I'm considering adding cabin heat (or at very least the firewall hole) before I close in the glareshield. Looking for thoughts on whether my plan makes sense. The plane is an Ohio based tailwheel, turbo aerovee powered Sonex-A still under construction.
Since I have the top mounted oil cooler, and it's now considered acceptable to not install the bottom oil cooler inlet scoop in the cowl, I'm thinking of running a round SCAT tube inlet from that location on the front face of the cowl. I also want to get some blast tube air for the gascolator and fuel line. I'm thinking 2" or 2 1/2" diameter SCAT from the inlet, running back to a Wye that splits to a 2" (to the heat muff) and a 1" or 1 1/2" SCAT tube for the blast tube.
My plan would be to put a heat muff on the turbo exhaust down tube (the lower removable section) with screen door springs wrapped around the exhaust tube to increase heat transfer. This way, during summer flying, I could just switch out the heat muff down tube, for a plain exhaust tube without the heat muff, saving weight and heat retention issues. The SCAT would just be spliced together giving an extra source of fresh air in the cockpit.
On the firewall, I'm either going to to buy or make a stainless steel diverter valve like this one from plane innovations.
http://www.planeinnovations.com/product ... ve-hbv-02/Installed orientation of this photo: right side is up, left side with the inlet tube would be down on the firewall, bottom is cabin side.
This diverter valve design will keep all of the controls on the pilot side, and keep it simple for penetrations. I would mount this on the passenger side, right above the rudder pedal tubes, and below the tank. Run a solid bar from it to below the panel for operation. There should be enough room on the firewall between the turbo exhaust and the firewall for the diverter valve and tubing to fit.
If I make my own diverter valve, I may just make the flapper and hinge from SS (directly attached to the firewall), and form the box from Aluminum for ease of construction. From a fire point of view, it shouldn't matter as the firewall and closure would still be all stainless, and would remain whole even if the diverter box melted off the firewall.
Concerns running through my head.
A.) Am I going to get enough heat from that short tube section to make this worth the time/expense?
B.) Is the exhaust tube joint going to leak causing fume issues? To some degree, I could mitigate this by welding the muff to the tube (but that makes the muff steel vs. alum). A welded heat muff shouldn't be a big issue since it should be inspectable from the inside.
C.) With the heat muff installed, and diverter valve closed, the diverter is going to dump more heat directly under the turbo...exactly where we don't want it...but this may not be an issue for cold weather flying when the heat muff would be installed. Might still be an issue for the shoulder seasons.
D.) Performance issues with the inlet in the front of the cowl...would a NACA scoop on the side or bottom of the cowl be a better choice? That's more expensive/ time consuming...
E.) Is a 2 1/2" inlet overkill vs. just use 2" SCAT throughout? Since the air will expand on heating, a 2" feed, even with some drawn off for the blast tube may be sufficient.
F.) Any ideas on where to buy a Wye like I'm describing? Thinking I'm going to have to fab something from some thin wall aluminum tube.
G.) Will the weight of the heat muff and tubing be too much for the exhaust extension connection springs, and will I need to add additional support for the system?
Anyone done anything like this, particularly with a turbo?
Thanks,
Gregg Short
Sonex 715
Burbank, OH