Why not try a sling seat like the Taylor mono plane and keep things simple.
I can see that Alum seat cracking and your a$$ landing on the elevator
cables and then what a mess

On Thu, Aug 30, 2018 at 7:14 AM Teate, Stephen via KRnet <
krnet@list.krnet.org> wrote:

> I think the decision of what kind of seat is  every bit as important a
> decision as to what resin or wood we use in our airplanes. I would say that
> there is little argument as to the simplicity of the stock sling seat but
> if you are going beyond that then it should require some real thought
> especially when you consider the possibility of having a real bad day and
> then that seat may be the only thing between you and concrete.
>
>
>
> I have resized and attached a photo of my two seat designs that I came up
> with. The first one is the grey composite seat. Made by just cutting and
> fitting foam between the spars all the way down to the bottom of the
> fuselage with cutouts for the cross members of the fuselage floor so the
> entire seat bears on the spars and bottom skin. Since it is solid foam I
> liked the idea that should I have that bad day the glass would probably
> fail pretty quickly but the foam would continue to absorb a load assuming
> it stays in place. I am 6'-5" and I have already deepened my fuselage to
> get the required headroom that I am going to need while wearing a headset .
> Even by doing this I had to cut down the depth of the seat as much as
> possible to get my butt as close to the bottom as I could. By doing this I
> effectively destroyed the ability of my seat to take any real load. As it
> loads up it will "form" itself to the available area between and over the
> spars. As the load increases the bottom of the fuselage is going to flex
> and the only thing that will hold the seat is the spars. Each side of the
> seat becomes a shear web at this point but because of the depth of the seat
> its load carrying ability is zilch almost regardless of how thick I make
> them. And since most of the load of my reclined body will be on the aft
> portion of the seat this is even worse.
>
>
>
> Now look at the aluminum version and remember this is really all because
> of my height. By using a 1/8" sheet on the bottom I can get my butt as
> close as I want it to be to the bottom of the fuselage. I then used the
> same thickness of sheet to make 2" deep sheer webs on each side of the
> seat. These span the full length from spar cap to spar cap and then over
> the edges of both. The bottom has an "H" pattern of 1" x 1" x 1/8" angles
> that span from sheer web to sheer web and the cutout for the stick is lined
> in the same material. Also by bending the aft part of the seat from the
> bottom slope to the horizontal I create additional stiffness. The back of
> the seat is the same back as used on the composite seat and is hinged for
> access behind them. Believe it or not there is not much if any difference
> in weight between the two once the lightening holes are cut. Both versions
> use the same cushions so it is fairly comfortable but the load carrying
> capabilities are miles apart.
>
>
>
> And if you think this welding is bad you should have seen the intake
> manifold on the old Subaru, downright breathtaking.
>
>
>
> Stephen Teate
> Paradise, Texas
>
>
>
>
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