Infusion-Test Panel and Fuselage

Ran across an interesting Youtube video demonstrating an epoxy resin infusion process on some test panels and fuselage.  It is interesting how everybody has their own terminology and technique for resin infusion.  There is definitely more than one way to get the job done.

They use an interesting layup, including lots of the Soric material.  I have used this before, and it is a good material to infuse with.  Made by a company called Lantor, it is a non-woven polyester material that acts as a core material.  It appears that the folks in the video are using the SF grade Soric, which comes in several thicknesses.

An advantage of using Soric as a core is that it flows resin very well for infusion.  It is easy to cut and handles well.

Disadvantages also abound.  One of them is the possibility of print-thru on the surface of the laminate.  Another is the negative effect on the structural properties of the laminate.  This non-woven material does not have much crush resistance such as a balsa or foam material.  A serious issue that I have found is the higher risk of delamination.  Like any core, this material works by separating the two skin layers to create a sort of “I beam” effect.  The problem is that this material is not inherently strong within itself.   Though it does become saturated with resin during a proper infusion, it is not nearly as strong as glass or carbon fiber reinforcement.

As the video demonstrates, a proper resin infusion can look easy.  With proper materials, practice, and knowledge it can be.

Panel Stiffness

Composites structures have requirements for stiffness to provide support and stability.  Tests can be completed to identify the stiffness of a given area on a composites structure, i.e. how much it will bend for a given force.

The required stiffness of a section of a composites part depends upon the overall design and service expectations.  Several factors, including the life expectancy of the object, the load rating of the composites surface, the inter-laminar bond strength, will help determine the threshold requirements.  Testing is very important to determine the life expectancy of the part and whether it meets the requirements of its’ job.

Panel stiffness can be modified to meet these requirements using two basic methods.  One way to increase the stiffness of an unsupported composites panel is to reduce the size of the panel through additional support structures.  The other way is to increase the panel thickness across the same area.  Choosing which method to use depends upon the engineering of the part and determining which method is acceptable with the surrounding part layout.  If there is room to add supports, this is likely a quick and easy option.  If there is room to increase the thickness, adding new or additional coring materials may be a simple solution.

Building a strong and stiff composites structure can be accomplished with the extremes of  building a robust “skeleton” with small open areas and a thin skin, or having a basic, limited “skeleton” with a heavy duty cored laminate that supports itself.

A combination of the two usually works out best.

Making Holes

If you are working with fiberglass parts, you may need to attach other parts, pieces, and features mechanically with fasteners.  Bolts and rivets are the most common mechanical fasteners used to accomplish this.

Composites with a nice, decorative gelcoat finish such as boats and RV’s require special care to make holes in them for placing bolts and rivets.  Disturbing the area around your hole in a gelcoated surface can lead to very expensive repairs by a fiberglass expert.

You can make holes yourself, but it requires extra care and attention.  I found a great Youtube video that demonstrates this from user CenturionCrew.

Of course the biggest mistake that can be made is improper placement of the hole.

Following the instructions in the video and drilling a nice slow speed hole is the best way to be successful.  He also mentions the caution that must be noted to stop the drill chuck from contacting the gelcoated surface.  One tip that I have is to place a small piece of rubber hose over the drill bit to contact the gelcoat before the drill chuck.

One other note with holes (all shapes and sizes) in cored composites fiberglass pieces.  If there is a layer of balsa or foam core in the cross section, extra precautions should be exercised.  One is to coat the inside surface of the hole with gelcoat, resin, or silicone to keep moisture and UV out of the core.

Another concern is compression of the core with mechanical fasteners.  Balsa and foam cores typically are low in density, and are not meant to be highly compressed.  If you are going to bolt something on, and it is going to be really tight, it is best to use a metal sleeve in the hole that is the same thickness of the fiberglass part.  Large washers or backer plates should also be used to distribute the load across a larger surface.

Vacuum Infusion Processing

Resin infusion processing offers several advantages over traditional open mold processing techniques. All of the reinforcements and core materials are placed in the mold without resin, so care can be taken for close fit and proper orientation. And it is a lot cleaner without the sticky resin. Resin waste is typically lower because all of the resin is added at once. VOC’s are reduced as well, and are only emitted from the open mixing containers. There is much less worker interface with messy and stick resin on people and tools so cleanup materials and personal protection equipment expenses are reduced. The laminate itself is typically more consolidated, uniform, and visually pleasing.

One of the considerations that needs to be taken into account is that the ratios are different and the glass and resin are more compacted by the process. Using the same layup schedule would result in a thinner laminate that is lighter weight and uses less resin. One drawback to this is that the cross sectional area is less, usually resulting in a loss of stiffness. This can be regained by increasing the core thickness to compensate for that loss and to restore overall panel thickness.

Infusion processing does require specialized equipment, consumables, and materials. The resins need to have much lower viscosity(flow like water). The core and glass need to have holes and channels for the resin to flow. A bag needs to be created to cover and seal off the laminate to the mold with out ANY air leaks. The mold needs to be able to be sealed to the bag and be airtight. A high vacuum needs to be able to be drawn on the bagged mold to move the resin. The vacuum pump or venturi needs to be able to achieve a minimum of 28 inches of mercury.

The basic process is that the mold is gelcoated abd skinned with a good, low-shrink resin and chopped strand mat. Then layers of dry glass are added. Coring is placed nice and tight and glued if needed. And the final layers of glass are placed. During the process, any gaps in coring or glass will “bridge” where the vacuum doesnt pull them down, and solid resin will fill them. So good fit is very important. The the bag is placed and sealed after auxililary runner strips are added and resin feed hoses are placed. The perimeter vacuum channel is plumbed to the vacuum pump.

Air is removed from the laminate for a good amount of time before the resin lines are opened up and resin flows into the part (do not forget to catalyze it). This is part of the art of flowing resin to fill the whole laminate with resin before an area gets cutoff from the vacuum or the resin begins to harden. There are some tricks and practice is key.

Resin is stopped just before fill and hopefully resin doesnt run into the vacuum line too far, but that is what resin traps are for. The vacuum is left running as the part hardens and gets to full cure in a couple of hours.