Chapter 18 – Canopy, my canopy!

I should note starting off that it took me a bit of research and thought yesterday to figure out that I needed what was essentially an interior “wall” to retain the wet flox & BID that goes into all the component hard points on the canopy frame.  Thus the reason for a layup of 2-3 plies of BID –above and beyond the normal layup schedule– at each hardpoint location.

I started off today with another long round of more refined clean up of the canopy frame.  I Dremelled off a lot of dead micro, and also Dremelled a small trench around the front edge of the canopy about a foot in each direction from CL.  Like the top side per plans, I’ll also lay up the first ply with the glass going into this trench and fill it with flox.

I then got to prepping the right front hinge location for a retainer layup, as I mention above. The plans denote a 1.5″ thick (over normal width longerons… more on that below) canopy frame where it contacts the longerons, but since my canopy rail matches the thickness of the longeron (~0.8″) on the front half, I needed to ensure I maintain (or make) my hard points at the 1.5″ width.  As it goes, at the front end of my canopy frame it’s not difficult to obtain or keep the 1.5″ width for the hard points.

But I digress, back on the front hinge hard points, I used micro on the areas that would not get dug out and then placed raw epoxy and then a patch of peel ply over each actual hard point spot.

I then laid up my prepregged 2 plies of BID over the hard points, and then peel plied that since the final interior canopy frame layup will cover this glass.

I then taped off the back right half of the canopy along the “glass-to” line that matches the exterior glass line of the canopy.  I then sanded the bare canopy edge to give it texture to grip the interior glass when it’s laid up.

Since I don’t have 1.5″ of foam frame here, I manufactured it by shaping a piece of foam that will get micro’d to the existing foam rail.  I made it “L” shaped so that it also rests on the bottom half of the exposed canopy edge, with plenty of room for glass above it.

I then micro’d the additional foam piece in place that then gave me 1.5″ wide on the canopy rail right at the right side canopy aft hinge hard points.  The foam piece extends 1″ beyond the hardpoint segment forward & aft to allow for a transition back to the existing narrower canopy frame.

I then made up another piece, only for one hardpoint, on the other side for the #3 of 4 canopy latch.

[NOTE:  I’m going with 4 canopy latches.  Here’s why:  My canopy goes much further aft than plans, plus I have a longer aft canopy frame.  In addition to that little factoid, I don’t have a good option for keeping/incorporating the middle latch in the same place due to my roll bar frame.  If I move the middle latch forward 2″ than I can just barely clear the frame, but since I have the entire kit from Jack Wilhemson, pre-made, then I only have enough of the long rod (tube) that then forces me to move the aft latch forward about the same as the middle latch.  So, I have much more canopy + frame aft, but then I’d be moving my aft latch forward a minimum of 2″.  I don’t much care to do that.  I’d rather move the aft latch back an inch, move my middle latch forward 2″ and then fill that gap in with another latch.  With a MUCH bigger canopy than stock I think I wouldn’t mind having one more securing latch anyway!]

Here’s the foam piece micro’d in place for the #3 of 4 canopy latch, that will be located just aft of the roll bar frame.

I then cut another piece of foam (quickly, since I had leftover micro) and clamped it in place on the left side aft canopy frame.  This foam piece will of course make up the left aft canopy latch hardpoint.

So, here are the foam pieces (incorrect width! more on that below…) for the aft 2 canopy latches, secured in place with clamps while the micro cures.

And a bit a later after the micro cured…. look nice eh?  But again, wrong width!

My mindset the whole day had been geared towards the aft hinge hardpoint, which, no matter what size the longeron is needs to be 1.5″ minimum width to have a good foundation for mounting the hinges to.

With that in mind, I got busy shaping/curving the top side of the added foam so it made a nice transition into the canopy edge.

I prepped it in the same fashion as the front hinge hard points and as I was finishing up the 3 ply BID layup I was thinking about my next task: glassing the 2 hardpoint retaining layups on the other side…. I then had a DOH! moment.

As I mentioned, no matter what size the longerons are, the 1.5″ wide hardpoint works fine for the hinge hard points, but that is not the case with the canopy latch hard points, which MUST overhang the longeron inboard since the latch assemblies attach inboard of the longeron.  Remember, from the pilot’s seat aft my longerons are a hair over 1″ wide, so a 1.5″ wide hardpoint works for a 0.7″ wide longeron, but not a 1″ wide longeron.  Ugh!  The good news is that I caught my error before I glassed in the retaining layups at these hard points.

Again, having some left over micro, I quickly made up 2 more additions to bring the canopy frame inboard a minimum of 0.35″ to allow enough hardpoint for the latch assembly to attach to.  The foam pieces are a bit thicker than required, but of course I’ll just sand them down to the proper thickness before glassing the retaining layups.

I then got busy digging out the foam and removing the inboard peel ply off the 3 left side forward hardpoints . . .

And the two forward right side hinge hard points.

BTW, although these layups were fairly fresh and I used NO micro on the foam surface where I applied the peel ply, it was still amazingly difficult to remove…. each hardpoint took a good 10 minutes in just removing the peel ply!

About this time in the evening is when everything turned magical, and by magical, I mean it went south ….. a bit.  Kinda weird and still assessing!

I started off by rereading the plans and then proceeded to glass in the 3 hard points along the front left side canopy frame.  I knew from accounts from other builders that 15 plies in these hard points, especially the deeper ones I had, was simply a fantasy and that it required a whole lot more than that.  I gathered up all my BID scraps, whipped up some flox using my “slow” hardener (75/25 slow/fast) to a point where it was right at the cusp of being wet flox (i.e. towards the thicker side of wet flox), and got to work.

Ok, first off, my bad for not taking into account the heat in my shop.  It was HOT outside and well over 80° F in my shop.  Secondly, I had never encountered an issue with a large scale exotherm type event with anything other than using fast hardener.  IIRC, in Germany I had an exotherm with a huge cup of epoxy when I left it sitting there for a good while when I was doing something really big like the wings or fuselage, and one event when I used fast hardener for the filling in the one of the elevator hinges . . . which resulted in it spitting the flox right out of the hole.

But just as I was a few plies from finishing up these holes, I started to see some bubbling around the edges of each hole.  I felt the sides of the retaining glass and it was hot, so I grabbed my thermometer.  I got one reading at 201° F for a blip, but couldn’t replicate it. Most of the readings on all the surfaces on or around the hardpoint layups were in the range 160-195° F.

I had a couple of small leaks around the retaining glass layups going on which had annoyed me since I had to keep wiping up epoxy running down the inside of the canopy (one of the few times I’ve used paper vs plastic, and I got a fair bit of epoxy running down the paper!)…. however, I think these leak areas worked to allow the heat to vent and the layups to stay in place with no expulsion action going on.  I continued to monitor the temps as there was no discoloration of glass on the top side of the canopy frame and no melting foam anywhere.

Out of curiosity I tried to add a bit of flox to the top side of each layup just to use it up and get the final 0.2″ of fill on each hole.  However, when the flox hit the bubbling brew on each hole it just burned out immediately and turned white (as you can see in the pics below).

The layups stayed warm for quite a while, but again, except for one non-repeatable blip just over 200°, I never saw any dangerous temps.  I’ll cut a core out of one of the hard points to see if it is solid [it should be, it was filled with glass] and check to see if the epoxy/flox just cured overly fast or if it burned out.

Having learned my lesson, I then grabbed a can of straight SLOW hardener and got to work on the right front hinge hard points.  Note the duct tape on the front hardpoint… this tape plays a key role in the next part of my story.

You see, as I was filling up the 2 front hinge hard points, I thought to myself the front hard point must be bigger than the back one, because the back one is filling up noticeably quicker with the same amount of flox and glass going in.  That’s when I realized the front hardpoint was leaking and thus harder to maintain the same level as the aft hardpoint.

Seeing that I wasn’t going to win this game, and almost out of flox in my cup, I simply cut a piece of peel ply for each hole and set the peel ply in place.  I would simple finish these holes with flox paste tomorrow and call it a day.  I did a final wipe down of all the epoxy that had run down into the canopy onto my thick brown paper, and knew I’d be back one more time for some cleaning before heading to bed.  And with that, I went upstairs and took a shower.

 

 

When I returned to clean up the epoxy mess caused by the leaking front hardpoint, what did I find?!  These hardpoint layups –with straight SLOW hardener– both had some minor bubbling going on around the edges!  I grabbed the IR thermometer again and checked temps (again!) and sure enough, same range as the left side: 160-195° F.  Highest temp I saw on this side was 198° . . .  amazing.  Again, no discolored or burned glass or foam anywhere, just a really hot curing layup. (sorry, no pic of this tonight but I’ll grab one for tomorrow’s post).

So, I cleaned up the epoxy, went upstairs to spend some time uploading the pics for this post and returned about 45 minutes later.  The temps were still fairly high, although significantly cooler (130-150° F), and the epoxy leak had stopped, so I did a final cleanup of the epoxy and pulled out the wet tape and paper from inside the canopy to ensure I had no curing flox or epoxy on the inside canopy surface…. thankfully it was really clean and nothing had really gotten onto the canopy.

Since the weather temps are high here and my canopy hard points are significantly deep, for the last 4 hard points I will fill them halfway and then peel ply the layup, and then finish it after it cures.  All I can say is wow.  I guess my technique of trying to follow the plans is more hazardous than stuffing the holes with BID and pouring wet flox in & around it!

All part of the struggle I guess of building these airplanes!

 

Chapter 13/18 – Canopy hard points

I started off today by doing one final sanding of the aft nose cover –specifically where I added height by installing 1/8″ thick Balsa strips– and prepped it for glassing.  I then applied a bit more micro to do one final smoothing of the transition between the added Balsa wood and the originally glassed aft nose cover.

I also added some protective duct tape at the aft end to protect the intersection with the glare shield.

I then laid up the 1 ply of BID on the aft nose cover, which should do it for the major glassing on the cover.

I then peel plied the layup.

One last shot of the peel plied final major layup in the aft nose cover.

I took the leftover micro and knocked out another strake rib by filing in the mouse holes with the micro … almost!  I then realized I forgot the cutout in the middle part of the rib! That will need micro on the last 2 recent ribs that I’ve just done.

Jumping ahead a few hours –to stay on course thematically!– the layup on the aft nose cover was essentially cured.  Here it is after I pulled the peel ply.

A view from the nose (always nice!).

Moving on to the canopy, I then set the canopy structure up on saw horses.

And then spent a good while cleaning it up… a lot of dead hot glue and micro needed to come off!

I realized that I just couldn’t add the myriad of layers of flox and BID for the hardpoints with my canopy rails configured like they are . . . there’s just not enough meat to do it, nor is the shape of the side foam (mine are more vertical vs. horizontal) conducive to constructing hard points in the traditional plans manner.  Thus, I decided to add inboard sidewalls just for the hard points and for retaining, restraining & containing the BID and flox laid into each hardpoint.

I peel plied the underside (outboard) side of each BID pad for these 3 front left side hard points (from left: front canopy latch, canopy safety catch, and middle canopy latch) and also the inboard side so that I could add the normal glass layup schedule right over these pads.

I also did a bit of assessing on the right side canopy’s hard points for the 2 hinges.

Finally, I marked the thickness and did an initial trim of the the right side interior turtleback foam (I couldn’t easily get to the left side because it’s a bit too crowded currently on that side…. plus, it was late!).

Tomorrow my goal is to get all the hard points laid in and curing.  I also plan to get the canopy interior glass laid up by Tuesday so that after my next short trip to North Carolina I can get the canopy mounted in place with the hinges.

 

Chapter 18 – Canopy removed

I started off today by marking the cut line that will separate the turtleback from the aft canopy frame.  To reiterate, not only is the overall combined length of the turtleback and canopy frame significantly shorter on my airplane that per plans, but the ratio is much different in that the canopy frame is longer than the turtleback. This is opposite the configuration than the way the plans has it.

I also cut the overhanging/excess glass from the latest layup over the added 1/4″ foam piece.

I then did a quick mockup of the upper engine cowling to determine where the shoulders of the upper cowling were located –these shoulders are a unique feature of the Mike Melvill CF cowlings.

I marked the shoulder interface and then extrapolated where the turtleback & CS spar portion of the slope that extends from the cowling shoulder would be.  I won’t be using this information now, but I did want an idea of what I’ll need to do down the road to prep for this configuration issue.

Not really having contended with the upper cowling “shoulder” issue and how the requisite forward wedge/coned shaped piece that terminates just forward of the CS Spar front face means that I will have to cut off the lower aft corner of the canopy frame and reattach it to the front bottom corner of the turtleback-to-longeron intersection.  Clearly I couldn’t do it at this point because the releasing duct tape that I placed between the bottom of the canopy frame structure and the longerons prevents any permanent structure to remain at this point.  It simply has to be done one the tape is removed.

After I cut the turtleback-aft canopy frame line with the Fein saw, I then took a few hour break to go run some errands and pick up some 1×3 and 1×4 pieces of wood for the canopy brace that I then constructed around the canopy frame before I removed the canopy from the fuselage.

Here’s the finished canopy frame constructed to remove the canopy from the fuselage.

I ended up having to use Bondo in a few key places to ensure the wood strips along the side would stay in place.  I also used it on each end to reinforce the vertical parts.

I went upstairs for a bit while the Bondo cured, and when I returned back to the shop the canopy was ready for removal.

I have to say that with the 1/8″ spacers in place on top of both longerons, the canopy removal wasn’t that big of an issue.  It took a little over half an hour and I had the canopy off and on the floor inverted.

I should note that before I started in on the canopy removal in earnest, I reached up through the hell hole and used a 1×2 ACS shipping piece of wood to knock loose the aft canopy vertical spreader cross support boards that were wedged and hot glued into place.

Of course there was a bit of a mess on/around/in the fuselage when I removed the canopy, but I had it all cleaned up in fairly short order.

I also cleaned some of the foam gunk out of the channel between the GIB headrest and the interior foam wall (currently) of the turtleback.

Part of cleaning up the fuselage involved finally ripping out the foam and tape that I used as a form to create the glare shield.  The pic below is the first time I’ve seen my glare shield without any form underneath of it.

And here’s a quick pick of the glare shield with rubber edging in place.

I then proceeded to spend as much time or more than I did removing the canopy on cleaning up the “melted” duct tape (very gummy) from off the top of the glare shield.

I also grabbed a shot of the underneath side of the glare shield structure.

Now, because I was sticking a knife underneath the canopy edge to work it loose, there was some slight collateral damage in that the right aft outboard corner of the glare shield got dinged up a bit…. as did the left side actually!

I also put a decent sized gouge on the underside of the canopy front skirt.

Speaking of the underside of the canopy front skirt, I have to say I’m extremely happy with how the pour foam filled in the gaps and contoured in spot on fashion with the raised aft lip of the glare shield.

Finally, I liked the way this look so I snapped a shot of it.  Here we have a new version of the fuselage with the canopy off again.

Tomorrow my goal will be to get the interior canopy frame shaped and the hard points glassed at a minimum.  If possible, I would like to layup the canopy’s interior glass… but that may be pushing it a bit.

 

Chapter 13/21 – Turtleback tweak

First off, I know I’m spending a number hours more per day than I had planned on this canopy… however, I both want to clean up what I consider a big SNAFU on my turtleback and get the canopy acceptably configured for transport.

Defining the turtleback issue:

In the pic below, note the 9 O’Clock bulge and the 1-2 O’clock deflation.  I think I unknowingly did this by forcing the canopy bottom corners both over to the right before placing the turtleback foam in place.  Actually, I did notice it, but I thought it was a very slight, minute shape shift. It just wasn’t obvious nor clear that it would become so obvious and prominent after shaping and glassing the turtleback.

I wanted you to see the pic below, with the turtleback unmarked and in its current “natural” state.

The turtleback shape mitigation plan:

Here is my analysis of how to minimize the misshapen turtleback, and as you can see in the pic below I’ve marked it up to explain my mitigation plan.

First off, let me reiterate and be clear that my plan is to MITIGATE this off-balanced issue as best possible.  I have NO illusions of completely eliminating it.  The only true fix would be to rip off the canopy and redo the whole thing, with my entire focus then being how to mitigate this configuration debacle on the aft end vs (again) eliminating it.  And of course risking the chance of screwing up the very nice outcome of the front 90% of the canopy!

Problem #1 is the bulge on the left side, denoted in the pic below with the red oval and the white star being the apex of the bulge.  Note how below the star the canopy is vertical to almost coming back inboard.  Contrast this with the other side (right) where it has a comparatively gentle sloping curve, much more constant in nature.  To be clear, the aft canopy edge drove the shape of the turtleback so the only thing further outboard than that canopy bulge on the right is the 3 plies of BID holding it in place.

The REASON this shapeshifting occurred was most likely my maniacal –and probably misplaced/misguided– adherence to keeping the center canopy elevation even with the upper engine cowling extended contour angle (denoted by the green arrow and line).  If I had adjusted the canopy and let the elevation of the top go where it wanted to naturally, I think I’d still be dealing with this configuration oddity, but just in a less severe form.

Yet another issue, that will actually help in the attempted remedy of this SNAFU, is that for some mysterious reason –despite many repeated measurements– the fore/aft vertical canopy line of the turtleback glass overlaying the aft edge of the canopy is 0.35″ aft on the right side than it is on the left… which I’ve denoted with the blue line.  This obviously means the left is more pronounced when looking at the turtleback from CL aft as in this pic because its termination line is 0.35″ forward than the right side.  Making the bulge even more pronounced!

My plan is a 2 step plan.  First is to fill in the area marked by the yellow dashed line with 1/4″ foam and shape it.  Focusing on trying to manufacture a right side apex (purple line) opposite the left one.  I will also very aggressively sand the left side along the apex line to knock that down as much as possible.  Even 0.020″ will make a difference.

Part of the deflation between the 12 O’clock and 3 O’Clock positions is that on the left side my sanded depression for the 3″ UNI tape was close to spot on and it was even with the other foam surface, whereas on the right I went just a hair deeper and the UNI tape is not proud nor even, and is ever so slightly sunken… but not enough to affect the glass transition with the overlying BID.  It just adds to the depressed/flat/deflated look on that right side.

Now, I say a 2 step plan due to the fact that I feel I can/should deal with the turtleback to canopy angle issue later, after I get the upper cowling in place.  However, IMO I need to see if this remedy for the right side will work effectively BEFORE I pull the canopy off to shape and glass the interior surfaces.  If it just doesn’t work, I may go further in my corrective actions.

One final thought on the remedy to my unsightly creation, which actually isn’t really a remedy but rather of byproduct of the shape and configuration of my plane’s major components.  The bulkiness, size and shape of the canopy does a good job of hiding this issue from the front.  It will most likely be more noticeable with the airplane in the grazing position because it naturally takes more of the canopy’s sheer size –that serves to block the turtleback from view– out of play.  The other saving grace for my surreptitious cover up here is that the cylinder humps on each side of the upper cowling serve to block the view of the lower half/third of each turtleback side when viewing it from the back side of the plane (determined by my holding the cowling in place and assessing the aft view with cowling in place).

Clearly what I’ve shown here in these 2 pics is NOT visible (to my knowledge) in any of the pics I’ve taken at other angles.  Since you can’t be on separate sides of the airplane at the same time, I think if I add mass to the right side and mitigate the off balance between the two sides it would be really hard to get a really good view of this abomination at any other angle other than straight forward or aft of the plane.

Finally, I’m not trying to hide bad workmanship and be done with it.  Clearly there are no structural issues at play here and it’s my belief that any airflow imbalance will be minimal.  But for the sake of getting this thing in the air, and also to not waste any more time, materials, or money, I want the best mitigation possible and point out the view-blocking components as a point of note.  No builder wants a glaring, non-structural issue being the focal point that eyes are drawn to on their creation as it sits on the ramp!

So I started today by trimming the overhanging cured glass from around the firewall.

Here’s a side shot of the overhanging glass over the firewall’s aft edge.

Here we have the glass trimmed away that was hanging over the firewall and also the 1/4″ thick Divinycell foam that I micro’d to the right side turtleback.

I then did an initial round of sanding on the added foam, as well as cleaned up some micro runs.

Here’s the 1/4″ thick added foam piece sanded and shaped down close to its final shape before glassing.

Here you can see that, although still not perfect, the addition of the foam has taken the shape & aft view of the turtleback from “Ooh, gross!” to “Hmm, it’s not horrible…”

I then micro’d the foam and glassed it with 2 plies of BID.  I used an extra ply to allow me to really hit it hard with a sanding block if need be when it comes time to finish the surface for paint… with the micro finish allowing me to further fine tune the turtleback’s shape and symmetry as well.

Here’s a shot of the shaped & glassed foam added to the right side of the turtleback

This pic shows the newly positioned line of the canopy to turtleback intersection.

Before I got busy sanding and shaping the added turtleback foam, I Fein saw cut the aft edges of the canopy at the longerons.  Here’s the left side, but I forgot to grab a shot of it on the right side before I reglassed the added foam piece.

I also took a few minutes to dig out the foam in the mouse holes on one of the 3 strake ribs that I left out of the last haul to NC.  I’ll try to knock these out as I go about my other build tasks so they’re ready when it comes time to build the strakes in the next 2-3 months.

I also took a little bit of time to take the long sanding board and really finalize the shape of both the flocro transition for the added Balsa wood strips on the aft nose cover, as well as the intersection of the “old” nose sidewalls and the new foam I just recently added to make up the forward nose sidewalls.

[I have some slight “shoulders” on the nose sides right where I added in the new PVC foam when creating the top nose structure.  I sanded these for a bit but I think I have to accept the fact that since I left my original nose sidewalls a bit high and with a vertical surface, that the nose then somewhat sharply transitions into the top curve… this makes for a somewhat abrupt change at the nose sides from curved (top) to vertical (side).  So although curved, it’s not as smooth as I would want.  A minor issue, as I think it has zero affect on nose structure strength or aerodynamics, and I suspect not highly noticeable when the nose is finished to paint.]

Here are some closer up shots of the flocro transitions between the edge of the added Balsa wood and the front/side areas of the aft nose cover.  To be clear, the height of the front edge of the balsa wood was about 1/32″ when I applied this flocro, so there is not a ton of added flocro added here.

Tomorrow I plan on actually cutting the turtleback to separate the aft canopy frame and then remove the canopy from the fuselage to begin canopy internal shaping & glassing.

 

Chapter 18 – Canopy Tweaks

The external canopy layup has passed the 48 hour mark for curing, but before I pop the canopy off the fuselage to shape and glass the inside I need to contend with one of two issues involving the turtleback (aka turtledeck, D-Deck, etc.).

The issue that I’m not contending with today is the profile angle between the turtleback and canopy.  I’ll deal with that once the upper cowling is mounted and I know the exact angle I’m dealing with.

In regards to the other issue, as you may be able to see below –which coincidently I clearly DID NOT/COULD NOT see before I glassed the canopy frame– is that the turtledeck is a bit curvier on the left side, a bit flatter on the right side and a bit deflated on the upper right side.  This all comes down to one thing really:   Sins of the past.

With my fuselage being slightly askew, although virtually imperceptible to the naked (or unaware) eye, it seemingly took its toll on the aft canopy to turtleback interface . . . although I tried (in vain) to mitigate it as best possible before glassing.

A sideline issue that may actually help mitigate the issue above is that the vertical seams between the turtleback and canopy are at different Fuselage Stations, with the right side corner being about 3/8″ aft of the left side.  This should actually help my mitigation actions (note that I’m not saying “fix” actions because I think the configuration is such that I should be able to mitigate the turtleback imbalance to a good degree, but not eliminate it altogether) since it will give me more space forward for another layup that I will add to this structure.

Yes, it may be hard to tell, but underneath that strap and all those boards and wedges is a 1/4″ thick piece of PVC foam that I will sand and shape down to fill in the low spots on the right side turtleback.

Here’s a closer shot . . . Again, there will be no way to completely eliminate the offset of the turtleback without redoing the entire canopy install (that is NOT going to happen!), but I am cautiously optimistic that this will help balance it out to a good degree.

With the aft extra foam piece in place, I then spent about 45 min marking and trimming the overhanging glass from the sides of the canopy, starting on the right side first.

I then did the same on the left.  The edge will most certainly require more work before final canopy install, but so far it’s looking pretty good.

I then spent some time cleaning up the intersection between the canopy front skirt edge and the aft edge of the nose cover.  Again, this is the rough start to this process, but so far the lines are looking pretty good and the elevation glass-wise will be very close between the two structures once I get a ply of BID on the aft nose cover (which I now plan to do after I remove the canopy from the fuselage).  I also took about 15 minutes to sand down the flocro transition around the Balsa wood on the aft nose cover.

Tomorrow I’ll sand and shape the foam I added to the right side turtleback to (hopefully) create a better turtleback transition that balances with the left side.  I then plan on laying up 2 plies of BID on the new turtleback foam.  Once that cures I plan on cutting the turtleback-canopy split line and then removing the canopy from the fuselage (after I build a wood frame around the canopy to support the it inverted and off the fuselage).  I also plan on laying up the final ply of BID on the aft nose cover.

 

Chapter 18 – Canopy layup cleanup

Today was a cleanup day for last night’s external canopy layups.

I started by pulling the peel ply and cleaning up the seam areas of the peel ply.

I then pulled the edge tape off the canopy that last night’s laid up glass butted up against…. and a number of times over.

I then spent the next 3+ hours very carefully cutting away overhanging glass off the canopy edge at the canopy to frame intersections, while also removing any trapped and/or extraneous protective tape.

It took a while, and is a bit nerve-racking work since you have to be close up to the canopy surface with a sharp razor knife to extract the dead glass and tape.  I’m pleased to report that besides a few very, very minor scratches I made with the knife, the job came off without any major casualties (except my fingers of course!).

A little while later –curious to see how the canopy looked!– I pulled the protective plastic off the canopy to take a peek.

I have to say, barring any aft canopy issues that I may have, I am very, very pleased with the size and shape of this canopy.

Again, except for the slightly off center shaped turtledeck and it’s angle with the canopy, I am so far very pleased with the canopy install into the canopy frame.

This shot gives you a good idea of how it will look once the plane is finished.

And the requisite nose shot of course!

A profile view . . .

And one more slightly down angled side shot.

I also grabbed a couple shots of the GIB headrest and the internal turtleback from each side.

Again, with the canopy still in its 48 hour cure tomorrow, and with the canopy cleaned up as much as it can be, tomorrow will be a working-on-the-house day for me!

 

Chapter 18 – Canopy glassed

I started off today spending over 4 hours prepping the canopy frame for glass.

Part of that prep was marking and sanding a 3″ wide depression in the aft canopy frame for a strip of 3″ wide UNI tape, the same that is used for the spar caps.

I then did a rough cut of the 3″ wide UNI tape.

I was going to take a pic of only the UNI tape laid up but I was on the phone and forgot, so here’s a shot of the laid up 3″ wide UNI tape with 1 ply of BID laid up over it and the rest of the turtleback.

After the above shenanigans, I then spent another 8 hours laying up all the external canopy fiberglass following the plans layup schedule.  I then peel plied the layups.

Here’s the aft side of the canopy frame glassed as per plans, with of course 1 extra strip of 3″ wide UNI tape.  To keep the aft canopy from spreading I will add 2 plies of the 3″ UNI tape on the inside of the canopy frame as well.

Now, my canopy is a tale of 2 canopies …. I am extremely happy with the front half of the canopy, the skirt and the interface with the aft nose cover.  Unfortunately, due my slightly asymmetrical “D” shaped fuselage, coupled with a huge oversized canopy, the turtleback is a bit off kilter.  It is simply fatter on the left side than it is the right.  My neighbor, who has a really good eye for detail, had a hard time noticing it standing aft of the plane looking at it, but as with anything, once you see it you can’t “un-see” it!

Then there’s the issue with the turtleback and aft canopy intersection angle.  It is clearly a bit severe and I’ll need to ponder some on fix actions for that.  In talking with Mike Beasley in prepping to construct the canopy, he said to ensure that the line forward of the firewall maintains the upper cowling profile.  Moreover, Mike stated that if the canopy profile and cowling profile didn’t agree, then the turtleback profile should match the cowling, not the canopy.  Thus, as you can see, this is the predicament I find myself in . . . and not caring much for being in predicaments, I look forward to the day when I am not finding myself in one canopy & turtleback wise!!

I will probably pull the peel and clean up around the edge of the canopy where it intersects the glass tomorrow, but beyond that –while the canopy does its 48 hour cure thing– I will be attending to house stuff in prepping my place to sell.

Chapter 18 – Canopy frame shaped

Today was all about shaping the canopy frame.

I started off by shaping 4 separate foam blocks for the canopy’s front skirt.  I then used micro and “pour-in-place” foam to keep them all in place.  I most likely would not have used the “pour-in-place” foam except that my underside contours of the canopy front skirt and glare shield/aft nose cover interfaces were a bit sloppy and had some significant gaps present.  Yep, the side-to-side, front-to-back, and up-and-down contours and shapes of the glare shield definitely presented some challenges.

So, I punted and just used pour foam both as a shaping mechanism for the underside of the front canopy skirt (fingers crossed!) and also the bonding agent for two front corner pieces and the very front CL seam of the 2 inboard foam pieces.

As you can see, I then had to weigh down the foam to keep it in place since the expanding “pour-in-place” foam required a bit of tamping down.

Here we have a side view of the canopy skirt front foam pieces weighed down in place.  To be clear, there is micro securing the center pieces to the canopy, each other and to the foam pieces aft of this very front row of foam blocks.

While the canopy front skirt foam pieces cured I then got to work on cleaning up and shaping the foam that makes up the turtleback.  I took my time as to not jack anything up, and got the aft canopy frame and turtleback to about 70-80% of its final state.

With the “pour-in-place” foam and micro that secures the foam pieces at the front side of the canopy cured, I then removed the weights and got to work.

I started by shaping the right side first, starting at the front and working my way aft along the right side canopy rail.

Here is the right front canopy skirt and right side canopy rail nearly sanded to its final shape.

After a fair amount more sanding and tweaking the shape, I finally got both the right and left foam canopy frame shaped.

Here’s a shot of the shaped aft right side canopy frame.

And a shot of the shaped left side canopy frame.

And let’s not forget the turtleback on the left side!

Here we have a head on view of the freshly shaped canopy frame.

And a bit closer view.

Shaping and adding the final canopy skirt foam blocks into place and shaping the canopy frame took a bit longer than I expected.  I would have pressed on to glass the canopy if I didn’t have to take my truck into the shop early tomorrow AM.  So, I’m going to stop my canopy build here for the evening and press on tomorrow to get this baby glassed!

 

Chapter 18 – Canopy front skirt

I’m dealing with a repair issue on my truck that took up a number of hours both yesterday and today, so I didn’t get as much shop work in as I would have liked on the canopy today.  I did get a few hours in though.

I started by cutting the glare shield’s aft edge trim/seal to length.  I also tapered the ends so that it flows in nicely at the outboard edges.

[Note the very outboard edge of the glare shield that is situated immediately over the longeron, this is discussed below].

Here’s a shot of the right side cut/tapered aft edge trim/seal of the glare shield.

I then covered the trim/seal with painters tape to protect it from getting gummed up by the duct tape.

I then applied a couple layers of protective duct tape over the glare shield.  After I got the tape on I realized I hadn’t (re)trimmed the very outboard edges of the aft nose cover, along side the glare shield.  These ends are immediately over the longerons and for the canopy frame to be shaped properly they needed to be trimmed in width . . . or at least very close to their final width.

So I peeled back the tape on each side and, using the Fein saw, trimmed off about 0.1″ of the very outboard edge of the glare shield in between the taped in 1/8″ aluminum spacer for the canopy and the aft outboard edge of the Balsa wood on the aft nose cover (no pics on this trimming).

I then laid the tape back down in place.

A side shot of the taped up glare shield…. with the aft edge trim/seal in place.

I then spent about 45 minutes measuring and shaping a block of foam for the center section of the canopy front skirt.  I’ll get a shot of that tomorrow with the plan being to finish up the canopy skirt/frame foam, and then get the canopy frame shaped and glassed.

 

Chapter 13/18/23 – Glare shield trim

In prep for getting the canopy install much farther along than it currently is in order to haul the fuselage down to North Carolina, I measured, researched and then ordered some black trim for the aft vertical edge of the glare shield.  The trim will serve two purposes:

  1. Keep from slicing open body parts that come in contact with the rather sharp edge.
  2. Compress slightly into a groove on the bottom of the canopy skirt to guard against incoming rain and moisture, wicking it to the outer edges of the glare shield/canopy.

I ordered the trim from McMaster-Carr a few days ago and it came in today.  I have to say I’m quite pleased with both the fit and the look of the trim.

Here’s a bit closer look.  When the airplane is finished to paint, the current green area of the glare shield will be a flat black, whereas the Balsa wood area will be painted whatever color the nose and canopy frame is painted (haven’t decided yet . . .).

I also received yet another L12 micro-linear actuator that I’ll be using to manipulate louvers that will cover the oil cooler to adjust the airflow for optimized oil cooling temps: louvers closer to closed in the winter for less engine oil cooling and pretty much wide open during the hot summers, with stages in-between during the fall and spring.

The switch that I also bought from the Robot Shop is a latching type switch (analogous in function to a latching relay) that will allow a simple actuator to be stopped at discreet positions –versus just merely fully opened or fully closed– to allow for a myriad of settings to dial in the oil cooler to temp during flight ops versus having to mess around with making, sizing and attaching oil cover plates on the ground.

As a point of note, I got the louver idea from Marc Zeitlin who incorporated this simple mod on his Cozy IV with great results.  The main difference in my configuration vs Marc’s is that Marc incorporated a cable to manipulate the louvers whereas I will be using a significantly lighter micro-linear actuator.

I’ve been painting the house all week with the phenomenal help of Stacey from North Carolina.  It’s been a very productive week but I am quite tired, so after taking just a bit to recharge I’ll be back on the canopy build for the next 2-3 days (interspersed with some house prepping tasks of course).