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		victorbravo(at)sbcglobal. Guest
 
 
 
 
 
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				 Posted: Tue Mar 22, 2016 12:54 pm    Post subject: Addendum - Elevator/Stabilizer hinge ass'y | 
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				With all sincerest respect to Mr. Wainfan and any other great engineers out there who might be monitoring this discussion, the credentials and field experience of the engineer (who I asked to review the elevator attachment) are high enough for the purposes of settling any questions about the appropriateness of any particular aircraft structure.
 
 He is a graduate of the 1950's DeHavilland Aircraft Engineering program in England (from youth apprenticeship up through engineering degree in aerostructures and metallurgy), and I believe Arnold Schwarzenegger cannot physically lift his aerospace resume' . Any further comment on his achievements or abilities would sound like an infomercial, so I will leave it at that.
 
 Bill Berle
 www.ezflaphandle.com  - safety & performance upgrade for light aircraft
 www.grantstar.net           - winning proposals for non-profit and for-profit entities
 
 --------------------------------------------
 On Tue, 3/22/16, Stuart Harner <stuart(at)harnerfarm.net> wrote:
 
  Subject: RE: Elevator/Stabilizer hinge ass'y
  To: kolb-list(at)matronics.com
  Date: Tuesday, March 22, 2016, 12:27 PM
  
  
  "Stuart Harner" <stuart(at)harnerfarm.net>
  
  Bill,
  
  I am not an engineer but I did stay in a Holiday Inn last
  night.    No, not really, but I do have a fundamental
  understanding of load transmission through a structure.
  
  First a question, and please don't be offended.  Have
  you had an opportunity to observe the structure of the Kolb
  tail while it was being folded and then again when it is
  bolted into place?  I asked this because I found a
  couple of things in the plans of the Firefly that I did not
  understand until I was able to actually see it live. Simply
  put, I had trouble visualizing it from just the plans.
  
  One thing that I think is missing from this discussion is
  the loads carried by the brace wires. I would posit that
  most of the forces from the tail that are transmitted to the
  boom tube are carried by the braces. These, when properly
  tensioned are actually pre-loaded slightly. This puts the
  tubes in compression which makes the whole thing quite
  strong. It also transfers the loads from the horizontals to
  the steel post of the verticals which in turn is transferred
  to the boom tube via the steel ring which is bolted and/or
  riveted to the tube.
  
  Of course some loads are transferred through the hinge
  points and the front hinge must be able to slide slightly as
  the elevator moves through its arc of travel. Could this be
  made stronger? Of course, but not without sacrificing
  something else such as weight or foldability. It is actually
  a very clever design and I suspect that the majority of
  loads that move through the rear hinge come from the
  elevator and not the stabilizer. 
  
  I would also bet that the loads carried through the hinges
  is far below the shear and tension limits of properly
  installed rivets.
  
  I am actually more "freaked out" by the fact that everything
  in the tail depends on that one little 3/16" bolt (Firefly)
  that holds the lower braces in place. Really, the threads on
  that bolt are all there is between you and falling out of
  the sky. To combat this irrationality I swap out the bolt
  fairly often and the nuts even more often. If it really
  bothered me, I would stay on the ground.  
  
  Perhaps you could send a copy of your plans to Barnaby
  Wainfan and ask for his analysis. I hear he is a really nice
  guy. From reading his articles over the years I am sure he
  could provide the answers you seek.
  
  As Uncle Red used to say: "Remember, if women don't find you
  handsome, they should at least find you handy"
  
  Stuart
  
  --
 
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		Leland.Lam
 
 
  Joined: 19 Nov 2014 Posts: 20 Location: Phoenix, AZ
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