I have a 21 lb cap on my system for this
very purpose. I don’t presently have a coolant recovery tank and if the
cap burps, I could lose coolant overboard. I am rethinking this and plan
to install a coolant recovery tank as well.
By the way, on the high coolant pressure,
in surfing the web I have found that this problem is most likely caused by
combustion gasses getting into the coolant. That would mean a busted
o-ring. I have been in denial that this is the cause because I don’t want
to tear the engine down. Today I plan to see if I can find any coolant
coming out of a sparkplug hole. Fingers are crossed!
Bill B
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Ed Anderson
Sent: Friday, March 25, 2011 8:27
AM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Radiator Caps
[FlyRotary] Re: On the subject of installations...Coolant Pressure
One thing to keep in mind about the
pressure rating of the radiator cap you are using. All are rated relative
to a standard sea level ambinent pressure. This means that he air
pressure itself is contributing 14.7 psi at sea level.
So at sea level when your differential
pressure coolant gauge is reading 10 psi - the absolute pressure in your coolant
system is then 14.7 + 10 = 24.7 psi. Now if you are flying at 8000
MSL your ambient pressure is approx 1/2 at sea level. So your 14.7 psi
CAP now has the lesser capacity of 7.3 + 10 = 17.3 psi absolute pressure
capacity - somewhat less than the 24.7 psi absolute it had at sea level.
When you increase in altitude this
component naturally decreases. So while a 14.7 psi CAP may work fine at
sea level, more than one person found that at altitude that rating
was insufficient and some coolant was lost.
I personally would not fly with less than
a 21 psi cap and currently fly with a 24 psi radiator cap.
There is another factor that occurred to
me. Once a hot coolant system blows the relief valve on the cap,
that lowers the pressure inside the system, superheated (>212F) coolant can
quickly flash to steam and further cause lost of coolant. So a Higher PSI
cap can lessen the chance of that happening.
Sent: Thursday, March 24,
2011 5:30 PM
Subject:
[FlyRotary] Re: On the subject of installations...Coolant Pressure
Lynn,
You have hit my quandary squarely on the
head. Assuming that the pressure was zero at room temp and rose to say
6-7 pounds at 200 degrees, and assume that the flow restriction in the system
caused a pressure rise of about 2 pounds at 2000 rpm and a pressure rise of,
say, 6-7 pounds at 6000 rpm. Under that scenario, you would have a
pressure that ran at between 7-9 pounds at 2000 and rose to 12-14 pounds at
6000. Those pressures would be easily contained with the stock cap of 14
pounds. And the pressure would be constantly changing with rpm and
possibly temp of the system as you were under power or not.
I have a 21 pound cap. My system climbs
smartly to the top and stays there. No fluctuation with rpm, no real
fluctuation at temp because it has already hit the 21 pounds before the engine
is actually hot. (around 190)
Something is wrong and I don’t understand
what it is.
Bobby
I am going to insert answers to your
questions in your msg below.
Bill B
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bobby J. Hughes
Sent: Thursday, March 24, 2011
1:57 PM
To: Rotary
motors in aircraft
Subject: [FlyRotary] Re: On the
subject of installations...Coolant Pressure
Bill,
This is all I can think of at the moment.
Are you running a thermostat or did you
plug the hole between the inlets and outlets of the water pump?
No thermostat. The Renesis has a
thermostat tower which is too tall to fit under my cowl, so I removed it and
fabricated a flat plate with two 1.25 aluminum tubes for the inlet and outlet
of the water pump. That hole you are referencing exists in the tower, but
not in my plate.
If plugged did you drill a small hole in
the plug to allow air a place to escape? I used a #30 drill.
Any air in my system would have to be
carried to the highest point, (radiator cap) then be forced by pressure to the
bottom of the swirl tank where it would be trapped. This seems to be
working because I have found that after I open the system for some reason, the
level in the swirl tank will go down and there is never any air at the top of
the radiator.
After an engine run is the radiator the
same temperature at the inlet / outlet / bottom and top? If I have trapped air
only part of my radiator gets hot to the touch. Dual pass barrier leaking?
Seems to be. I have mistakenly laid
my arm on the top of the radiator after a run…usually I manage to get off
pretty fast! :>) I can not see into the radiator tank on the
barrier side. It is possible it could be leaking. I suppose if
there was a rag in the thing it could be trapped here also. I have no way
to see in there even if the hose was removed. I would need some kind of
flexible camera or something like that.
Use an extra CHT channel and clamp it to
the inlet of your radiator to measure Delta T.
Good idea. I will have to rig one
up. I don’t have an extra now.
My water pressure does not vary that much
in operation. But it does hold a little pressure for a few days after shutdown.
1-2 psi.
What is your pressure during
operation? What is the pressure cap rating? Does it vary at all
with temp and/or rpm? Mine is maxed out..always!
What size hoses? I’m running 1in.
The RX-8 uses 1.25 hoses. I stuck
with that size as well.
Where are you measuring water pressure?
The hose that comes off the top of the rear
iron goes to the top of the radiator, just below the cap. A tee in this line
has the water pressure sender in it. The radiator cap is just a cap, not
a pressure cap. The outlet in the radiator neck goes to the bottom of the
swirl tank.
Is your pressure cap on the bleed / swirl
tank?
Yes.
Any pictures of the plumbing?
Not of the current setup.
Bobby
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Bill Bradburry
Sent: Thursday, March 24, 2011
10:23 AM
To: Rotary
motors in aircraft
Subject: [FlyRotary] On the
subject of installations...Coolant Pressure
I need some help with figuring out my
cooling problems.
Just so it doesn’t get lost in the
following BS, I need to state that I think the problem is related to the
coolant pressure. It seems to me to be way too high. I am beginning
to think that the coolant is somehow partially blocked.
Now the rest of the story….
After I did the flight described in the
attached email, I installed an opening in the bottom of the cowl that would
work something like a cowl flap that is permanently open. The new opening
is 9 inches by 5 inches or 54 sq in.. There is a flare in front of the
opening that is at an angle of 45 degrees and extends down into the airstream
about 4 inches. (it is 6 inches long.) This opening is in addition
to two 6 X 6 openings, one of which has a 3 inch diameter exhaust pipe in it.
This helped a little, but nothing like I
expected it would. The pressure inside the radiator inlet dropped from 10
inches of water to 8 inches of water. (by the way, Steve was right about
it being inches of water and not inches of Hg.)
The pressure after the radiator and inside
the cowl dropped to 8 inches as well. The temperature of the water
dropped to 208 and the oil a couple of degrees. Neither of these had the
result that I expected.
My water pressure cap is rated at 21
lbs. I have not calibrated the sender that came with my EM-2 and it shows
3 lbs when the engine is cold. I assume that this is zero. When in
flight the pressure climbs to 24 lbs and stays there. I assume that at
this point, the cap is at 21 lbs and is bleeding off air. There is about
a pint to a quart of air above the coolant in the bleed tank.
This morning I ran the engine on the
ground for about 10-15 minutes at an rpm of 3000 to 3200. The OAT was 75
degrees.
I read the temps and pressures every
minute or two during the run. I hope this doesn’t get jumbled during
transmission.
Oil temp –
80
103
130
139 144
155
162 165
Air temp after cooler -
97
109
122
129
133 134
Water temp
-
86 126
161
173
178
190
198 199
Air temp after rad
-
109
133
157
169 179
183
Water pressure
-
2
11
17 20
21
24
I noticed that the water pressure could be
brought from 2 lbs to 9 lbs by changing the rpm while the engine was still
relatively cool
What should I expect for water pressure at
lower temps and how could I go about making a determination that the water
passages are clear?
I am beginning to think that a rag has
been left either in the engine or the radiator. I have never torn the
engine down and I sent the radiator out to have a leak repair a couple of years
ago. It is a double pass radiator. I can look into the end that has
both sides connected thru the radiator cap neck, but not into the inlet and
outlet end.
Suggestions???
Thanks,
Bill B
From: Bill Bradburry [mailto:bbradburry@bellsouth.net]
Sent: Sunday, March 20, 2011 5:29
PM
To: 'Rotary
motors in aircraft'
Subject: On the subject of
installations...
My water temp has been running between 199
and 217, depending on the OAT. The oil is pretty steady at around
175. Today I finally got to fly with pressure probes inside the
cowling. I was all set to try and enlarge the inlet to the radiator to
solve the problem. It turns out that “in” is not the problem, it is “out”
that is the problem!
I have 10 inches of Hg pressure in the
radiator inlet and 10 inches of Hg on the outlet side as well as the same
pressure everywhere I measured inside the cowl. I need to open up the
cowl some so more air can get out. I had considered a cowl flap but that
would not work in this instance because the problem is at cruise. I need
a permanent opening. I am considering louvers and I am looking for a
source. I know some of you are using them. Where did you get them
and how are they installed so that they look ok?
I am also considering some kind of flare
around the exit area to create a low pressure area to help suck air out.
Do any of you have those and do they seem to work?
While I look into this, I also need to do
something about my muffler…Thank you, Bobby!
I wonder about that spiral muffler some of
you are trying??
Bill B 9 hours and counting…
By the way, I was considering putting a 1
or 2 inch wide piece of cardboard across the bottom of the oil cooler to
partially block it in the hopes that more air would then flow through the
radiator. Sort of like truckers do with the radiator in cold
weather. What opinions do you have about that idea? I realize it
would make more sense if the oil was really cool, but I think the oil might not
get much hotter if an inch or so was blocked. What do you think???