The joiner tube is a bit large so it needed filing down. The reason for the size is that the carbon joiner needs a fair amount of carbon in it and the aluminium tube is quite thick walled.
This is the joiner tube area after the first application of epoxy-cabosil-cotton flocks-micro balloon mixture. Some voids still need filling.
The aluminium tube with its carbon tows ready for insertion after resin application.
I am using the standard Reed specified S6062 at 7,95% thickness. For the stab I used an aramid leading edge but this was a bit tricky as I did it at the same time as the bagging! Not as per the experts and it was made even trickier because I only 3M77éd the stab halves together. Epoxy dissolves the bond after a short time...
For the wings Í discussed the layup with Craig (thanks!) and also used Joe Wurts' spreadsheet (http://www.charlesriverrc.org/artic...vacbaglayup.htm) which gives some comfort that things won't just break apart in mid air (as opposed to the more common/acceptable ground breakage!).
All the glass for the wings has been cut and is just waiting for the final sanding of the joiner tube areas while I debate whether to put on an aramid leading edge....
No comments:
Post a Comment