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Earlier, Wallace Berry wrote:
...Wing skins form the hinge for the wing control surfaces. No mylar needed... A minor nitpick: That is the way it looks from the outside. However, structurally, the upper wing skin does not actually support the aileron. Inside the wing there are several support linkage gadgets that transfer lift loading between the aileron and the wing. I can't remember if they're four-bar links or track-and-roller arrangements. However, these gadgets are carefully arranged so that the effective hinge axis coincides with the surface of the upper wing skin. There are other sailplanes that use this sort of system; the flaps of the Slingsby T65 Vega come to mind. It is a compelling system, since as Wallace points out it needs no mylar and no internal curtain sealing. However, what I've seen of one or two Speed Astirs in service is that the control loads tend to be greater than in more conventional systems, especially as they age. Also, the flexible skin portion tends not to hold its surface finish well; I've seen cracking and bubbling in this area on both Vegas and Speed Astirs. It's also hard to achieve the kind of surface travels that it takes to make high-aspect ailerons do their job effectively. Getting off-topic, there _is_ at least one Chris Heintz powered airplane that does actually support the aileron on a flexible portion of wing skin. For more information, see: http://www.zenithair.com/kit-data/ht-aileron.html Thanks, and best regards to all Bob K. http://www.hpaircraft.com |
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