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I was reading some information on Fisher Celebrity builders websites
and saw that one builder did not like the idea of glueing the fabric to the ribs as per the plans. The ribs on the Celebrity are very thin and he didn't think there was enough glue area for a satisfactory bond, so he rib stitched. I also recall reading somewhere that the glue area doesn't really affect the strength of the bond between the fabric and wood rib ( which I can't believe ) I know the wing loading of the Celebrity is low compared to some of the more high performance bipes, but if the glue area is such a concern, wouldn't it be OK to just increase the rib capstrip width slightly to give more glueing area? Might only increase the whole airplane weight half a pound. Thoughts? Thanks Neal |
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#3
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#4
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In article ,
Stealth Pilot wrote: btw dont be beguiled by the semantics. the glue strength doesnt change with the glue area since it is a force per unit area measurement. the glue area directly changes the amount of total force that the rib fabric join can stand. a pound per square inch strength applied to a square inch can hold a pound a pound per square inch strength applied over a square foot can hold one hundred and fourty four pounds. Stealth Pilot Australia I'll bite into this topic from an intellectual curiosity perspective. What are the forces acting on a rag plane that would tug against the rib bond? Source? Direction? Magnitude? How common are such bond failures? What is the cause? Poor surface prep or other application shortcomings? Deterioration of the glue or fabric over time? Other? If I take a 3" long piece of tape and stick it on my desk, and a 12" long piece and stick it next to it, does it take more force to peel the longer one, or just more time? I'd say a wider one would stick more assertively, but not a longer one. Is this at all analogous to what's going on in an airplane, or way off? Has this been studied like wing loading, with safety margins built in? Does an airplane fall out of the sky if the fabric starts letting go? I guess eventually it would, if pieces started tearing and departing the airplane. That would disrupt the airflow, I imagine. There was a discussion of punch testing a short time back. Is there also a "pull test" to see whether the glue bonds are getting ready to fail? These are the things that I think about while I struggle valiantly to smash two rivets to the same shape and size. |
#5
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It might be like that old rag-top car we've seen tooling down the highway
with the fabric ballooning away from the metal top when the adhesive gave way. The altered profile might change the lift characteristics of the wing to some degree I suspect. I read somewhere that anything above 75 should be rib stitched, but I'm no engineer. wrote in message oups.com... I was reading some information on Fisher Celebrity builders websites and saw that one builder did not like the idea of glueing the fabric to the ribs as per the plans. The ribs on the Celebrity are very thin and he didn't think there was enough glue area for a satisfactory bond, so he rib stitched. I also recall reading somewhere that the glue area doesn't really affect the strength of the bond between the fabric and wood rib ( which I can't believe ) I know the wing loading of the Celebrity is low compared to some of the more high performance bipes, but if the glue area is such a concern, wouldn't it be OK to just increase the rib capstrip width slightly to give more glueing area? Might only increase the whole airplane weight half a pound. Thoughts? Thanks Neal |
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#7
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![]() "Stan Premo" wrote in message ... It might be like that old rag-top car we've seen tooling down the highway with the fabric ballooning away from the metal top when the adhesive gave way. The altered profile might change the lift characteristics of the wing to some degree I suspect. The fabric lifting off the top of the wing can, and has killed people. This is still not to say that it has to be stitched. If loads on the surface are low enough that the correctly glued fabric stays place, then all is well. Just make sure the correct techniques are used, and that loads are low enough! -- Jim in NC |
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Morgans wrote:
It might be like that old rag-top car we've seen tooling down the highway with the fabric ballooning away from the metal top when the adhesive gave way. The altered profile might change the lift characteristics of the wing snip The fabric lifting off the top of the wing can, and has killed people. This is still not to say that it has to be stitched. If loads on the surface are low enough that the correctly glued fabric stays place, then all is well. Just make sure the correct techniques are used, and that loads are low enough! What about the 3rd option from the Tony Bengals books, covering the wing with thin fiber glass cloth and resin? I know it would make it harder to inspect the condition of the wood years down the road (sky?) but it sounds like it would last longer in the first place. Tony |
#9
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![]() Anthony W wrote: Morgans wrote: It might be like that old rag-top car we've seen tooling down the highway with the fabric ballooning away from the metal top when the adhesive gave way. The altered profile might change the lift characteristics of the wing snip The fabric lifting off the top of the wing can, and has killed people. This is still not to say that it has to be stitched. If loads on the surface are low enough that the correctly glued fabric stays place, then all is well. Just make sure the correct techniques are used, and that loads are low enough! What about the 3rd option from the Tony Bengals books, covering the wing with thin fiber glass cloth and resin? Just in case anyone wants to find his books its _Tony Bingelis. Fiberglass wings are not fabric wings. You might as well say, hey, why not cover them with aluminum sheet metal. Also, I _think_ fiberglass wings will be heavier. -- FF |
#10
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Thread | Thread Starter | Forum | Replies | Last Post |
Any Info on Hipec? No Rib Stitching? | bling bling | Home Built | 5 | November 19th 03 09:24 PM |