Started drilling and setting the leading edge to the ribs/spar. Here are some pictures of the progress.
I start my measuring and drilling the hole nearest to the spar (first pic) then measure out the remaining eight holes using a rivet spacing tool and square to draw a line and mark the locations. Seems to be working out okay. Measure twice - drill once is the mantra.
About two hours work for the first two ribs. Of course I have been taking my time and the remaining ones should go a bit quicker. Now that I have the mark, measure, drill, process figured out.
Thanks for checking in -
Greg.
Tuesday, September 17, 2013
Thursday, September 5, 2013
Should I Re-do My Leading Edge Bend???
A bit of a pickle here. I noticed my leading edge skin has a little "buckling" in the bend on the bottom side. I don't think this is a problem. It is a bit ugly. How does this impact the aerodynamics? I'm not sure. I will get some input from the CX4 Builders Group to see what they think. I guess for aesthetics it should be trashed and redone. But then I've wasted a big chunk of costly .020 6061-T6 aluminum.
Anyone out there have any ideas or recommendations?
Anyone out there have any ideas or recommendations?
Does this call for a new bend? I tried to push the dimple out but it didn't work.
Going to delay drilling and riveting the skin until I can check with the designer and other builders to see if this is a problem or not.
Darn!
Greg.
Update - 9/10/13 - I asked Dave Thatcher (CX4 Designer) and he said "no problem - Just hit it with some bondo and it will be fine" I may just do that. Thanks Dave.
Wednesday, September 4, 2013
Marking Skin for Rivets - Measure Twice, Drill Once (or maybe measure more?)
Marking the rivet holes for the inboard leading edge rib. Measuring per plans for 1.5" spacing I can only get eight (08) holes on a rib. Hmmmm. All the pictures I have seen and the plans show nine holes...
Here is my initial marking for the rivet positions at 1.5" spacing
That's marked on the center of the rib flange from just within the trailing edge to the leading edge end of the rib. With the 1.5" spacing I can only get eight holes. Is that enough? On the plans the rivet locations indicate nine locations:
Here is my initial marking for the rivet positions at 1.5" spacing
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| Setting the 1.5" spacing with the rivet placement tool |
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| Plan clearly shows nine rivets on the top flange and eight on the bottom |
I checked the plan and the first rivet location (at the spar) is just inside the trailing edge of the rib. The second rivet location measures about 3/4" from the first. Then they are evenly spaced at 1.5". Even allowing for the 3/4" space between the first two holes I can only get eight. I think the best thing I can do to meet the nine rivet requirement is to adjust the space between the rivets. Maybe making the space 1.25" instead of 1.5" will work? I'll try that and get back to you...
Thanks for checking in -
Greg.
Sunday, September 1, 2013
Leading Edge Bending and Attachment
August 31 - Saturday
Spent a couple of hours preparing and then bending the left wing leading edge. Used an 8' 2x4 to do the bend just like the instructions said. Thought I was going to need help doing it. I was able to do the bend and it was pretty easy. I just used the 2x4 to press down on the sheet I cut to make the bend. I then clamped and strapped the leading edge skin to the spar/rib structure.
Pressing the skin onto the ribs after making the bend. I first just pressed down on the sheet without the rib/spar structure to the initial fold/bend. Then I placed the rib/spar structure into the skin and squared it.
Here I clamped the skin to the leading edge.
Spent a couple of hours preparing and then bending the left wing leading edge. Used an 8' 2x4 to do the bend just like the instructions said. Thought I was going to need help doing it. I was able to do the bend and it was pretty easy. I just used the 2x4 to press down on the sheet I cut to make the bend. I then clamped and strapped the leading edge skin to the spar/rib structure.
Now I have to line up and mark the skin for initial drilling. Then match up the ribs to the holes and cleco in place. Will try to get that started tomorrow.
Thanks for checking in -
Greg.
Monday, August 26, 2013
Progress on the Wing
Progress is being made - slow but steady at this point. I had to clear off the work table and unroll a 12' x 4' sheet of .020 6061-T6 to mark and cut the leading edge skin for the right wing.
Made the first cut. 28" from edge and the second cut 90" long in the sheet. You can see it marked out in these pictures. I used hand shears to do the cut. They worked okay. Have to take your time to keep a straight cut. When cutting the .040 sheet for the wing spar webs I used a hand-held electric jig saw. But with this thinner stock I figured the shears would do better.
It wasn't that bad cutting with these shears. Next I have to bend the leading edge. Mr. Thatcher recommends using a 2x4 and bending the skin to within 3/4" of the surface to get the proper radius. I'll probably get some help with the bend. Think it may be easier with two people.
I will update with the bending process when we get to it.
Thanks for checking in -
Greg.
Oh, BTW - It was a REALLY nice day Sunday. So I went flying - Can you blame me??
Made the first cut. 28" from edge and the second cut 90" long in the sheet. You can see it marked out in these pictures. I used hand shears to do the cut. They worked okay. Have to take your time to keep a straight cut. When cutting the .040 sheet for the wing spar webs I used a hand-held electric jig saw. But with this thinner stock I figured the shears would do better.
It wasn't that bad cutting with these shears. Next I have to bend the leading edge. Mr. Thatcher recommends using a 2x4 and bending the skin to within 3/4" of the surface to get the proper radius. I'll probably get some help with the bend. Think it may be easier with two people.
I will update with the bending process when we get to it.
Thanks for checking in -
Greg.
Oh, BTW - It was a REALLY nice day Sunday. So I went flying - Can you blame me??
Saturday, August 17, 2013
Nose Ribs on right wing
Using a Dremel 90 degree attachment I was able to drill then rivet the nose ribs to the right wing spar today. With able assistance from my son we finished attaching the ribs.
Drilling the holes
Here is a view of the leading edge (nose) ribs attached to the right spar. I know, it's on top of my car. I did that for lighting. And to show off the construction to my family. It is very rewarding to start seeing a structure taking form. Thanks to my oldest son Greg for his help and the use of his variable speed Dremel tool.
Wednesday, August 14, 2013
Rib Drilling Update
I was able to get the Dremel 90 degree attachment and drill chuck. Recommendations from the CX4 User Group gave me this option for drilling rib holes to vertical angles on the wing spar. I tried to drill using my on speed Dremel tool that turns at about 30,000 RPM. That is a little fast and hard to control the drill. Hit the switch on the Dremel tool and it immediately whirls up to that high RPM leaving no room for error when starting to drill. So, I have to either get a variable speed Dremel tool or borrow one. Given the price of almost $80 for a variable speed Dremel it makes more sense to borrow one. More delays...
Here is the 90 degree attachment from Dremel:
Here is the 90 degree attachment from Dremel:
Dremel 90 Degree Attachment and drill chuck below.
Just contacted my Son. He has a variable speed Dremel tool! YES! Maybe we can get drilling this weekend. I will update then.
Thanks for checking n -
Greg.
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