| SMALL Articles by Joe Wagner |
I like aluminum landing gear struts greatly. Their advantages considerably outweigh their disadvantages; and with Sig carrying such a wide range of preformed sizes, blanks, and tempered hard aluminum sheet, just about anything anyone could want in the way of a "main gear strut" can be easily achieved.
The only problem occurs in bending hard aluminum. It's very easy to weaken or even crack an aluminum LG blank by using the wrong method -- and unfortunately the instructions Sig supplies are based on a misconception.
Aluminum hardens in a totally different way from steel -- and is "annealed" differently too. To harden steel you heat it and quench it quickly. That's how you ANNEAL aluminum! Tempered aluminum's springiness comes mostly from its alloying elements. After annealing, the hardness will gradually return of its own accord.
Hardened aluminum can be temporarily annealed by heating it to about 500 degrees F, and quickly quenching it with cold water. It will then remain soft for between a few hours and a couple of days (depending on how hot the weather is); gradually regaining its original hardness. (To speed up the re-hardening, you can re-heat the aluminum in boiling water or a 250-degree oven for a half hour or so.)
Here's how to bend tempered aluminum landing gears:
DON'T use anything that will scratch the aluminum!
Doing the job this way insures that the landing gear "legs" will remain straight during and after the bending procedure.
This same technique is also useful in re-shaping preformed aluminum landing gears. Sometimes a preform doesn't have quite the right dimensions for a particular model. But "spot annealing" allows easy re-bending of "tempered aluminum" to whatever size and shape you need.
Now for attaching the strut to the airplane. The "usual method" is to install a plywood plate in the fuselage bottom, and bolt the aluminum LG to it. But that's not the best way to do the job!
Instead, glue 3/16" X 1" birch plywood "doublers" inside the fuselage sides at the landing gear location. Drill and tap two # 4-40 threaded holes vertically in each doubler. These are for nylon screws, which attach the LG strut via matching holes close to the bend line. Leaving the center area of the strut unattached allows it to flex there under heavy loads, thus absorbing impact.
(This basic technique is standard practice in homebuilt & "kitplane" man-carrying aircraft.)