Geof
Sorry, been off-line for a bit.
Absolutely no offense taken with any corrections or suggestions. I'll try to make the corrections.
I'm afraid I'm an engineer wanna-be, but not sure I have the discipline for it. I dreamed this up, did a rough draft of it, but a lot of things didn't fall together until I actually started building it. I'll have to start writing it down as I go (what a concept, real engineer/scientist.) I DID take the pictures as I built it, at least that helped
Okay, trying to answer your questions.
On post #2, the right-hand template image, the rotor stop inner angle is marked as 15 deg, but you clearly mean 75 deg. The 15 degree (or 75 degree angle) on the HINGE gives you the “force” that makes the rotors spin when the rotors deploy, the heavy engine combined with the rotor drag orients the helicopter “upright” (engine down), and the helicopter falls/descends, generating an air current perpendicular to the rotors. If you remember those Christmas decorations with the four candles and the rotor thing on top, the ascending heated air rotates the Angels or Santas or whatever to spin.
The Rotor stop angle gives the rotors a certain amount of dihedral with the tips higher than the hub (at least dihedral is what it is called in the airplane/glider world.) I originally picked 15 degrees cuz that's what I use for my gliders. The dihedral in gliders helps with stability (I think of it as the part of the design which helps orient the glider up side up and down side down in the glide phase.) The "cost" of the dihedral is less blade directly perpendicular to the descent path (or parallel to the horizon.) Just as in a glider, there is a small cost in lift (for 15 degrees, 1-cos15 is about 3.5%.) One of my reviewers suggested that having a flatter angle would give me more lift (although if I do the math, I think it comes out to about 2%, which doesn't sound like much. He probably knows more than I do, however.) On my Gyskelion (build thread pending) I DO think I need the extra dihedral because it is engine eject, with only the paper nose and balsa hub pulling the down side down. On the Whopper Flopper Chopper (WFC) I have a long dowel and a reeeeallly heavy engine casing, I could probably go with no dihedral at all. Note you CANNOT have a zero angle on the hinge as the rotors won’t rotate (yes, I know that is not COMPLETELY true, but we will consider it so for purposes of the WFC.)
1.
if you choose a different angle, it does not affect any other angle or measurement in the design whatsoever. With my design I don't think changing the angle makes any difference in any remaining flight characteristics or otherwise changes the build. Partly because a lot of the recovery system is probably "air brake recovery", meaning rotor rotation on my design (with no airfoiling) is simply big honking blades coming down perpendicular to the descent path-- the rotation just keeps it perpendicular. As der Micromeister pointed out when I dared post in the competition section some questions (and showed my blatent ignorance, lol), competition choppers require careful airfoiling and balancing, and the degree of airfoiling is dependent on the rotation speed (and some say actually the optimal airfoil changes along the length of the rotor as you get further from the hub, as relative to the air stream the tip ends are going much faster than the hub ends.) At least at this point, all that is beyond my abilities. As a Sport Flyer, I actually think I got lucky, the length of flight for the WFC is just right to be fun and exciting for me, and I don't think there is a great risk of thermaling this puppy away. Which is probably a good thing, as people think a 12 inch rocket landing in their yard or pool is cute. A 10 foot monstrosity landing in the pool or the park tennis court is pushing it-- even when it lands as softly as this puppy does. But I digress…..
I'm also planning on airfoiling the blades a bit.
This may sound stupid of me, but probably important to decide your goals with the build. “Basic Sport Flying” or “Long Duration Flights.” I kind of see this also when people talk about tapering fins.
I don’t know yet whether this design will ever be a competition bird (although at least it meets criteria for competition, as opposed to Gyskelion which is engine eject=auto-DQ’d.) As I said, I like my 50 to 60 second flights with only a few hundred yard runs at most. So if your (very logical goal) is long flight times, I THEEENK airfoiling will help, although I have no idea how much. I do know with this much lumber it is going to be a LOT of work (somewhere there is an experienced BAR who keeps posting on his signature he loves to sand. THIS is the bird for him!) I do know you won’t hurt this bird with sanding, especially with the thicknesses of balsa that we are using here (and you are going up a bit on the inner rotor.) Definitely agree with sanding BEFORE you assemble, definitely don’t airfoil the hub, and probably wise to leave a cm on each side of each hinge un-foiled. I would also leave a trail edge thickness of at least 1/16 inch if you are planning on flying this regularly for sport, I think if you taper it any finer you probably will end up with a lot of knicks in only a few flights.
Next slight unclarity. Post #2 says to use the template to cut the notch at the nose end. There is no measurement given.
My bad. That’s not a template, that’s just a diagram. Originally I had a template, but I didn’t bring it on the road with me, so I couldn’t post it and I forgot to correct it in the instructions. I have corrected the post and just given the location, the dimensions, and the diagram. Interestingly, this does not HAVE to be centered, it does absolutely have to be straight with the long axis of the rocket.
In post #3, you omit any indication of what piece of balsa is supposed to be taped to the outer rotor, except that you call it the "Hub-outside rotor".
Okay, understood. Corrected to say after the cut the Little Piece is the HUB, and the Big Piece is the OUTER ROTOR. I am going to stick with the term Stand-Off Adapter.
For the front hinge, post #3, I made two of them with the outside tape on the outside face and two with the outside tape on the inside face. I was careless.
You’re actually making me feel better. I’ve built around 30 helicopters using these tape hinges, and I’ve done what you did at least 10 times. I am afraid that in my case I always think of the nose as pointed away from me and the tail as toward me, and I diagram things and draw them that way. For me personally it is more intuitive, although I agree with you that when you are working with 30 plus inch rotors you are more likely to lay them sideways. My clarification for this was to place a black mark on the lead edge and try to refer to that in all my orientations (lead edge left, lead edge right, nose end away from you.) I thought about trying to label the surfaces inside and outside, but even that gets confusing, especially with the inner rotor, as the face that is truly “inside” at launch is contiguous at deployment with the outer rotor “outside” face. In fact, the OUTER ROTOR at launch is closer to the hub at deployment (and technically would be the “inner rotor”—vice versa for what I call the INNER ROTOR.)
I think I’m going to stay with marking the lead edge and trying to describe the orientations relative to that and the nose position. I have made an emphasis to the lead edge orientation in the instructions.
Originally Posted by BABAR
... and mark the Trail Edge 8.5” from the tail end. Connect the marks. Cut across this line. The longer section is the Rotor, which will be 31.5 inches long. This should match the dimensions on the diagram.
The mark should be at 8.25 if it is going to match the diagram and the other parts.
Oops. You are correct, and I have corrected the post. 5.5 plus the fin width of 2.75 = 8.25. Thanks!
(BTW, I used 3/16 instead of 3/32 thick; the thinner stuff just seemed too fragile. We'll see later how this screws me up.)
That MAAAAY be a problem. Because the Outer and Inner Rotors are concentric squares, the remaining internal diameter (the "lumen" of the square tube) will decrease if you increase the thickness of the Inner Rotor without increasing the WIDTH of the inner and outer rotors accordingly.) I'll try to post a pic in next post.
As for the reason I went with 3/32"--- As I was building, I was really getting concerned about weight, and I had never used an E engine before (I had originally planned on doing this on a D.) I suspect as you go over this you will come up with ways to save weight that will more than make up for the difference in thickness here. Your fins will also be stiffer, and therefore will flex less on descent, which is a plus for your change.
So from a STRUCTURAL standpoint upping to 3/16 should not be a problem, but from a DIMENSION standpoint it may leave the inside too crowded.
Tom
Honestly Geof, I definitely appreciate the critiques, and I apologize for my errors that messed you up!:bang:
Tom