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#1
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In Robert Little wrote:
very stable once it dries. Again, dope on cotton and linen has been used for the 50 years prior to the introduction of the newer fabrics. Yes, but both of those fabrics have built in shrinking ability and will continue to shrink as they age. How can you make fiberglass cloth shrink? Maybe I just don't understand enough about your process to get it. Do you have a website with technical information, or could you post an excerpt from the relevant part of your application manual? ---------------------------------------------------- Del Rawlins- Remove _kills_spammers_ to reply via email. Unofficial Bearhawk FAQ website: http://www.rawlinsbrothers.org/bhfaq/ |
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Del Rawlins wrote:
In Robert Little wrote: very stable once it dries. Again, dope on cotton and linen has been used for the 50 years prior to the introduction of the newer fabrics. Yes, but both of those fabrics have built in shrinking ability and will continue to shrink as they age. How can you make fiberglass cloth shrink? Maybe I just don't understand enough about your process to get it. Do you have a website with technical information, or could you post an excerpt from the relevant part of your application manual? ---------------------------------------------------- Del Rawlins- Remove _kills_spammers_ to reply via email. Unofficial Bearhawk FAQ website: http://www.rawlinsbrothers.org/bhfaq/ Del, Check the model airplane supply houses. You can find glass down to 1/2 ounce per yard. Butyrate shrinks quite a bit. Even the "non-taughtening" variety pulls up a bit. So a glass skin would rely on the coating for taughtness (not in the MS dictonary?) - just like linen does. |
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In Richard Lamb wrote:
Del Rawlins wrote: In Robert Little wrote: very stable once it dries. Again, dope on cotton and linen has been used for the 50 years prior to the introduction of the newer fabrics. Yes, but both of those fabrics have built in shrinking ability and will continue to shrink as they age. How can you make fiberglass cloth shrink? Maybe I just don't understand enough about your process to get it. Do you have a website with technical information, or could you post an excerpt from the relevant part of your application manual? Del, Check the model airplane supply houses. You can find glass down to 1/2 ounce per yard. I'm not sure what this has to do with the effects of cold weather on the glass cloth. I think you are confusing me with Ernest. Butyrate shrinks quite a bit. Even the "non-taughtening" variety pulls up a bit. So a glass skin would rely on the coating for taughtness (not in the MS dictonary?) - just like linen does. I thought that the natural fiber coverings like linen or cotton were primarily shrunk using water? I.E. they get most of their tautness from natural shrinkage as the water dries, prior to the coating being applied. Or am I all wet? I don't know a lot about fabric covering and am just trying to get a clear understanding of the various systems. ---------------------------------------------------- Del Rawlins- Remove _kills_spammers_ to reply via email. Unofficial Bearhawk FAQ website: http://www.rawlinsbrothers.org/bhfaq/ |
#4
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![]() "Del Rawlins" wrote in message ... In Richard Lamb wrote: Del Rawlins wrote: Butyrate shrinks quite a bit. Even the "non-taughtening" variety pulls up a bit. So a glass skin would rely on the coating for taughtness (not in the MS dictonary?) - just like linen does. I thought that the natural fiber coverings like linen or cotton were primarily shrunk using water? I.E. they get most of their tautness from natural shrinkage as the water dries, prior to the coating being applied. Or am I all wet? I don't know a lot about fabric covering and am just trying to get a clear understanding of the various systems. No, the water was just to take out the natural shrinkage of the fabric before putting in the artificial tautening that occurs from either the nitrate or butyrate dope. Either dope can tauten so much that with too much application they can actually crush the airframe. The dope grabs hold of each fiber and pulls the spaces between the fibers closer together. This is the tautening action achieved with using dope whether it is cotton, polyester or glass. And yes, you can find glass fabric in the model plane catalogs that can acheive similar results. We would be glad to send anyone our instruction manual for free if they will just send us their snail-mail address. I hope that I've sparked som interest in the alternatives available to the aircraft builders. One other thing, though. The use of epoxy or polyester resin combined with glass again starts the deterioration clock. The glass is permanent, but the resins are what age so quickly in the presense of UV radiation. Old fiberglass boats look rough after a few years and will burn like gasoline. The glass does not age and will be the big mess left after the fire since it does not burn. Our process doesn't use any resins as one usually assumes when glass is mentioned. The "temporary cellulose" base dope is used to fill and tauten only. It can burn off but the glass will remain in place with little to no loss of strength to the fabric. The late Bill Hale always used our fabric on his acrobatic aircraft due to the glass acting as a fire wall to the occupant. Many NASA experimental windmill and wind tunnel blades have been covered with our glass as well. ---------------------------------------------------- Del Rawlins- Remove _kills_spammers_ to reply via email. Unofficial Bearhawk FAQ website: http://www.rawlinsbrothers.org/bhfaq/ |
#5
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Robert Little wrote:
One other thing, though. The use of epoxy or polyester resin combined with glass again starts the deterioration clock. The glass is permanent, but the resins are what age so quickly in the presense of UV radiation. Old fiberglass boats look rough after a few years and will burn like gasoline. The glass does not age and will be the big mess left after the fire since it does not burn. Our process doesn't use any resins as one usually assumes when glass is mentioned. The "temporary cellulose" base dope is used to fill and tauten only. It can burn off but the glass will remain in place with little to no loss of strength to the fabric. The late Bill Hale always used our fabric on his acrobatic aircraft due to the glass acting as a fire wall to the occupant. Many NASA experimental windmill and wind tunnel blades have been covered with our glass as well. Robert, you're starting to sound like a very bad salesman, creating dark ghost where everyone else sees daylight. Epoxy is not a vampire that burst into a cloud of dust if the blinds are raised. In fact, the proper formulation can sit in the sun for years without measurable effects. I personally plan to take the very unusual step of painting my airplane to keep it from rotting away in the sun. Where are these people who don't paint their aiplanes after having paid to get them covered? Furthermore, if my elevons catch on fire then I will have been burned to death long before. A quick look at the Delta planform will explain why. But this begs the question of, "If the FG can take the forces and stresses of flight without the butyrate without excessive deformation, then what is the point of the butyrate?" Didn't you say the glass was glued on with the butyrate? If it's not necessary, why not just tie on the FG cloth, spray a coat of paint or two, and go flying? That is not a redundant question or a taunt. I am really trying to understand the role each of the parts play in your system. I want enough information to know if I can apply your product, or a variant of your product, to my situation. I have a firewall already, and I don't need a windmill or wind tunnel. I need a very light elevon. On a more serious note, I think I called you Richard in another post. Do you have practice kits available? -- http://www.ernest.isa-geek.org/ "Ignorance is mankinds normal state, alleviated by information and experience." Veeduber |
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Richard Lamb wrote:
Butyrate shrinks quite a bit. Even the "non-taughtening" variety pulls up a bit. So a glass skin would rely on the coating for taughtness (not in the MS dictonary?) - just like linen does. If this is the case, and please note that I'm not saying it isn't, then the fabric in flight will be getting it's strength from only the butyrate until it is stretched enough to engage the fabric. Up until that point, the fabric is just a filler holding the butyrate together. It would then follow that the FG/butyrate system would experience more deflection in light use, even though it has a higher utltimate strength, because the polyester based systems would engage the stronger fabric earlier in the defelection. Does this actually occur, and do you have to account for it by choosing a paint system that will accept the stretching from the deflection? -- http://www.ernest.isa-geek.org/ "Ignorance is mankinds normal state, alleviated by information and experience." Veeduber |
#7
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On Thu, 15 Apr 2004 13:52:47 GMT, Ernest Christley
wrote: Richard Lamb wrote: Butyrate shrinks quite a bit. Even the "non-taughtening" variety pulls up a bit. So a glass skin would rely on the coating for taughtness (not in the MS dictonary?) - just like linen does. If this is the case, and please note that I'm not saying it isn't, then the fabric in flight will be getting it's strength from only the butyrate until it is stretched enough to engage the fabric. Up until that point, the fabric is just a filler holding the butyrate together. It would then follow that the FG/butyrate system would experience more deflection in light use, even though it has a higher utltimate strength, because the polyester based systems would engage the stronger fabric earlier in the defelection. Does this actually occur, and do you have to account for it by choosing a paint system that will accept the stretching from the deflection? Ernest, did you miss this post by Robert Little? See below, it explains how taught the fabric is. Corky Scott Many of you have some ideas about glass fabric that may or may not be valid. First of all, I own the RAZORBACK FABRIC Company. The company started in 50's and the FAA signed a letter in 60's that deemed our glass covering as a permanent covering that no longer needed testing as all other fabrics do on certified airframes do. This is due to the fact that all hydrocarbon based material deteriorate in the presents of UV radiation. It is true that our fabric is heavier than the choices that are now available. It was originally designed for agricultural aircraft, Stearmen to be exact. It weighs 3.6 oz. and uses less dope than Grade A cotton that weighs 4 oz. So technically, it weighs 17% less than the original fabric on J-3s, BC-12s, and etc. So with 35 yards for a average project, the total weight difference from a temporary dacron fabric of 2.4 oz per yard and the less expensive, but 200% stronger, permanent glass fabric system doesn't add up to all the negative talk about weight to the economists. As in a poorly installed rivet, I supposed our glass could frett. Our shop is dedicated to repairing and recovering frieght aircraft and so far, I have never seen this ocurrance. I have seen poorly installed fabric wear away the aluminum, though. It is much harder than aluminum and steel and care should be taken to protect the rivet and etc. with anti-shafing tape, as with any fabric installation. Once installed correctly, it has a much stiffer surface than the more flexible and stretchy dacron. I have seen many pictures on the covers of aviation magazines that show the top of the wing with pillows deforming between the ribs as the fabric stretches under the aerodynamic load of flight. Properly installed glass fabric does not stretch and will remain closer to the profile of the ribs than any other covering short of metal. Many of our customers comment that our fabric has gained them real increases in airspeed beyond the fact of being covered with a fresh finish. This also allows your paints to last longer as the flexing really stresses the surface coatings. Plus, you don't have the worry of falling through it if you should mis-step on a low wing. You can walk on it as long as the rib underneath it can handle the weight. By the way, since our fabric does not rot, deteriorate in acid rain and sunlight or even burns and is easily applied and repaired, it is still the only synthetic fabric that is authorized for use by our and other militaries. It is FAA-PMA'd, FAA-STC'd, MIL SPEC and ISO 9002 rated. Our biggest sales are still the military. Yes, C-130s and C-141 still have fabric on them and in them. We don't own chemical companies and we are not trying to corner the fabric market. But if you want a permanent awning, aircraft covering, or a firewall, you might want to find out more about RAZORBACK FABRICS, INC. Thank you for your time. Robert Little |
#9
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On Thu, 15 Apr 2004 19:00:06 GMT, Ernest Christley
wrote: wrote: Ernest, did you miss this post by Robert Little? See below, it explains how taught the fabric is. Corky Scott Once installed correctly, it has a much stiffer surface than the more flexible and stretchy dacron. I have seen many pictures on the covers of aviation magazines that show the top of the wing with pillows deforming between the ribs as the fabric stretches under the aerodynamic load of flight. Properly installed glass fabric does not stretch and will remain closer to the profile of the ribs than any other covering short of metal. Many of our customers comment that our fabric has gained them real increases in airspeed beyond the fact of being covered with a fresh finish. This also allows your paints to last longer as the flexing really stresses the surface coatings. Plus, you don't have the worry of falling through it if you should mis-step on a low wing. You can walk on it as long as the rib underneath it can handle the weight. Robert Little Guys, either I'm missing something here or I'm just not smart enough to get my mind wrapped around it. How is the FG stretched tight enough to make it stiff? Is the butyrate a hard substance once it dries/cure/whatever-butyrate-does? Is the following statement correct? If there is any looseness at all in the fabric, and it is pulled tight by the dope, then the dope is what will carry the stress, not the fabric. If the butyrate is carrying the stress, then would this system be any stronger that chopped strand composites? Yes. It is true. I do NOT know what I'm doing. But I will before I'm done! Ernest, it isn't the dope that provides the strength, not with Razorback fabric or with any fabric. The fabric itself is what gives the wing it's strength and/or stiffness against the wind. The initial application of the correct dope, in the case of the Razorback fabric, or a calibrated heating iron, in the case of the Polyfiber fabric, is what shrinks it. The application of paints on top of the fabric serve to protect it from UV rays, make it waterproof, and look nice, but do not add strength. You should participate in one of Ron Alexander's fabric covering sessions and see for yourself how it's done. They offer hands on experience and you learn how to properly apply fabric to wings and control surfaces. You will discover that the fabric is incredibly taught, once properly shrunk. The skin of a drum comes to mind. You can shrink the fabric too much and actually crush or bend the framework beneath it, the fabric has that kind of strength. Corky Scott |
#10
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wrote:
Ernest, it isn't the dope that provides the strength, not with Razorback fabric or with any fabric. The fabric itself is what gives the wing it's strength and/or stiffness against the wind. The initial application of the correct dope, in the case of the Razorback fabric, or a calibrated heating iron, in the case of the Polyfiber fabric, is what shrinks it. The application of paints on top of the fabric serve to protect it from UV rays, make it waterproof, and look nice, but do not add strength. You should participate in one of Ron Alexander's fabric covering sessions and see for yourself how it's done. They offer hands on experience and you learn how to properly apply fabric to wings and control surfaces. You will discover that the fabric is incredibly taught, once properly shrunk. The skin of a drum comes to mind. You can shrink the fabric too much and actually crush or bend the framework beneath it, the fabric has that kind of strength. Corky Scott Corky, the polyester fabrics have long chain molecules that 'curl up' when you heat them. This makes the actual threads shorter, so that after the actual fabric is shrunk to size. The butyrate doesn't shrink the fiberglass threads. It just grabs a couple and pulls them closer together. "Chain is only as strong as its weakest link" comes to mind. Until a butyrate coated covering stretches enough to take out the slack that was there when the fabric was first put on, it is only being held together by the butyrate. That is the mental picture I have. I could be wrong, and I don't even know if it is good or bad. For starters, I don't know how strong butyrate dope is. It could be much stronger than polyester, and just needs the fabric to give it some shape. I'm in unknown territory and just need a compass and a map, or maybe just a practice kit to play with. Didn't I read somewhere that butyrate dope can be found in most hardware stores under a different name? -- http://www.ernest.isa-geek.org/ "Ignorance is mankinds normal state, alleviated by information and experience." Veeduber |
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