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| searchwing-fiber [2020/12/23 12:57] – added deskproto breakout install beckmanf | searchwing-fiber [2022/03/26 15:33] (current) – [Fiber Fuselage] add milling beckmanf | ||
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| * Fiberwings will pave the way to possible solar cell support for extending range | * Fiberwings will pave the way to possible solar cell support for extending range | ||
| - | The big drawback is missing experience with aircraft design and fiber technology. | + | The big drawback is missing experience with aircraft design and fiber technology. |
| + | |||
| + | * [[sw-fiber-wing|SearchWing Fiber Wing]] | ||
| + | * [[sw-fiber-servo|SearchWing Fiber Servo]] | ||
| + | * [[sw-fiber-fuselage|SearchWing Fiber Fuselage]] | ||
| + | |||
| + | As description about the tooling is here: | ||
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| + | [[sw-milling|Milling at Hochschule Augsburg]] | ||
| ==== Strategy ==== | ==== Strategy ==== | ||
| Line 15: | Line 23: | ||
| * Mill: Step-Four Xpert 1000 S in the Holzwerkstatt Modellbau | * Mill: Step-Four Xpert 1000 S in the Holzwerkstatt Modellbau | ||
| * CAD: Onshape, CAM: Deskproto, NC: XpertMill (Holzwerkstatt) | * CAD: Onshape, CAM: Deskproto, NC: XpertMill (Holzwerkstatt) | ||
| - | * Glueing of the Rampf MB-0600 for L shape: Rampf EP2306 | + | * Glueing of the Rampf MB-0600 for L shape: Rampf EP2306 |
| * Surface Sealing of the MB-0600 material with Münch Mikon 399 MC sealer | * Surface Sealing of the MB-0600 material with Münch Mikon 399 MC sealer | ||
| * Release Agent (Trennmittel): | * Release Agent (Trennmittel): | ||
| Line 25: | Line 33: | ||
| The Deskproto CAM software needs some RAM depending on the detail level. The Deskproto Software is [[https:// | The Deskproto CAM software needs some RAM depending on the detail level. The Deskproto Software is [[https:// | ||
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| + | ==== Design ==== | ||
| + | |||
| + | Stefan Laimer and Maximilian Schäferle did a first {{ :: | ||
| + | |||
| + | ==== Materials ==== | ||
| + | |||
| + | The [[searchwing-fiber## | ||
| + | |||
| + | === Vacuum Pressure Materials === | ||
| + | |||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
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| + | Neu für Flügel: | ||
| + | |||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | |||
| + | === Membrane Supported Vacuum Infusion Process (Composyst) Materials === | ||
| + | |||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * Lochfolie, Fließhilfen, | ||
| + | |||
| + | |||
| + | === Gewebebänder, | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | |||
| + | === Anschlüsse, | ||
| + | |||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * PVC Schlauch ID 8mm | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | |||
| + | === Kleber === | ||
| + | |||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | * [[https:// | ||
| + | |||
| + | === GFK Platten === | ||
| + | |||
| + | * [[https:// | ||
| ==== First milling ==== | ==== First milling ==== | ||
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| * {{ :: | * {{ :: | ||
| - | 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" | + | 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" |
| + | |||
| + | (Friedrich Beckmann, 23.12.2020) | ||
| + | |||
| + | ==== First Lamination Test ==== | ||
| + | |||
| + | Some initial lamination test with the " | ||
| + | |||
| + | On 4.3.2021 Alex, Björn and I did a lamination test of the 80cm fuselage half. | ||
| + | |||
| + | * Surface Sealing of the MB-0600 material with Münch Mikon 399 MC sealer | ||
| + | * 2 x Release Agent (Trennmittel): | ||
| + | * R&G Resin L with EP161 Hardener | ||
| + | * First layer of pure resin with brush | ||
| + | * 1 x 49g/m2 glas fiber (brush) | ||
| + | * 3 x 160g/m2 glas fiber (brush) | ||
| + | * Abreißgewebe (brush) | ||
| + | * Lochfolie | ||
| + | * Saugvließ | ||
| + | * Vakuumsack at -900mBar for 24h | ||
| + | * Removal of the laminate from the mould after another 24h | ||
| + | |||
| + | === Results === | ||
| + | |||
| + | The laminate is not waterproof. After about 10 seconds water penetrates through an optically o.k. laminate. | ||
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| + | * [[https:// | ||
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| + | There must still be air/voids in the laminate although it seems optically in good condition. The fuselage half has a weight of 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: | ||
| + | |||
| + | * Add an epoxy gelcoat layer. Yachts and gliders have a Gelcoat finishing layer but most model planes do not have that. This will hopefully provide a closed watertight surface layer. | ||
| + | * Hand lamination without vacuum. The hand lamination will have more resin in the laminate and the surface seems closed. No idea if the voids are reduced or if there is just a closed surface. | ||
| + | * Vacuum infusion. Compared to vacuum bagging literature claims that voids are reduced with this technique. The VAP membrane technology might be a way. This promises a void free laminate with a high fiber content. | ||
| + | * Degassing the resin. Is probably useless for hand lamination because bubbles are introduced during the lamination process. | ||
| + | |||
| + | (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 [[https:// | ||
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| + | Friedrich Beckmann (1.8.2021). | ||
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