Differences

This shows you the differences between two versions of the page.

--- searchwing-fiber [2021/03/07 12:37]
beckmanf [First Lamination Test] add degassing
+++ searchwing-fiber [2021/08/01 09:02]
beckmanf add concept design Laimer/Schäferle
@@ Line 25: / Line 25: @@
 The Deskproto CAM software needs some RAM depending on the detail level. The Deskproto Software is [[https://www.hs-augsburg.de/homes/beckmanf/dokuwiki/doku.php?id=breakout#deskproto|installed on the breakout]].
+==== Design ====
+Stefan Laimer and Maximilian Schäferle did a first {{ ::g4-faserverbund.pdf |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 [[https://cad.onshape.com/documents/462341583a3ce9a0ce3df71b/w/451ff5ec3fe9085daef8b15f/e/eae436c607beb291f9462ec2|"Onshape - Fuselage Shell"]].
 ==== First milling ====
@@ Line 64: / Line 68: @@
   * [[https://youtu.be/s8uSAbvXaIA|Youtube: SearchWing - Wassertest]]
-There must still be air/voids in the laminate although it seems optically in good condition. The fuselage half has weight of 116g.
+There must still be air/voids in the laminate although it seems optically in good condition. The fuselage half has a weight of 116g.
-{{::sw-2020305-80cm-rumpf.jpg|First Laminate - Weight 121g}}
+{{::sw-2020305-80cm-rumpf.jpg|First Laminate - Weight 116g}}
 === Ideas ===