Subject: Recent flight from Everett to Medford
From: rotaryeng
Date: 8/29/2012, 8:04 PM
To: AAAA Put this in the To box


 This week I flew my RV-4/13BREW from Everett Wa.  to Medford  Ore. and
 back.
 Headwinds on the way down were brisk- 30 kts at 8500 feet on the way down,
 but 35 kt
 tailwind on the way back. The engine ran flawlessly but the plane is slow-
 true
 airspeed was 110 kts at 19.5 manifold pressure,5600 rpm oil temp 161 and
 coolant 170,
 fuel flow around 8 gpm. My prop is a three blade Catto, 72 dia x 88 pitch.

 For one, the plane is  over propped. I'm going to have Craig Catto cut it
 down a
 little during the winter maintenance. The other thing is that the cooling
 scoop is
 effective, but way too draggy, so I'm going to re-do it this winter.

 Another issue is my left brake line- I"ve melted it twice. It's plastic,
 and although
 it is shielded from the exhaust pipes and insulated with fiberfrax, I
 think that
 heated air from the exhaust pipes is being forced out the opening in the
 cowl where
 the brake line goes to the gear leg. That's where I have found the line
 melted. I
 want to put  a reverse scoop near the exhaust pipes to get the heated air
 out of the
 cowl, and to replace the brake line with stainless steel. Everything
 inside the cowl
 except for the brake line looks OK- I wrapped and shielded everything -
 wires,
 coolant, fuel,and oil lines. There are three NACA ducts bringing air into
 the cowl to
 cool the alternator, the coils and exhaust pipes, and an exhaust eductor
 to suck air
 through the cowl and over the muffler.

 Comments?

 Brian Trubee

 Couple of questions.
 EGT?
 Size of throttle body?
 Is the engine ported?

 The manifold pressure is very low.

 Is the air filter plugged? :)
 Are you getting cold air?

 8 GPH is 50 pounds per hour at 6.25 pounds per gallon. At a BSFC of .47
 leaned that
 is only 106 HP. At a fuel burn of .5 that is only 100 HP. If it is really
 rich and
 the BSFC is .55 and that is only 90 HP.

 You need a p-port Brian :)

 Paul Lamar


 Brian,

 As some of you know my Wheeler will be a blend of certified parts and
 experimental parts. I noticed the issues with the nylon brake lines long
 ago. I went to NAPA and bought (8) 12" standard brake lines that go on
 trucks from the hard line to the wheels. I also bought a 25 foot roll of
 3/32 brake tubing, 24 double flare fittings, and a double flare tool. Total
 for all of this was $170.00. After I got back to my plane, within 2 hours I
 had the brake lines made up from the master cylinders to the wheels. Galv
 steel line inside the cockpit, 12 inch flex at the master cylinders, at the
 turn into the wings (mine are removable) one more at the flex point of the
 gear leg, and the last one at the wheel. I don't anticipate melting my
 brake lines. This is the way my Viking was done, and I had no issues with
 my 1968 Viking until I blew the Continental up.

 My fuel and oil system will be similar. The materials are inexpensive, and
 the labor is minimal. Cheap insurance.



 Kevin Alderman

 brian,
               This is the blind leading the blind as I have yet to depart
 the earth, but tied to a tree I get MP of 22 at 5000 rpm and from memory 24
 at 5600 rpm.  Where are you reading it from?  Neil.


 It's been a while since I did any static runs on the ground. I"d just be
 guessing at
 this point to give some numbers for static running.

 Brian Trubee


Brian,

You stated "...my EGT temps- they show up to 2000 at times- and above
1800 most of the time in cruise."  I too experienced very high EGT's
in excess of 1800* when I was using a muffler that was too
restrictive.  Also, power was way down, but it was quiet.  ;-)  The
high temps ended up damaging the o-rings and I had to rebuild the
engine.  Since replacing the muffler the egt's have dropped down to
1600 - 1650* range and power is much improved.  I suggest you examine
and modify or replace your current muffler.

Mark

The best muffler for a rotary is 3 to 8 feet long about 4 to 5 inches in diameter.
That gives the lowest aero drag for a given silencing. Lowest frontal area. Mufflers
work by the exhaust gases rubbing on the metal surface losing kinetic energy to skin
friction and losing heat to the metal surfaces. The cooler the gases in a pipe the
lower the gas speed. When high speed gas exits a pipe there is a sudden expansion
that causes the noise. The idea here is to cool the gases before they get to the end
of the inner pipe.

The inner tube is best done in .045 Inconnel but there is a trade off with thickness.
If you make the inner tube 2 inches in diameter and use 321 SS make it .065 thick
with a bunch of holes drilled in it. The outer tube can be .030" thick 321 SS as it
will always run cooler. Also make the front of the muffler look like this.

Don't drill any holes for the first 8 to 10 inches. The slip stream will blow cooling
air down between the coaxial tubes. At the back end make the inner tube 6 inches
shorter than the outer tube. That will act as an ejector to draw cooling air between
the two tubes. Patent applied for:)

A 2 inch diameter SS tube .065 thick 72 inches long will weigh about 8.8 pounds.

A 4 inch diameter SS tube .030 thick 72 inches long will weigh about 7.50 pounds.

Here is a dwg.

A 2.5 inch inner tube and a 5 and 1/2 inch outer tube may give a little less back
pressure for a weight trade off.

Paul Lamar

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