Chapter 6 - Fuselage assembly
Now all the flat parts are to be assembled into a 3-dimensional structure! The famous TUB!
The first thing to do is to test-fit all the bulkheads made in chapter 4. I cut them a bit oversize, deliberately, so I had to trim the parts a bit to get a good fit. Using the
multitool this is a quick job.
Test-fitting the front seatback. I have some gaps near the longerons, but these will be filled with flox so this is not a problem. The main
issue is to have a good fit along the sides, since this is essential to the width of the tub.
I used a contour gauge to transfer the shape from the fuselage sides to the corresponding bulkheads.
When fiddling with F22 I discovered a strange thing. I have built the bulkheads using the large drawings - not the M-drawings. I then discovered that the width of
F22 on the large drawings is 33.7" while the width according to the M-drawing should be 34.5" approx!! There is no doubt that the drawings differ, but which one is
correct? I asked the question on the Cozy-list, the canard-list and the canard-forum. No one could answer this but several builders had used the large drawings and
confirmed that their F22 was 33.7" wide. I got a tip to check the lift-tab-position of the canard to assure that they fit F22. That should be no problem, so I will
continue with the 33.7"-version of F22.
As you can see - it's 11mm that differs on each side.
The tub is starting to take shape! Here I have followed the plan assembling the tub the right way up. Many builders have assembled the tub upside down, but I
chose to do it the plans way. I started by leveling of the plank at the bottom, and also the 2"x4" fore and aft. The longerons are at WL23 - i.e. 23" up from the
plank. This is only a dry-fit. I will use flox when I assemble the tub permanently. I measured the diagonals to look for straightnes. It was only 2mm difference, so
I call it good to go. Just to the right of the tub in the picture is the landing-gear bow. I bought it from a builder in US that had to abandon his project. It is brand
new and came with the nose-leg as well. I got a good deal and helped him out as well. Pity he wasn't able to continue his project though.
Before I floxed the instrument-panel to the fuselage-side I routed a groove in the foam with the Dremel. This will give a little better bonding since the flox will
fill this groove.
After once again checking for straightnes in all dimensions, I have now floxed the front seatback, the instrument-panel and F22 to the fuselage-sides.
I used the plans method to squeeze the fuselage-side together using a couple of planks and some rope. Making a tourniquet it's easy to adjust the pressure.
Now it shall cure for 24 hours without anyone touching it. As Nat says in the plans: "Don't even let the dog inside while curing!".
While curing I started to cut all the BID-tapes using the plans method of laying an 8" BID-ply ontop of some plastic, apply epoxy and then cut in 4 2" strips.
Worked rather good, but if I should do this again, I would use 3" wide tapes rather than 2". My problem was that the BID-tapes stretched a bit hence got
more narrow. Then I had to widen them again, much hazzle her. Had I been using 3" tapes instead I would have had a greater tolerence here. It was also a
suprisingly long job to glue the BID-tapes on! I spent 2.5 hour to make the tapes and glue them on and peel ply.
The next step was to flox the landing-gear-bulkheads. Goofed up the aft. I forgot that there are a front and an aft side of this bulkhead. The front side had 8
plies of bid extra. I managed to flox it backwards. It was easy to cut it out and reattach it, no big deal at all. I discovered that I was not the only one doing
this, luckily I discovered it early. I sent a tip off to the Cozy-FAQ mentioning that it's easy to do a mistake here. After cure I floxed the front lower LG using
the plans method.
Suddenly the temperature outside dropped to -10 degrees celsius (14F). Christmas is also just around the corner. I decided to turn the heater off to save
some money and wait for the temperature to rise over christmas again. The weather-forecast says it will be cold until next year, so I guess this will be the
last work done in 2009.
2010:
Off to work again! The temperature has raised to approx 0 degress celsius so I have started the heat-pump again. I finished the landing-gear bulkheads
using the plans method. I have also added 3 plies UNI on the front side og the front LG as per plans. Finally I BID-taped the front LG to the fuselage and
taped the joint between the lower and upper front LG. The next step will be to turn the fuselage upside down!
Finally I BID-taped the front LG and the joint between the upper and lower LG and peel-plied the whole thing.
Since the temperature is low outside, it is rather cold at the floor. To boost the temperature while the epoxy is curing, I made a "heat-tent"
of some plastic that I covered the tub with. Inside I have a small heater that raises the temperature to approx 30 degrees centigrade.
I've now turned the fuselage upside-down and floxed the lower part of the permanent firewall as well as taped the rest of the landing-gear.
Following the plans method I mark the parts on a sheet of H45 (substitute for Last-a-foam) and glass the parts before I cut them out.
I need to fabricate the bracket for the fuel-selector. I bought the aluminum-piece from Aircraft Spruce - but I had to cut it out
according to the template in the plans. After carefully measuring and drilling the holes, I have to bend the piece making to 90
degreees bends. Many people have had problems here with the aluminum breaking in the bends. The first thing to observe is to bend
across the grains in the aluminum. The next thing is not to make a sharp bend, but make a radius. To help me I cut a piece of wood
2" wide that matches the inside of the bracket. Then I sanded the corners making a gentle radius for the bracket.
I then fastened the aluminum and the wood-template in my vice and with a hammer I carefully bent the piece to the proper
shape.
The result was perfect!
The next part to do is the heat-duct and seatback-brace.
I then riveted the two anchor-nuts and alodined the bracket and the aluminum-tube for the seatbelts.
Here is the seatback-brace wich contains the map-pocket and the fuel-selector. I have made two plywood-inserts as
pr plans where the fuel-selector-bracket is to be floxed in place. I have also floxed in place the spacers inside the
brace and covered the unglassed sides with 1 ply of BID. Next step is to flox the upper triangle ontop of the
construction and flox the fuel-selector-bracket in place.
The whole assembly is now curing. When cured I will glass the outside with two plies of BID.
Here is my first deviation from the plans. I was to install a aluminum-tube through a hole in the plywood for the
landing-brake-mechanism. Since I am going to use an electric actuator instead, I don't need this tube. I didn't realize this until after I
drilled the holes. I just filled the holes with flox - no big deal.
Actually I see now that I could have skipped the plywood-inserts completely.
The heat-duct-parts are assembled with flox (glassed side facing in!) and I have removed foam two places - for the
seatbelt-tube and for the fuel-tubes. I will then flox the seatbelt-tube to the heat-duct and cover it with 7 plies of
UNI as pr. plans.
The UNI-layer (7 plies) are made as pr. plans. I wet out 2.5" then fold the cloth over and cut the fold. I tried to
use a scalpel but ended up using my scissors to avoid messing the fibers in the cloth. Had to rinse the scissors
afterwards with acetone.
Not so easy to see but here the 7 plies are neatly stuck ontop of each other making a nice tapered edge with the
thickest part at the center - right ontop of the seatbelt-tube.
The heat-duct is placed ontop of a plank to raise it above the table a bit to allow the two plies of BID to hang
down from the bottom edge. I then peel-plied the whole thing. The seatbelt-tube is visible to the left and the
space for the fuel-tubes is the large low part to the right.
Since it's -2 degrees celsius (26 Fahrenheit) I had to make a little heat-tent to raise the temperature
around the heat-duct so it will cure. Works like a dream. I have a thermometer at the other side of
the tent showing 30 degrees celsius (86F).
Glassed the outside of the seatbrace with 2 plies BID. I made a stand to mount the seatbrace on so I could
glass both sides at once. Put the plastic-sheet around as I did with the heat-duct and put the heater on.
Still cold outside - and snowy! :-(
Floxed the seatback-brace to the heat-duct. Later I will add BID-tape to secure the joints. To be sure the seatbrace is
vertical I made a jig that I leveled up and used a clamp to hold the brace against the jig while curing.
Floxed the assembled brace/heat-duct to the tub.
Used a laser to be sure that the assembly is dead center. Could as well used a thread but a laser is
much cooler... :-)
Here I have cut the foam for the floor and made the wood-frame to keep the right curvature when
glassing the inside of the floor.
The floor is here lying on the frame. I have cut out spacers and just fastened them with nails. Next step is to
taper the edges to make a smooth transition between the floor and the spacers. Showing in the next picture is
the cutout for the landing-break. I followed others advice here and made the hinge-line at full width, not the
10" suggested in the drawings.
When I tapered the spacers in the fuselage sides (chapter 5) I used a manual hack-saw, quite a job that required much
sanding afterwards. This time I decided to use my jigsaw. I have quite often used it as a table-saw by fasten it upside-down in
a workbench. I developed this concept further and made a solid base of 15mm plywood where i routed a depression to fit the
base of the jigsaw. This plywood-base is then just fastened in my workbench when I need it. It's easy to slide the jigsaw in and
out of the base when I need to use it elsewhere.
To make the 30° cut required I had to make a jig since the maximum angle I can tilt the jigsaw is 45°. To get the geometry
correct I actually have to tilt the blade 60° to make a 30° angle if I was to use the jigsaw without any aiding-tools. The above
picture show how the jig was made out of some plywood-pieces I had. The jig is fastened to the base with a couple of screws
so it sits firm. As seen on the full-size picture the cut is clean and requires no additional sanding.
Beware your fingers if you try this method! Since the blade goes both up and down the foam may jump right
out of your hand and possible your fingers may slide into the blade! Happend to me a couple of times, luckily I
managed to avoid my fingers getting hurt. It's very important to hold the foam steady with a firm grip while passing it slowly
through the saw. I also used a wood-stick in front to push the last inch through the blade as an extra insurance.
The corners was cut out manually using a hack-saw and glued back in place with 5-min epoxy. After the spacers
are microed to the bottom and cured, I will sand them to a smooth finish and prepare them for glassing.
Now the spacers are sanded and prepared for glassing. I put the floor on place on the tub to check that everyting fits,
and it looked all very well. Spent an hour and a half afterwards cutting the glass and peel-ply. I can't glass the floor
before I know I have an uninterupted room of hours ahead of me, so I guess I'll wait until Sunday. The family
demands my attention also :-)
Btw - I am not using Last-A-Foam for the spacers, but Divinycell H80 since LAF is not available in Norway. H80 is a
better quality foam, but also more expensive. Still - it's cheaper for me than paying freight for the foam across the
Atlantic. Since LAf is urethane-based I guess it's a bit easier to sand and form than H80, but with good tools sanding
H80 is no problem at all.
The next thing to do after the floor was glassed was to flox it onto the tub and weigh it down while curing. The plans
tells us to glass the floor, wait 12 hours, then flox the floor and BID-tape it right after. Many builders choose to do this
is three steps since the workload is rather high during these steps. I choose the same thing. So I glassed the floor,
allowed it to cure, then floxed the floor to the tub and allowed it to cure again. The last step in this chapter was to
BID-tape the floor to the sides. According to the plans I should do this while the tub was upside down (since the floor
was curing). Luckily I know could turn the tub sideways and do the BID-tapes a lot more easy. The last picture here is
the BID-tapes with peel-ply, curing.
There was lot of work in this chapter, including some time-consuming parts. I look forward to the next chapter where the
fuselage will be formed and glassed! Need to buy some more epoxy now. I have almost used the first batch of 25kg!
Time used this chapter: 69 hours
Started: 2009-11-22
Ended: 2010-03-13