated. I weighed a square foot of this and at the same time re-weighed the peel ply sample from above. I’m not sure why it (or if it actually!) got heavier, but here’s the new resin estimate for the peel ply (left) and the resin uptake estimate for the breather (right):

Yikes! The breather soaked up 333 grams per square meter of resin. It may have been slightly less, again with the scale giving non-repeatable measurements. But still, that’s a lot! This laminate had a total of 1783g of resin per square meter. The bleed from peel ply and breather was about 375g. That’s about 20% of the resin available in the laminate. The calculated resin ration went from 37% to 32%. I will measure the thickness and weight of the panel when I get it trimmed up and report back.

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Cored Pre-preg Parts in One Cook

This post is about a technique that lets you speed up the construction of basic cored pre-preg parts by potting the core edges in thickened epoxy. While not the best idea for highly loaded or critical parts, it does let you cut one of the big corners that makes pre-preg parts expensive and time consuming – the price for this – thickened epoxy!

The key idea here is that the whole part gets cooked at once, but only after the core “chocking” material (ideally epoxy that needs post-curing filled with low density filler) had b-staged and is hard to the touch. You are using the cast-in-place core to apply pressure to the outside skin, so it will never be as good as a multiple cook part – but it sure is faster and primary bonds are nice too.

First Example: A Cored “Sawhorse”

Here’s an example of a test part I made a long time ago. It was a prototype bench for tuning snowboards and I wanted to core the top but also wanted it to be as quick and cheap to build as possible. Weight was important but not critical. This is what the core fit looked like before the second skin went on:

Nomex honeycomb potted around the edges with thickened epoxy so the part is cured in one cook.

The skin in the mold is not cured – it is just debulked in there well and glue film is debulked into the outside skin under where the core will go. Glue film is just pre-preg resin in a sheet – it is added when bonding core so there is some resin to soak into the core material and form a nice bond.

The honeycomb core was loosely fit and then I mixed up a batch of slow epoxy and thickened it with glass microspheres and about 10%-20% silica. Ideally you could use a resin system that requires a post cure so that there would be some primary bonding going on with the pre-preg – so they would co-cure. This isn’t necessary though – you just want to use a system that doesn’t produce amine blush. The filled resin was squirted into the radii under the core with a cake bag – you could do with a fillet stick too but it would be messier. Then I pushed the core (the corners had been radiused so it didn’t hang up in the corners) down into the fill and it shot up into the honeycomb cells. Then I used the cake bag again to squirt thickened epoxy around the edges to make a fillet. I used a lot!

Once the core was manually pressed in and the fillets were cut neatly, I placed a piece of peel ply (bias-cut no doubt!) then perforated release film and breather and bagged the core in using my debulk bag. This left the nice radii of cured filled resin, ready for the second skin. You can see the peel ply surface on the above picture – that’s why the uncured pre-preg doesn’t look shiny.

carbon sawhorse for tuning snowboards made in one cook with Nomex core - and cool aluminum leg inserts.

Here is the second skin laminate before cooking. The aluminum leg socket formers/mandrels were part of the experiment – they were wrapped in pre-preg material and bedded into the uncured outer skin before the inner skin was laminated over them. Worked pretty well! The part on the right shows the cured and trimmed part – the core didn’t print or leave any voids on the mold surface because it was essentially “potted” in place against the debulked skin.

Second Example: Foam Cored Stairs for a Yacht

SAN (Corecell) foam is carefully fit before the part is laid-up.  Once the first skin is debulked and film adhesive is applied...

Here is a more complicated cored part with Corecell foam core instead of honeycomb. One the left it the core fitting stage, which was done before the skins were laminated in the mold. The idea was that the skin thickness (about 0.04″/1mm) would offset the foam uniformly and that if the joints were loose, there would be room for the filled resin to pot the foam against the debulked inner skin. Here the inside and outside radii as well as the perimeter flange made fitting carefully a necessity. One the right – the pre-preg glue film is debulked onto the outer uncured skin.

the foam is potted down in thickened epoxy and then vacuum bagged (gently) so that the wet-filler is compressed and perfectly fit against the pre-debulked skin.

Here is the step where the core is pressed into the wet filled resin so that it forms a chock-fit – essentially a cast-in-place addition to the foam. One the perimeter of the steps there is a rebate for secondary bonding and this is why there is a wide skim of filled resin around the edge. During the cook, the foam will soften and “thermoform” over any excess glue – which won’t be a big deal because we are going to vacuum bag the foam down with the debulk bag as soon as it is all fit.

more filled epoxy applied to the uncured pre-preg to fill all the small gaps between the foam and the skin.

Above is a closer look at the process. This would probably get you taken aside for a stern talking-to at Boeing or SpaceX but in this case it saves time and makes a good solid part with only a small weight penalty. The core is all perforated to bleed air and resin when it is cooked – and the excess adhesive mix bleeds out and into the bag stack while the core itself is bagged. So a good deal of this white filled material will never make it into the final part. Here is the core the next day after the bag, peel ply, perforated film and breather was removed:

after the wet-epoxy has gelled, the excess is cleaned up.

We went around and detailed the radii by either scraping away high spots or filling carefully with more filled epoxy. The foam here is neatly potted into the outside skin all around and all the pre-preg will get cooked in one final cook at the end. Next we started laminating the second skin. The first layer of the second skin was “combo-laminated” with glue film on a debulking table so that we didn’t have to handle glue-film and then place pre-preg plies onto the film itself – a surefire mess! After cooking, the part was demolded and looked like this:

Finished prepreg carbon stairs for a large yacht with taping rebates around the perimeter and a bonding flange to meet the finished hull.  Once cook!

It came out great! There were no voids or nasty radii and the rebate are around the edge was tight. This would have been even easier with honeycomb core but it works ok with foam – you just have the make sure the core fits loose and there’s room for the excess filled resin to squeeze out. There’s not a ton of detail here but it should help you if you have never used this method before. If you have any questions, just ask!

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