Hi Guys,
Some time ago I started a post with some ideas about making a UAV using rapid prototyping to construct the wings and fuselage......I suppose my initial idea came from a thought that it would be great to create an airframe that has been designed from the outset as a UAV and with my experience of RP I know how simple it is to make complicated thin wall shapes with these machines. Currently you either have to make a UAV like from an RC kit or go down the route of using expensive composites with all the attendant tooling and production costs. I wondered if it was possible to design something that could be printed off from an RP machine have a minimum ammount of prep work done to it and then asembled and flown......

Is the future of commercial UAVs acceptance going to be limited by the current construction methods? if you can print off a UAV like you do a sales brochure the problems of crashing and damaging airframes becomes less of an issue, got a hazardous mission? send in the UAV, if it never comes back we can just print another......Henry Ford said " If I asked my customers what they wanted they would of asked for a faster horse!"

I have attached a pic of one of my concepts that shows an idea of what I am attempting to do. The idea is to print off the wing and then stiffen it up with a bonded on carbon fibre spar. The CAD concept shown is 33" long, 7.75" wide it is made from 1mm thick polycarbonate and weighs 500grams can anyone tell me how far off being an acceptable weight this is? The carbon fibre spar would fit into a carbon fibre box section bonded into the fuselage. The fuselage would be made using the same process as the wing.

My next job is to try and optimise the concept using cosmos to see if it can sustain +/- 6G with carbon spar fitted in the wing and to see if I can loose some weight anywhere. Let me know what you think!



Regards




Oliver

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Looks good. Just a FYI--it's more effective if you embed images in your post, rather than attaching them, to save people from having to click. Use the little camera icon.
Nice drawing! What software did you use?
Manufacturing of CNC components you speak of could be achieved within DIY drones community: Differences in foreign exchange rates could make it cheaper for some members.
I use CAD (Microstation) every day, as an Architect, and don't have first-hand knowledge with CNC technology (although we've recently used it to model parts of a project I'm working on).
I'm aware .dwg format is the international standard for Architecture & Engineering, but can anyone tell me if there is an "international" file format for CNC tech?
Hi Nigel thanks for the response. I used solidworks for the CAD modelling. The manufacturing process would be an aditive one rather then CNC. The advantage of this is that you can make the wing in one piece with all the internal features you need in one operation.

The largest machines can currently make wing sizes 900mm long by 800mm wide. The material I have selected is a polycarbonate, ideal for high impact applications, crucially none of the currently available materials have the required strength/stiffness so they would need some kind of carbon fibre spar to give them the required strength.

The CAD model I have shown doesn't really take advantage of some of the unique properties of this manufacturing process so the next concept will have a skinned honeycombe structure and a central spar box.



Regards





Oliver
Hi Oliver

First, I really like your idea for using RP to manufacture planes. My primary concern with the idea is the surface finish that your wing will have. How much sanding (if any) is involved in finishing these parts?

Are the ribs you have in your CAD model going to be made from polycarbonate also? I would think one way to reduce weight would be to create the ribs out of something lighter, like balsa, rather than the polycarbonate. What's the density of the material you're planning to use? That will help determine whether it's worth making it all out of polycarbonate or making the ribs out of something else.

As for your 500 gram weight, that sound a bit high. There is no easy answer though, it all depends on how much payload you need the plane to carry. You might be able to get away with this weight, but you wont be able to carry as much in electronics. The airfoil you choose will also impact whether or not this weight is acceptable. What have you chosen?

Anyway, it's an interesting project. Please keep updating on how it's going.
Hi Jordan

The finish you get from the RP process would require a paint finish to make it smooth and possibly to seal the surface, the additive manufacturing process gives a stepped finish usually in 0.010 slices. (Could this be a useful aerodynamic feature like the corrugated wings on a Junkers?).

The build process of the RP machine doesnt really allow us to use seperate materials, the idea is to build all the structure in one go. However one idea I came up with was bonding a box section wing spar to seperately built leading and trailing edges. My aim has always been to try and build a wing which has simplicity and ease of build as the main criteria rather then ultimate performance.

I understand what you say about the density of the material (polycarbonate 1.2 grams/cubic centimetre versus balsa 0.155 grams/cubic centimetre) but the tensile strength of the Polycarb is between 5 and 9 times stronger depending on the fillers used in the plastic.

The wing profile I have used is an E205 Naca form, I am sure its not ideal for what I want but it was a convenient place to start. I started out just looking at the feasibility of using this manufacturing process on a conventional wing, I am wondering if it works better on larger scale wings as the material weight is less critical.

Regards





Oliver
No one uses RP for production due to the costs. A wire-cut styrofoam wing is far more cost effective and broadly attainable.

RP is really only cost effective when the parts being produced are expected to change significantly on a daily basis.

I believe Boeing already made and flew a fully RP drone, not sure if a market emerged.
Hi there thanks for your reply,


RP has moved on from one off parts to "digital production" which is seen by industry pundits as the big growth area for the future.......see this link for a company offering (low volume) production parts: http://eu.redeyeondemand.com

I'd love to get any information on the Boeing drone you mentioned, RP can be a bit of a misnomer as its a generic term and is sometimes used to describe anything from high speed CNC machines, additive fabrication ( what I'm talking about) and just doing things quicker!

Just to make a point about how the cost of RP will continue to become cheaper, the cheapest machine available now is just £ 750 .....http://www.bitsfrombytes.com

I understand what you say about the wire cut foam foam, I am really exploring the concept of what may be possible in the future, perhaps looking for a method of production that doesn't need the kind of model making skills found in the RC community. My concept is design, print, fly or perhaps download files, print, fly.


Regards



Oliver
The reason I asked about making the ribs out of another material is because they don't need the higher strength that the polycarbonate provides. One way to reduce weight would then be to make the top and bottom half of the plane shell as two separate pieces and place balsa ribs in between the halves before gluing it all together.

It sounds like that defeats your purpose though. If you would rather be able to print the plane as one complete piece, you're going to have to add some weight. With the right wing design, this shouldn't be a problem. I have a plane that I've designed and am currently building which could accommodate this additional weight without much trouble.
Hi Jordan,

What kind of plane have you designed? did you do it on cad or do you have drawings for it?


Regards


Oliver
Have you attenpted to print a single section rib to rib? It seems to me that the wing covering (skin) would be difficult to print since it is not supported in the middle.
Hi Ken,

I have spent some time looking at this. The best ( I think at the moment with what I know!) way to build an exterior wing profile is to build it vertically rather then to lie it down. This is because all the additive RP processes slice up the cad file to create 2 d slices which are then built layer by layer on top of each other until the part is finished. If you lie the wing down horizontally the slices run through the wing giving you pronounces stair-casing on the part. Most RP processes use support structures to hold the part in place, I think your assumption is correct in that building 2 seperate parts could prove difficult if they warp during the build especially if your part transitions from thick to thin sections.

When I have built large RP parts in the past I have added dowel or step features on the cad model to help align the part and make it easier to join parts.

If you are trying to build the "core" of a wing (I think!) the above does not apply because any surface stepping should be lost when the surface skin is applied, ie if you covered it in fibreglass or CF.....Although I have to say I havent tried this yet!


Regards






Oliver
What if you printed just the ribs, essentially everything in your picture above except the skin, then had an easy covering method like a shrink wrap bag of some sort...it may not be as quick, but it could be lighter. Additionally, if you were going to go that route you could make all of the ribs thinner and maybe even go to something like a thin walled honeycomb internally - significant strength, less material. Just some thoughts.

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