Pietenpol-List Digest Archive

Tue 03/26/13


Total Messages Posted: 9



Today's Message Index:
----------------------
 
     1. 04:39 AM - Re: Steve from Owings, MD (chase143(at)aol.com)
     2. 09:24 AM - Glue and Varnish Test (dgaldrich)
     3. 10:26 AM - Re: Glue and Varnish Test (John Francis)
     4. 11:51 AM - Re: Glue and Varnish Test (biplan53)
     5. 01:09 PM - Re: Glue and Varnish Test (tools)
     6. 07:08 PM - Re: Glue and Varnish Test (dgaldrich)
     7. 07:34 PM - Re: Glue and Varnish Test (tools)
     8. 09:09 PM - Cable Symmetry (John Woods)
     9. 09:13 PM - Re: Saturday afternoon patrol (taildrags)
 
 
 


Message 1


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    Time: 04:39:58 AM PST US
    Subject: Re: Steve from Owings, MD
    From: "chase143(at)aol.com" <chase143@aol.com>
    Hello Axel, Wow, thank for the kind words. We've met you a few times over the years, and I am very glad you will be there again this year, in one piece (give or take a few pins) ;-). Hope your new project is coming along! Regards, Steve -------- Steve www.mypiet.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397073#397073


    Message 2


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    Time: 09:24:46 AM PST US
    Subject: Glue and Varnish Test
    From: "dgaldrich" <dgaldrich@embarqmail.com>
    Several days ago, I revealed that I had "dunked" my ribs in varnish. Someone pointed out that the varnish might pose a problem with future glue. In order to determine whether I'd have to sand all the nose portions of the ribs, I did an experiment, or rather two. I had some turtle deck stringers that were varnished and almost 1/4 inch thick -- .220-.245 inch -- that were laying around so I ripped them into 1/2 inch pseudo cap strips and glued 6 inches of them to a piece of 1/4 okoume plywood. That length was chosen to approximate the amount of rib that would be glued to the plywood leading edge. Since I had some mixed up, I used West System epoxy as well as T-88. Glued 3 each for a total of 6. Also had some douglas fir that was approximately .285 thick so I ripped some of that into 1/2 inch strips and also glued them to the same piece of 1/4. After the glue had cured for 24 hours, I marked the sticks at 6 inches out from the plywood, put the plywood in a vice and hung a water bucket at the 6 inch mark. I chose this particular test, rather than a tension or compression arrangement with the thought that the primary strain on the glue joint would be a side load on the nose part of the rib where it's nominally glued to the leading edge plywood. After hanging the water bucket on the cap strip, I added water to it until the wood or joint failed and then weighed the bucket on a bathroom scale. Did it for the twelve samples and the results are pictured below. ALL of the test pieces failed in the same manner. They all broke at the "hinge" point where the cap strip met the plywood. NONE of the glue joints failed. Conclusion: Since this was more of a qualitative experiment than a serious quantitative one, the primary one that I reached is that a T-88/West System glue joint with varnished wood is strong enough for the intended purpose and I don't have to sand off my ribs. Observations: The Douglas fir pieces were approximately 25 percent thicker than the Sitka and yet failed at an average of 70 percent higher load. This lends credence to the AC 43-13 note that Douglas is stronger and those that use it could probably use slightly thinner longerons and diagonals in the fuselage. Notes: This test was for ONE failure mode and the data samples were not tightly grouped so the quantitative reliability is not very accurate and any calculations should be based on much more rigorous testing. Since the glue joints did not fail, this is confirmation that West System is suitable for at least this sort of application. Pictures: Glue 1 is the board before testing. Glue 2 is the varnished pieces after failure. Glue 3 is the Douglas fir pieces after failure. The numbers are the weights at failure. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397093#397093 Attachments: http://forums.matronics.com//files/glue_3_734.jpg http://forums.matronics.com//files/glue_2_176.jpg http://forums.matronics.com//files/glue_1_717.jpg


    Message 3


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    Time: 10:26:25 AM PST US
    Subject: Re: Glue and Varnish Test
    From: "John Francis" <Mrkringles@msn.com>
    I believe it would be a mistake to proceed with your project based on these results. My understanding is that although a strong bond may appear to have been made, the epoxy has adhered to the varnish and not the wood. Varnish will eventually break down as the moisture content of your wood changes seasonally and the wood expands and contracts because of it. Time will weaken the joint. Have you checked with the manufacturer about these tests? John -------- John Francis Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397110#397110


    Message 4


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    Time: 11:51:58 AM PST US
    Subject: Re: Glue and Varnish Test
    From: "biplan53" <biplan53@hotmail.com>
    I just read in the Bible(Tony's books) not to get ahead of game and varnish anything to be glued later. I am not trying to be a rain cloud but I trust someone who has been there and done that. -------- Building steel fuselage aircamper. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397116#397116


    Message 5


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    Time: 01:09:11 PM PST US
    Subject: Re: Glue and Varnish Test
    From: "tools" <n0kkj@yahoo.com>
    What needs to be glued to the ribs after you have varnished them? The leading edge sheeting or the leading edge itself? I can't see any reason why you would have a problem. I'd sand any portion of the rib that needs glued for some key, and then wouldn't worry about it. My dad dipped all his ribs just like you did on his Hatz, no problems. It's a similar wing. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397128#397128


    Message 6


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    Time: 07:08:38 PM PST US
    Subject: Re: Glue and Varnish Test
    From: "dgaldrich" <dgaldrich@embarqmail.com>
    I forgot to mention that the varnish on the wood was 12 years old and was taken from a previously flying airplane. With a great deal of difficulty, I pried off the pieces that remained on the plywood. None exhibited the failure mode you're describing. I've redone some 90 year old varnished furniture (I grant you not SPAR varnish) that was not giving up without a serious fight. The point is properly applied varnish of most any kind is a b++++ to get off. I think for use on the leading edge plywood, this is not an unreasonable test. This ends up being a low stress joint in any event due to: 1) the fact that all the ribs will be held parallel by a combination of the drag/antidrag wires and the fabric rib lacing and 2) there is very little, if any, "side load" from aerodynamic forces. As a reference to the amount of stress on leading edge fairing, take a look at Aeronca Chiefs and Champs. Their leading edges are .016 or .020 aluminum held on by a relatively small number of short wood screws. Please note that I am NOT recommending using varnish under glue for anything structural. What I am suggesting is that the dunking technique DOES insure that the entire rib, even the nooks and crannies behind the gussets, is varnished and protected from moisture. The "conventional wisdom" that you can't or shouldn't use glue on varnished surfaces may NOT apply to this specific kind of stress with these specific epoxies. That's what experimentation is for and why I offered this data. Dave Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397149#397149


    Message 7


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    Time: 07:34:32 PM PST US
    Subject: Re: Glue and Varnish Test
    From: "tools" <n0kkj@yahoo.com>
    I agree with you. Epoxy is recommended to glue all sorts of non porous things together, don't know why wood with the grain sealed would be any different. Key is the key, needs to be sanded some is all. I've never seen varnish release due to seasonal movement. I do believe some very old varnishes eventually oxidize to the point they flake off, just like the paint on old machines. Varnish being spar or not shouldn't have anything to do with it's ability to hold either, spar varnish means that it's got UV inhibitors is all. I like the idea of dipping the ribs because of the difficulty of ensuring you've painted all the surfaces. It's EASY to miss places. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397151#397151


    Message 8


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    Time: 09:09:10 PM PST US
    From: John Woods <johnwoods@westnet.com.au>
    Subject: Cable Symmetry
    Hi Steve from Owings, I just had a look through your construction web site (www.mypiet.com) and it is full of great detail. The one which caught my eye was the Cable Configuration Thoughts and in particular the slides showing the elevator cable configurations. I must agree with you that Setup B is the one to aim for to avoid those loose cables we hear about on flying examples. The key there is ensuring that from the control column all the way to the control horns, everything is symmetrical. By symmetrical, I mean in the neutral position, the control column, idler bar and control horns are vertical or at the same angle from vertical AND the cable connection points on each of those items are equidistant from the pivot point. By equidistant I don't mean that all three items have to have the cable attached at the same measurement, they can be different, but for each item the cable should be the same measurement from the pivot point. Does that make sense? This is why setup B works. The same would apply to all the cable controlled surfaces. Symmetry is good! When moving things are symmetrical, they move together in harmony and all is good. Hope this information is found to be useful. Best regards, John Woods Perth, Western Australia


    Message 9


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    Time: 09:13:07 PM PST US
    Subject: Re: Saturday afternoon patrol
    From: "taildrags" <taildrags@hotmail.com>
    We ARE going to get that airplane onto the cover of a national publication! It's a beauty. -------- Oscar Zuniga Medford, OR Air Camper NX41CC &quot;Scout&quot; A75 power Read this topic online here: http://forums.matronics.com/viewtopic.php?p=397155#397155




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