| Home | Articles | CP reprints |
New exhaust system for N26MS
From CP89-Page 1 (January, 1996)
by Mike Melvill
The 4-pipe exhaust system
that I built back in 1986 has served faithfully for 1360 flight hours, with only a couple
of minor cracks (after the original trial and error test program). For some time
now, I have wanted to try a 4-pipe exhaust system that does not run the high pressure
exhaust plume through the prop, right at the hardest working area of the prop blades. I
have discussed this idea over the years with anyone who would listen, but just never got
around to doing it somehow.
I guess I have just been too lazy to get it done, but I also knew
that my existing exhaust system had performed essentially without problems for many years.
I worried about going through all the development hassles
that I was sure I would have to endure if I went ahead with my plan.
Just a few weeks ago I decided to bite the bullet and try it. I
have long felt that the high pressure exhaust pulse trashing what is essentially the
highest activity area of each blade, was probably costing some prop efficiency, and may
have been causing some of the vibration felt in our Long-EZ. I also hoped that it might be
quieter if the exhaust was not being cut to pieces by the high speed prop blades.
As I saw it, I had two choices: (1) I could route the exhaust
out-board far enough to completely miss the prop (maybe the best choice?) or (2) I could
route the headers to direct the plume through the prop, close to the spinner, where the
prop blades really aren't very aerodynamically useful, and just as important, where the
rotational speed of the blade is a lot slower.
I decided the problem of running a hot exhaust pipe inside the
wing roots was too great, so I designed and built a system that consists of four separate
pipes that terminate about 1-inch inside the cowling cooling air exit. My cowling goes aft
much further than the standard plans-built cowling, and I also have a 9-inch long heavy
duty prop extension. The exhaust pipes end about 4 3/4 inches in front of the leading
edges of the prop blades, close enough to the spinner so that most of the grayish exhaust
deposits end up on the spinner! (One of the disadvantages of this system). I did feel that
in order to see any improvement in prop efficiency, I would have to run the exhaust
through the prop as close-in to the spinner as possible, and I have done just that.
I built the exhaust system, one header at a time, in place, on
the airplane/engine. I felt this was the only way to ensure that it would fit, would not
interfere with the top or bottom cowling, and would point right at the prop where I
thought it would cause the least disruption to the smooth flow of air into the prop disc.
I ordered all of the tubing from Ken Brock and started cutting
and fitting. I used Hot Stuff model glue to "tack' the pieces together, then drove
over to Scaled and tacwelded the pieces. I had to bead-blast the Hot Stuff glue off the
headers before I could finish weld, because Hot Stuff could contaminate the weld. After
almost two weeks of evening and weekend work, I had the exhaust system done.
I had modified the rear baffle (see photos) and patched up the
areas of the cowling where the old 4-pipe exhaust system used to exist.

Left side - Two exhaust pipes supported by aft baffle extension. Note gas
deposit on prop very close to spinner.

Right side - Shows routing of pipes and the baffle support
I now had a much cleaner, neater-looking installation, but how
would it fly? My first impression, when I started the engine, was that it was much louder!
It certainly sounded different. On the take-off roll, I noticed it was much smoother. In
fact, smoothness is the most noticeable change. Up at altitude, after I had flown it
around for a while at different power settings, I opened it up to full power and let it
settle for several miles. I did this at an altitude and temperature where I had gathered
this same data with the old exhaust system. The final result was that at exactly the same
engine RPM, manifold pressure, and fuel flow I was looking at five knots indicated faster!
I was blown away. I honestly never expected that large of an increment. The prop must be
that much more efficient without the high-speed exhaust plume disrupting the "sweet
spot" on the prop.
I have since heard from other builders and flyers who have
assembled similar exhaust systems. Several achieved similar results, and others gained
nothing. I believe you must direct the exhaust plume through the prop as close to the
spinner as you can in order to get this kind of improvement. If you just move the plume
inboard a few inches, chances are you won't gain any performance.
The disadvantage of the dirty spinner is overshadowed by an even
more important concern to me - the fact that I once again have an unproven exhaust system
that I can't have much confidence in until I get several hundred hours on it with zero
failures. I was so sure of my last exhaust system, it is an uncomfortable feeling at this
point. In fact, for now, I remove the cowl and inspect the new exhaust after every flight.
Only time will tell if this was a good idea.