Table of Contents

Fiber Fuselage

After still having major problems with waterproof design, the idea is to start a new fuselage design from scratch in fiber composite technology. This promises the following advantages

The big drawback is missing experience with aircraft design and fiber technology. Further Component tests are here:

As description about the tooling is here:

Milling at Hochschule Augsburg

Strategy

Tooling

The Deskproto CAM software needs some RAM depending on the detail level. The Deskproto Software is installed on the breakout.

Design

Stefan Laimer and Maximilian Schäferle did a first concept design of a fiber fuselage during the Systems Engineering 2 course in WS20/21. This design is used for the first lamination tests. The design is available in "Onshape - Fuselage Shell".

Materials

The membrane supported vacuum infusion tests are done with the material from Composyst in Landsberg. The other tests with hand lamination and vacuum pressure are done with material from R&G.

Vacuum Pressure Materials

Neu für Flügel:

Membrane Supported Vacuum Infusion Process (Composyst) Materials

Gewebebänder, Mumpe und Gelcoat

Anschlüsse, Schläuche

Kleber

GFK Platten

First milling

On 15./19./20.12.2020 we did a first milling test with a small MB-0600 test block

The milling was done aiming at best milling results. So the distance between milling paths and z distance was set to 0.06mm. Schlichten took 2h 50min for the “Z Konstant” strategy and 7h for the “Überkreuz” strategy.

(Friedrich Beckmann, 23.12.2020)

First Lamination Test

Some initial lamination test with the “Minirumpf” with 2 x 160g/m2 glas fiber with vakuum showed laminates which seem optically o.k. but the laminate is not waterproof. I made three tests with different amounts of resin in the mould. The final weight after the vakuum process is however always more or less equal. The area of the “Minirumpf” is about 3dm with a laminate weight of 21g.

On 4.3.2021 Alex, Björn and I did a lamination test of the 80cm fuselage half.

Results

The laminate is not waterproof. After about 10 seconds water penetrates through an optically o.k. laminate.

There must still be air/voids in the laminate although it seems optically in good condition. The fuselage half has a weight of 116g.

First Laminate - Weight 116g

Ideas

A flat test laminate without vacuum shows a closed surface and a simple water test did not show easy water penetration. I think we must find a way to avoid the voids/air in the laminate. I am pretty sure that the voids also have an impact on the strength of the laminate but nothing is tested on that side. So to improve water resistance I have the following ideas:

(Friedrich Beckmann, 7.3.2021)

Membrane supported Vacuum Infusion (Composyst)

A first lamination test with membrane supported vacuum infusion technology was done at Composyst in Landsberg on 19.3.2021. The results are very promising. I have made a video to show the differences between vacuum compression and membrane assisted vacuum infusion technology. (TODO: Describe the process).

Friedrich Beckmann (1.8.2021).