|
|
|
|
|
|
||
|
|
Quote:
You flatter me with your questions. I’m just returning back into the hobby after a 15 year hiatus, am struggling through each challenge that I encounter as I build the RELAX, and, on most days, feel very humbled by problems I cannot solve quickly. For the sake of conversation, I can give you my opinion but by no means should it be interpreted as authoritative or necessarily credible. Carbon fiber shafts for the fuselage longeron: The ideal fuselage longeron for an aircraft like the “Relax” should be stiff as well as light. But the question can be raised as to how stiff should it be without becoming too heavy? In my opinion, the longeron only needs to be stiff enough to prevent the long fuselage from warping. The weight of the tube should be given at least equal consideration. The RELAX was designed for flying indoor precision aerobatics at a slow speed. Such performance characteristic was achieved by minimizing the flying weight. The Relax’s wing loading is unbelievably low. I estimate that my badly overweight model will have a wing loading less than 1.5 oz/sq ft. (This is in stark contrast to the pattern airplanes that I flew in the West Texas winds, circa early 1990’s, which had wing loadings about 12 to 15 oz/sq ft). To acquire lower weight requires discipline, careful planning of the material/equipment as well as the building methods used. Having grown up with larger balsa models, I am having difficulty transitioning to ultra-light indoor planes. The selection of the longeron is a good place to start and I appreciate the reason why you ask this question. I don’t have any experience with carbon fiber arrow shafts and thus cannot offer any specific comment as to their merit. I have, however, searched for lightweight round carbon tubes and my initial find was discouraging. For example, a 8 mm (OD) – 6 mm (ID) carbon tube weighed 34 grams when I was hoping for tubes closer to 2 grams. The balsa stick was the best I could find when I began construction. Later, however, I read that there are two kinds of carbon tubes, extrusion and wound types (http://www.radicalrc.com/category/Carbon-Rod-Hollow-410). The latter is cheaper and lighter. But, at this time, I have not purchased a wound-type tube. Where to purchase Kevlar thread: Kevlar thread is commonly sold in stores specialized for fly fishing. You can order the thread over the internet from stores like http://www.edgeangling.com/Fishing-T...=kevlar+thread. There might be different types of Kevlar threads. The ones that I like are those that remain wound as you handle them. I can tie the joints more neatly with this type of thread (purchase from the store in the above hyperlink). The other type unwinds into a bundle of very fine fibers and is more difficult to handle. However, I don’t know which type of thread is stronger and I don’t know whether they are identifiable by different names. What are the thoughts of using hair thin copper magnet wire to make the terminal end bindings? The need for tying the carbon rods arises because the minimal surface that each tip of the rod makes contact at the glued joint. So when considering an aircraft constructed with extensive truss elements, you might appreciate that the greatest structural stress occurs at the glue joints, not in the carbon rods themselves. Lantsov Alexey apparently understood this and incorporated the method of tying each rod using the Kevlar thread. Kevlar thread accomplished two things. First, winding each joint with thread – in effect -- increased the glued surface. Second, because of its high tensile strength, the thread itself contributed to the strength of the joint. Kevlar thread has a tensile strength equal to that for the equivalent weight of steel. I suppose that the copper wire can be used in place of the Kevlar because the wire would increase the glued surface. But copper wire does not have as good strength and weight characteristics. Do your proposed methods have any merit. The answer is of course they do. The merit, however, depends upon the desired cruising speed and aerobatic performance. I just doubt that anyone would wish to invest the amount of time, effort, and money that this aircraft requires just to build a good sport flyer. May be I'm wrong. Sincerely, Rocky PS – I have finally got the servos and receiver satisfactorily installed. I’ve been trying for about 1 ½ months – which is far more time than I anticipated. That includes working through 7 failed attempts plus the ancillary work of their removal. The latter is time consuming as it is not easy to remove joints and material that were tied with Kevlar and glued with CA. Additionally, the removal of the failed attempts incurred unintentional slips of hand that often resulted in damage to nearby support braces. The 0.6 and 0.7 mm diameter rods fractured easily but the 1 mm rods survived the abuse quite well. ![]()
|
|
|
| Thread Tools | |
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Build Log VIDEO ADDED: Pro Design F-18 Build | MattinAZ | Electric Ducted Fan Jet Talk | 799 | Apr 03, 2013 05:56 AM |
| Discussion EJF Composite F-86 | Reco | Electric Ducted Fan Jet Talk | 11 | Jan 08, 2010 02:23 PM |
| Question Composite Arf P-51 Engine ? ? ? | dono | Fuel Warbirds | 0 | Dec 04, 2009 05:36 PM |
| Idea Composite D Box Design | j.m. | Composites Fabrication | 4 | Sep 02, 2009 02:38 AM |
| Jet Design Contest entry #3 -- Messerschmitt Me P.1092/5 | berniep1 | Electric Ducted Fan Jet Talk | 79 | Nov 22, 2007 05:46 AM |