T.R | Title | User | Personal Name | Date | Lines |
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357.1 | Lattest and GREATEST | SPKALI::THOMAS | | Tue Jan 27 1987 08:16 | 21 |
| Well I guess an update is in order. The club meeting has come
and gone. We didn't bring the ships but do plan to for the next
meeting. To date my buddy plane has had the wings joined and cap
stripped. Last week monday was snowed out. Last night was a different
matter. We got three good hours of building done. I was able to
catch up with my partner except for the cap strips. So, to date
both wings are sheeted and both fuse's are app 70% completed.
We made and installed the wing bolt hold down plates for both
ships last night. Our plans are to install the torque rods and trailing
edge centers and fiberglass the wings next week. If we get to it
we will bolt the wings to the fuses also. A change in the design
was agreed upon last night. We are going to go to 1/4 inch wing
tip blocks rather than the 1 inch we had originally wanted.
This is ti reduce tip weight and to shorted the wing down to 59
inches. Still at 59 " the wing area will be 724 sq's. That's not
bad. The thickness of the wing came out at the 2 1/4 inches we
wanted. With a root cord of 12.5 inches that gives us a 18% wing.
At 724 sq's and an 18% wing we will be displacing quite a bit of
air.
Tom
|
357.2 | Lattest update | SPKALI::THOMAS | | Wed Feb 18 1987 06:50 | 39 |
|
Well this project is still going, for those that thought I forgot
about it. The construction has slowed somewhat but I suspect that
it will pick up this coming monday. The Torque rods are in and
all of the other aileron parts cut. Both ships have large trailing
edges of app 1/2". As we looked over the balsa wood for a good
stiff piece of 1/2 inch material I became clear that there wasn't
any. To attain the desired stiffness we laminated two pieces of
3/8 by 2' trailing edge stock. These were in turn ripper on a table
saw removing app. 3/8 of an inch of material from the thinner trailing
edge part. A second rip cut was then done on the leading edge side
of the aileron that yielded a piecs of stock 1 1/2 inches in width
and 1/2 inch in thickness. the table saw was then adjusted to produce
a 30 degree angle. Two more rip cuts were done to the leading edge
of the aileron. Finished we had an aileron that anyone would appreciate
taking out of a kit box let alone have scratch built. The laminating
was done with simple CA glue. To say that these ailerons are stiff
is an understatement. I forgot to install two ply wing front dowl
supports at the spare so a little surgery was in order. Two slots
were cut and the pieces epoxied in place. I then install 1/8 inch
pieces of stock to fill the slots cut. These were then sanded to
a finished state. Repairs done this way yield a finish that doesn't
need any other fillers. Sometimes when you try and put the same
size sheeting back in place you tend to geta depression that then
needs to be fixed. Next week I'll be installing the landing gear
blocks and fiberglassing the wing center section. I'm going to
try a new method of holding down the fiberglass cloth while I apply
the epoxy to it. I'll be using a spray contact cement to keep the
cloth in place. Should be interesting. I suspect that the planes
will be ready for covering in mid March. This will work good as
by then most of the snow will hopefully be gone.
Regards
Tom
P.S. Is anyone reading this?
|
357.3 | Is anyone reading this?? | AUTUMN::NOYES | | Wed Feb 18 1987 08:04 | 6 |
|
YES!!
|
357.4 | yes | GOLD::GALLANT | | Wed Feb 18 1987 09:40 | 8 |
|
A-yup
Mike
|
357.5 | Contact Cement? | CLOSUS::TAVARES | John--Stay low, keep moving | Wed Feb 18 1987 10:34 | 5 |
| Tom, are you sure about holding that glass cloth in place with
contact cement? Seems like it would hinder the bond between the
resin and the wood underneath, and between the resin and the cloth.
Great idea, though. How about using CYA to tack the cloth in place?
Or 5 min epoxy?
|
357.6 | The theory | SPKALI::THOMAS | | Wed Feb 18 1987 12:19 | 28 |
|
I have used CA to tack the cloth in the past. I got the
idea of using the contact cement from a CA tape. Hot Stuff
I think. They used CA to bond the cloth to the balsa but
commented that they have in the past used epoxy for the
perminent bond. The contact cement is sprayed onto the cloth
not the balsa center section. To my knowledge there is no
penetration of the epoxy or resin into the glass fibers themselves.
Rather the epoxy or resin penetrates the balsa fibers and
surrounds the glass fibers to create the bond. The bond is
different from that of wood to wood where you get a penetration
of the glue into the two adjacent materials. I don't see a
problem if there is a surface of contact cement around the glass
fibers. I guess theoretically that if you took a cross-section
of the epoxy/contact cement/glass you may find that there is the
possibility that the glass fibers could be floating inside the
epoxy encasement on a film of contact cement. Would this matter?
I doubt it. I know that float between to adjacent surfaces can
cause problems. That is why most if not all pattern birds use
epoxy to bond the sheeting to the foam. However I think that
this theoritical floating of the fibers inside the epoxy would be
minimal if at all present due to the make-up of the weave of the
glass cloth.
These are my thoughts, any comments?
Tom
|
357.7 | | BASHER::DAY | Real men fly model aeroplanes... | Wed Feb 18 1987 12:28 | 5 |
|
I usually use a drop of thin ZAP to hold the
cloth in place while I put the resin on..
|
357.8 | Contact Cement? | CLOSUS::TAVARES | John--Stay low, keep moving | Wed Feb 18 1987 16:23 | 18 |
| The only thing that bothers me is that the value of a glassed
surface is the strength brought about by the union of the brittle,
but tough resin, and the strong (as in impact resistance), but
flexible cloth. The value of the bond is proportional to the
wetting out of the cloth. If you put something on the cloth to
prevent the resin from wetting it out, you are no longer
fiberglassing; in your case you are contact cementing!
As I see it, your resin is worthless in this case; it is only
serving to glue the contact cement/cloth to the fuse. Why not save
the weight and glue the whole thing together with the contact
cement?
Remember the note we had in the old file about spraying the cloth
with nitrate dope before applying? This was done to make the cloth
easier to handle and cut...could use the nitrate to tack the cloth
too, I suppose. I think that works because the resin will disolve
the nitrate as it wets out the cloth. Thats a happy marriage.
|